2009 Weapons File

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PREFACE The 2009 Weapons File is published in response to requests from our “Warfighter” customers, and is an item you indicated had high utility. Distribution of this book is to U.S. Government Agencies and private individuals or enterprises eligible to obtain export-controlled technical data in accordance with DoDD 5230.25. All pages are marked For Official Use Only (FOUO). Ensure it is handled, stored, and disposed of accordingly. This twelfth edition published by the Air Armament Center, Eglin AFB, Florida has been revised and updated to reflect the latest armament information available. Additions include Chapter 23 “Aircraft,” Chapter 24 “Unmanned Aerial Vehicles (UAV),” and Chapter 25 “Test and Evaluation Instrumentation.” The Weapons File is designed to be used as a quick reference tool for information purposes only. It is not intended to be used as a procedural or technical manual in accomplishing mission planning, campaign planning, targeting functions or munitions maintenance operations. Air Force Weapons Technical Orders 1-1M-34 and -34-1 should be used by the operational community. Chapters 3 and 13 are concepts/technologies pending funding/program approval at publication. Remaining chapters focus on currently fielded, Air Force stock listed, as well as airborne delivered munitions, tactical missiles, weapons, gun systems and stores support equipment in development. The Weapons File is not intended to be a complete Department of Defense guide to weapon systems; however, it does contain several Navy and Army systems. The Weapons File is available online: https://peonet.eglin.af.mil/weapons and includes film clips and additional photographs of some systems. This is YOUR weapons file: therefore your help is needed to ensure only the most current and correct information is published. Suggestions for improvements in the form of additions, deletions, updates and corrections should be sent to: AAC/XR, 207 West Avenue D, Suite 300, Eglin AFB, FL 32542-6844 or email them to AAC/XR Capabilities Integration Directorate at [email protected] with Weapons File in the Subject Line. TO ORDER additional Weapons File hard copies, send your request to [email protected] with Weapons File in the Subject Line and provide a POC, Number of Books Requested, Mailing Address, Phone number, and email address.

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TABLE OF CONTENTS 1 June 2009 CHAPTER ONE - Air Intercept Missiles (AIM) AIM-7 AIM-9M AIM-9X AIM-120

Sparrow Sidewinder Next Generation Sidewinder Advanced Medium Range Air-to-Air Missile (AMRAAM)

1-1 1-3 1-5 1-7

CHAPTER TWO - Air-to-Ground Missiles (AGM) AGM-65 Series AGM-84D AGM-84K AGM-86/B AGM-86/C&D AGM-88B&C AGM-88E AGM-114 Series AGM-129A AGM-130 AGM-154 AGM-158

Maverick Harpoon Standoff Land Attack Missile-Extended Response (SLAM-ER) Air Launched Cruise Missile (ALCM) Conventional Air Launched Cruise Missile (CALCM) High Speed Anti-Radiation Missile (HARM) Advanced Anti-Radiation Guided Missile (AARGM) Hellfire Advanced Cruise Missile (ACM) Powered Standoff Weapon Joint Stand-Off Weapon (JSOW) Joint Air-to-Surface Stand-Off Missile (JASSM)

2-1 2-4 2-6 2-8 2-9 2-11 2-13 2-15 2-18 2-19 2-21 2-23

CHAPTER THREE - Directed Energy (DE) Technologies TBD TBD YAL-1A TBD TBD TBD TBD MX-20DLI Laser Dazzler Laser Dazzler TBD TBD TBD

Active Denial System (ADS) Advanced Tactical Laser (ATL) Airborne Laser (ABL) Counter-electronics HPM Advanced Missile Project (CHAMP) DE Airbase/Area Protection Tactical Relay Mirror System MAX POWER Standoff Intelligence Detection (SID) Personnel Halting and Stimulation Response (PHaSR) Aircraft Countermeasures (ACCM) Advanced Tactical DE System (ATADS) Imaging Seeker Countermeasures Proactive Infrared Countermeasures

3-1 3-3 3-5 3-6 3-8 3-10 3-12 3-13 3-15 3-16 3-17 3-18 3-19

CHAPTER FOUR - Unguided Munitions, Bombs, and Penetrators BDU-33D/B BDU-38 BDU-45 BDU-48 BDU-50 BDU-56 BLU-109/B, A/B, B/B, and C/B BLU-110/B, A/B, B/B, and C/B

25 lb. Practice Bomb Practice Bomb Practice Bomb 10 lb. Practice Bomb 500 lb. Practice Bomb 2000 lb. Practice Bomb Hard Target Penetrator Warhead

4-1 4-2 4-3 4-5 4-6 4-7 4-8

General Purpose (GP) Bomb

4-9

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CHAPTER FOUR - Unguided Munitions, Bombs, and Penetrators (Cont) BLU-111/B, A/B, B/B, and C/B BLU-113A/B BLU-116A/B BLU-117/B, A/B, B/B, and C/B BLU-119/B BLU-121A/B BLU-122/B BLU-126/B M117 M129/MJU-1 MK 56 MK 58 MOD 1 MK 62 MK 63 MK 65 MK 76 MOD 5 MK 77 MOD 5, 6 MK 81 MK 82 MK 83 MK 84 MK 106

General Purpose (GP) Bomb

4-11

Desert Storm Special Penetrator Warhead Special Purpose Bomb General Purpose (GP) Bomb

4-13 4-14 4-16

CrashPAD Enhanced Blast Weapon Hard Target Munition Penetrator Warhead Low-Collateral Damage (LoCo) Bomb 750 lb. GP Bomb Leaflet / Chaff Bomb Moored Mine Marine Location Marker Quick Strike Mine Quick Strike Mine Quick Strike Mine 25 lb. Practice Bomb Fire Bomb 250 lb. GP Bomb 500 lb. GP Bomb 1,000 lb. GP Bomb 2,000 lb. GP Bomb 5 lb. Practice Bomb

4-18 4-19 4-20 4-21 4-23 4-25 4-27 4-28 4-30 4-31 4-32 4-33 4-34 4-35 4-36 4-39 4-40 4-42

CHAPTER FIVE - Guided Bomb Units (GBU) BDU-59B/B GBU-10 Series GBU-12 Series GBU-12F/B GBU-15 EGBU-15 GBU-16 Series GBU-24/B GBU-24A/B GBU-24B/B GBU-24E/B and G/B GBU-27/GBU-27A/B GBU-28A/B & B/B GBU-28C/B GBU-28E/B GBU-31 GBU-32 GBU-38 GBU-39A/B GBU-39/B GBU-43/B GBU-44B GBU-51/B GBU-52/B GBU-54/B

Laser Guided Training Round (LGTR) Laser Guided Bomb (LGB) (2,000 lb.) Laser Guided Bomb (LGB) (500 lb.) Dual Mode Laser Guided Bomb (DMLGB) Guided Standoff Weapon (2,000 lb.) Enhanced Guided Standoff Weapons (2,000 lb.) Laser Guided Bomb (LGB) (1,000 lb.) Low Level Laser Guided Bomb (LGB) (2,000 lb.) Low Level Laser Guided Bomb (LGB) (BLU-109) Low Level Laser Guided Bomb (LGB) (BLU-109) Low Level Laser Guided Bomb (LGB) (BLU-109) GPS/INS/Laser Guided Bomb (LGB) (BLU-109) GPS/INS/Laser Guided Bomb (LGB) (BLU-113) GPS/INS/Laser Guided Bomb (LGB) (BLU-122/B) GPS/INS/Laser Guided Bomb (LGB) (BLU-113/B or A/B) Joint Direct Attack Munition (JDAM) (2,000 lb.) Joint Direct Attack Munition (JDAM) (1,000 lb.) Joint Direct Attack Munition (JDAM) (500 lb.) Small Diameter Bomb Increment I (SDB I) FLM Small Diameter Bomb Increment I (SDB I) (250 lb.) Massive Ordnance Air Blast (MOAB) (22,000 lb.) Viper Strike Laser Guided Bomb with LOCO Bomb Body Dual Mode Laser Guided Bomb (DMLGB) Laser Joint Direct Attack Munition (LJDAM) (500 lb.)

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5-1 5-3 5-5 5-7 5-8 5-10 5-12 5-13 5-15 5-16 5-17 5-18 5-19 5-20 5-21 5-22 5-25 5-27 5-29 5-31 5-33 5-34 5-36 5-37 5-38

CHAPTER FIVE - Guided Bomb Units (GBU) (cont) Paveway IV

Dual Mode GPS/INS and Laser Guided Bomb

5-40

CHAPTER SIX - Cluster Bomb Units (CBU) CBU-78 CBU-87 CBU-89 CBU-97 MK 20, CBU-99/100/B, A/B, B/B CBU-103/104/105 CBU-107/B CBU-116/118 PDU-5/B SUU-76C/B

Gator Combined Effects Munition (CEM) Gator Sensor Fuzed Weapon (SFW) Rockeye

6-1 6-4 6-7 6-9 6-12

Wind Corrected Munitions Dispenser (WCMD) Passive Attack Weapon (PAW) Power Distribution Denial Munition (PDDM) MK 20 Rockeye II Leaflet Canister (Filled) MK 20 Rockeye II Leaflet Canister (Empty)

6-14 6-16 6-18 6-20 6-20

CHAPTER SEVEN - Nuclear Weapons B61 B83-1 W62-0 W78-0 W80-1 W87-0

Nuclear Bomb Nuclear Bomb Nuclear Warhead Nuclear Warhead Nuclear Warhead Nuclear Warhead

7-1 7-2 7-3 7-4 7-5 7-6

CHAPTER EIGHT - Aircraft Gun Systems GAU-2B/A, “Minigun” Machine Gun (7.62mm) GAU-17A (Navy), M-134 (Army) GAU-8/A “Avenger” Cannon (30mm) GAU-12/U “Equalizer” Cannon (25mm) GAU-18/A; XM218 Machine Gun (.50 Caliber) GAU-19/A Gatling Gun (.50 Caliber) GAU-21 Machine Gun (.50 Caliber) GAU-22/A Cannon (25mm) M137A1 Cannon (105mm) M197 20mm Gatling Gun M2A1 “Bofors” Cannon (40mm) M230 30mm Chain Gun M240D Machine Gun (7.62mm) M61A1 “Vulcan” Cannon (20mm) M61A2 Lightweight Cannon (20mm) Mk44 “Bushmaster” Cannon (30mm)

8-1 8-2 8-3 8-4 8-5 8-6 8-7 8-8 8-9 8-10 8-11 8-12 8-13 8-14 8-15

CHAPTER NINE - Impulse Carts, Bomb Racks, Launchers, and Pylons Impulse Cartridges ARD 446-1B ARD 863-1A1W BBU-35/B BBU-36/B BBU-46/B & A/B

Impulse Cartridge Impulse Cartridge Impulse Cartridge Impulse Cartridge Impulse Cartridge

3

9-1 9-2 9-3 9-4 9-5

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CHAPTER NINE - Bomb Racks, Launchers, and Pylons (Cont) BBU-48/B BBU-59/B BBU-63/B M796 MK 107

Impulse Cartridge Impulse Cartridge Impulse Cartridge Impulse Cartridge Impulse Cartridge

9-6 9-7 9-8 9-9 9-10

Bomb Rack Bomb Release (Left and Right Hand) Bomb Rack Ejector Assembly Bomb Rack Ejector Assembly Bomb Shackle Bomb Rack Ejector Unit Rack Assembly Ejector Unit Rack Assembly Canted Vertical Ejector Rack (CVER) Bomb Ejector Rack Bomb Ejector Rack Improved Multiple Ejector Rack (IMER) Improved Triple Ejector Rack (ITER) Bomb Rack Bomb Rack Bomb Rack Bomb Rack Bomb Ejector Rack Aircraft Ejector Bomb Rack (30 Inch Ejector Rack) Smart Bomb Rack Bomb Ejector Rack Common Carriage Assembly Bomb Rack Bomb Rack Cluster Bomb Rack Family of 14” Bomb Racks Bomb Rack Bomb Rack Bomb Rack Smart Bomb Rack Assembly Bomb Dispenser Bomb Rack Bomb Rack (High Speed) Bomb Rack (Electronic)

9-11 9-12 9-13 9-14 9-15 9-16 9-17 9-18 9-19 9-20 9-21 9-22 9-23 9-24 9-25 9-26 9-27 9-28 9-29 9-30 9-31 9-32 9-33 9-34 9-35 9-36 9-37 9-38 9-39 9-40 9-41 9-42 9-43 9-44

Bomb Racks 14-Inch Bomb Rack A-6 Bomb Release AERO 7A-5 AERO 7B-4 B-11 Bomb Shackle BRU-15A BRU-32A/A BRU-32B/A BRU-33A/A BRU-36A/A BRU-36B/A BRU-41/A BRU-42/A BRU-44B/A BRU-46/A BRU-47/A BRU-52 BRU-55/A BRU-56/A BRU-57/A BRU-59/A BRU-61/A BRU-67/A BRU-68/A CBR MA-4 MAU-12 MAU-40/A MAU-50/A SBRA SUU-20 TER-9/A TER-9/A MOD TER-9/A MOD Launchers

16S210 Guided Missile Launcher AGMBRL Aircraft Guided Missile and Bomb Rotary Launcher CBM Conventional Bomb Module DRA Dual Rail Adapter LAU-7/A-6, B/A, /A-7, Guided Missile Launcher B/A-1, C/A, D/A, E/A, and F/A LAU-10C/B, D/B Guided Missile Launcher LAU-61C/A 2.75 inch Rocket Launcher

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9-45 9-46 9-47 9-48 9-49 9-50 9-51

CHAPTER NINE - Launchers and Pylons (Cont) LAU-68A/A, B/A, D/A, and LAU-131/A LAU-88 LAU-105/A LAU-106A/A LAU-115C/A LAU-115D/A LAU-116/A LAU-116A/A LAU-116B/A LAU-117(V)2/A LAU-117A(V)3/A LAU-118(V)1/A LAU-118(V)4/A LAU-127A/A, B/A, D/A, and E/A LAU-127C/A, FA LAU-128A/A, D/A LAU-128B/A LAU-129A/A LAU-139 LAU-141/A LAU-142/A LAU-144/A LAU-147/A LAU-148/A M299 Modified M299 RLA SECBM

2.75 inch Rocket Launcher

9-53

Guided Missile Launcher Guided Missile Launcher Guided Missile Launcher Guided Missile Launcher Guided Missile Launcher (LH/RH) Guided Missile Launcher (LH/RH) Guided Missile Launcher (LH/RH) Guided Missile Launcher Guided Missile Launcher Guided Missile Launcher Guided Missile Launcher Guided Missile Launcher Guided Missile Launcher

9-55 9-56 9-57 9-58 9-59 9-60 9-61 9-62 9-63 9-64 9-65 9-66 9-67

Guided Missile Launcher Guided Missile Launcher Guided Missile Launcher (BOL) Guided Missile Launcher Guided Missile Launcher Configurable Rail Launcher (CRL) AMRAAM Vertical Eject Launcher (AVEL) Munitions Launcher Assembly Missile Launcher External Rail Launcher Missile Launcher Missile Launcher Rail Advanced Application Rotary Launcher MIL-STD-1760 Conventional Bomb Module

9-68 9-69 9-70 9-71 9-72 9-73 9-74 9-75 9-76 9-77 9-78 9-79 9-80 9-81

Power Sources F-35 Pneumatic Power Source (PPS)

9-82

Pylons Station 1 and 11 Station 2 and 10 Station 3 and 9 Station 4 and 8 Station 5 and 7 Station 6 Pylon Pylon ALE-25 Pylon LASER POD (LITENING) Pylon SUU-59B/A SUU-59C/A SUU-60B/A SUU-62/A, B/A SUU-63

A-10 Pylon A-10 Pylon A-10 Pylon A-10 Pylon A-10 Pylon A-10 Pylon F-22A Pylon Integrated Conventional Stores Management System (ICSMS) Pylon B-52H Aircraft Pylon B-52H Aircraft Pylon

9-83 9-84 9-85 9-86 9-87 9-88 9-89 9-90

F-15 Inboard Aircraft Pylon F-15 Inboard Aircraft Pylon F-15 Centerline Aircraft Pylon F/A-18 Centerline Aircraft Pylon F/A-18 Centerline Aircraft Pylon

9-94 9-95 9-96 9-97 9-98

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9-92 9-93

CHAPTER NINE - Launchers and Pylons (Cont) SUU-67/A SUU-72/A SUU-73/A WWP WWP (PIDS)

Pylon Pylon F-15 Centerline Aircraft Pylon Wing Weapons Pylon Assembly Wing Weapons Pylon Integrated Dispenser System

9-99 9-100 9-101 9-102 9-103

CHAPTER TEN - Countermeasures ADM-141A, B ADM-141C ADM-160B ADM-160C ALA-17 ALA-17/B AN/ALE-20 AN/ALE-48 AN/ALE-49 AN/ALE-50A(V)1 AN/ALE-50(V)2 LAU-74 LUU-1, -5 LUU-2, -19 M206 M206 (T-2)/B M211 M212 MJU-7A/B MJU-7(T-2)/B MJU-10/B MJU-11 MJU-12 MJU-17 MJU-23A/B MJU-27A/B MJU-32/B MJU-38/B MJU-32A/B & MJU-38A/B MJU-39/B MJU-40/B MJU-46/B MJU-47/B MJU-48/B MJU-49/B MJU-50 MJU-50/B MJU-51A/B MJU-52/B MJU-53/B MJU-55/B MJU-57/B

Tactical Air-Launched Decoy (TALD) Improved Tactical Air-Launched Decoy (ITALD) Miniature Air Launched Decoy (MALD) Miniature Air Launched Decoy-Jammer (MALD-J) Flare Rack IR Flare Cartridge Flare Ejector Set Chaff Dispenser Flare Dispenser Countermeasures Decoy Dispensing Set (CMDDS) Countermeasures Decoy Dispensing Set (CMDDS) Flare Launcher System Target Marker Illuminating Flare IR Flare Flare Simulator Decoy IR Flare IR Flare Flare Simulator IR Flare Chaff/Flare Magazine Flare Magazine Flare Magazine IR Countermeasure Flare IR Decoy Device IR Decoy Flare IR Decoy Flare IR Decoy Flare

10-1 10-3 10-5 10-7 10-9 10-10 10-11 10-12 10-13 10-14 10-16 10-18 10-19 10-20 10-21 10-23 10-24 10-26 10-27 10-28 10-29 10-30 10-31 10-32 10-33 10-34 10-35 10-36 10-37

IR Flare IR Flare IR Flare IR Flare IR Flare IR Decoy Device IR Decoy Flare Decoy Decoy Decoy IR Flare IR Decoy Flare IR Decoy Flare

10-38 10-39 10-40 10-42 10-43 10-44 10-45 10-46 10-48 10-49 10-51 10-52 10-53

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CHAPTER TEN – Countermeasures (Cont) MJU-57A/B MJU-61/B MJU-62/B MJU-64/B RR-129/AL RR-129A/AL RR-144A/AL RR-170A/AL RR-170A/AL (Navy) RR-180/AL RR-188/AL RR-196/AL FT-1289/ALE SM-875B/ALE SUU-25

IR Decoy Flare IR Decoy Flare IR Flare IR Decoy Device Chaff Cartridge Chaff Cartridge Chaff Cartridge Chaff Cartridge Chaff Cartridge Chaff Cartridge Chaff Cartridge Chaff Cartridge GEN-X Decoy IR Simulator Flare Flare Dispenser

10-54 10-55 10-56 10-57 10-58 10-59 10-60 10-61 10-62 10-63 10-64 10-65 10-66 10-67 10-68

CHAPTER ELEVEN - Fuzes and Sensors DSU-33A/B, B/B, C/B & D/B DTU-31/B FMU-54A/B FMU-56/B, D/B FMU-81 FMU-110 FMU-113 FMU-124 FMU-139A/B, C/B FMU-140 Series FMU-143B/B-Q/B FMU-152A/B FZU-39/B M904E4 M905 M907 MK 339 MOD 1

Proximity Sensor

11-1

Bomb Adapter Timer-Actuator Impact Bomb Fuze Bomb Proximity Fuze Bomb Impact Fuze Proximity Fuze Proximity Fuze Guided Bomb Impact Fuze Electronic Bomb Fuze Dispenser Proximity Fuze Electronic Bomb Fuze Electronic Bomb Fuze Proximity Fuze Sensor Mechanical Bomb Fuze, Nose Mechanical Bomb Fuze, Tail Mechanical Fuze, Airburst Mechanical Time (MT) Fuze

11-2 11-3 11-4 11-5 11-6 11-7 11-8 11-9 11-10 11-12 11-13 11-14 11-15 11-16 11-17 11-18

CHAPTER TWELVE - Munitions Material Handling Equipment (MMHE) 2.75 Inch Rocket Transport Module 20mm Ammunition Loading System (ALS) Replenisher Assembly 20mm Replenisher Table ADU-537 A/E Missile Munitions Loading Adapter (MMLA) A/E32K-3 Munitions Assembly Conveyor (MAC) A/E32K-9 Munitions Assembly Conveyor II (MACII) ALE-40 Series Chaff/Flare Transport Module ALE-50 Series Decoy Transport Module

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12-1 12-2 12-3 12-4 12-5 12-6 12-7 12-8

CHAPTER TWELVE - Munitions Material Handling Equipment (MMHE) (Cont) ALS

20mm Ammunition Loading System (ALS) Loader Assembly Aluminum Rail Set (ARS) Practice Bomb Transport Module (40 Round Version) Practice Bomb Transport Module (80 Round Version) 30mm Ammunition Loader 20mm USAF Linkless Ammunition Loading System (LALS) Truck, Lift, Aerial Stores Truck, Lift, Aerial Stores Munitions Handling Trailer Munitions Handling Trailer Manually Operated Lift Truck (MOLT) Munitions Handling Trailer Munitions Lift Trailer Munitions Handling Trailer Truck, Lift, Aerial Stores Mechanical RAM Assembly (MRA) 20mm Universal Ammunition Loading System (UALS) Loader Assembly Munitions Materiel Handling Equipment Focal Point

ARS BDU-33/MK-106 BDU-33/MK-106 GFU-7/E LALS MHU-40 MHU-83 MHU-110/M MHU-141/M MHU-194/E MHU-196/M MHU-204/M MHU-226 MJ-1 MRA UALS MMHE Website

12-9 12-10 12-11 12-12 12-13 12-14 12-15 12-16 12-17 12-18 12-19 12-20 12-21 12-22 12-23 12-24 12-25 12-26

CHAPTER THIRTEEN - Emerging Technologies TBD TBD TBD TBD TBD TBD TBD TBD TBD TBD TBD TBD TBD BLU 127/B, GBU-57/B TBD TBD TBD TBD TBD

Accurate Low Collateral Munition (ALM) Advanced Precision Kill Weapon System (APKWS) Area Dominator (AD) Close Combat Lethal Recon (CCLR) Conventional Strike Missile (CSM) Direct Attack Guided Rocket (DAGR) Hard Target Void Sensing Fuze (HTVSF) High Speed Strike Weapon (HSSW) I-500 Warhead Technology Demonstration (TD) I-1000 Warhead Technology Demonstration (TD) Joint Air-to-Ground Missile (JAGM) Low Cost Guided Imaging Rocket (LOGIR) Low Cost Mini-Cruise Missile (LCMCM) Massive Ordinance Penetrator (MOP) Shredder (Mod BLU-109) Small Diameter Bomb Increment II (SDB II) Small Smart Weapon (SSW) Very Small Missile (VSM) Tactical Wide Area Search Munition (WASM)

13-1 13-2 13-4 13-6 13-7 13-8 13-9 13-10 13-11 13-12 13-13 13-15 13-16 13-18 13-19 13-20 13-21 13-23 13-24

CHAPTER FOURTEEN - Personal, Individual, Crew Served, and Mission Specific Weapons Personal Weapons M9 M11

9mm Pistol (Personal Defense Weapon (PDW) 9mm Compact Pistol

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14-1 14-2

CHAPTER FOURTEEN - Personal, Individual, Crew Served, and Mission Specific Weapons (Cont) Individual Weapons M16/M16A2 M4/M4A1 MK-14 Mod 0 M-32 M203, A1, and A2 XM320 M249 Crew Served Weapons

5.56mm Rifle 5.56mm Carbine 7.62 Enhanced Battle Rifle (EBR) 40mm Multiple Grenade Launcher (MGL) 40mm Grenade Launcher 40mm Grenade Launcher Module (GLM) 5.56mm Automatic Rifle (AR)

14-3 14-4 14-5 14-6 14-7 14-8 14-9

M240B 7.62mm Machine Gun (MG) MK 19 40mm Grenade Machine Gun (GMG) M2 Cal .50 Machine Gun (MG) Mission Specific Weapons

14-10 14-11 14-12

Shotguns M24 M107 M110 M40A3

14-13 14-15 14-16 14-17 14-18

12 gauge Shotguns 7.62mm Sniper Weapons System (SWS) Rifle (USA) Cal.50 Special Application Sniper Rifle (SASR) 7.62mm Semi-Automatic Sniper system (SASS) 7.62mm Sniper Rifle

CHAPTER FIFTEEN - Small Arms/Gun Munitions 5.56mm 7.62mm 9mm Caliber .50 12 Gauge Cartridges

Ammo Ammo Ammo Ammo Ammo

15-1 15-3 15-5 15-6 15-8

CHAPTER SIXTEEN - Ground Defense Munitions Hand Grenades MK1A1 MK3A2 M7A3 M8 M14 M18 M25A2 M67 M69 M83 M84 Rubber Ball

Training Hand Grenade Concussion Offensive Hand Grenade Riot Control Grenade White Smoke Grenade Incendiary Grenade Colored Smoke Grenade Riot Control Hand Grenade Fragmentation Hand Grenade Practice Hand Grenade Practice Smoke Grenade Stun Grenade Riot Control Grenade

16-1 16-2 16-3 16-4 16-5 16-6 16-7 16-8 16-9 16-10 16-11 16-12

40mm Target Practice 40mm High Explosive (HE) 40mm High Explosive Dual Purpose (HEDP) 40mm High Explosive Dual Purpose (HEDP) 40mm Multiple Projectile 40mm White Star Parachute

16-13 16-14 16-15 16-16 16-17 16-18

40mm Grenades M385A1 M406 M430A1 M433E1 XM576 M583

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CHAPTER SIXTEEN - Ground Defense Munitions (Cont) M585 XM651E1 M674 XM675 M715 M716 M781 M918 XM1006 M1029 XM1057

40mm White Star Cluster 40mm Riot Control Agent 40mm Riot Control Agent 40mm Red Smoke 40mm Green Smoke 40mm Yellow Smoke 40mm Target Practice 40mm Target Practice Linked 40mm Sponge Grenade 40mm Non-Lethal Crowd Dispersal 40mm Non-Lethal Crowd Dispersal

16-19 16-20 16-21 16-22 16-23 16-24 16-25 16-26 16-27 16-28 16-29

CHAPTER SEVENTEEN - Medium and Large Caliber Ammunition PELE PGU-27 Series PGU-28 Series PGU-30 Series PGU-23/U PGU-25/U PGU-13/B PGU-14A/B PGU-15/B PGU-9C/B PGU-43/B PGU-44/B PGU-45/B FMU-160/B FMU-153/B M739A1

20mm PELE KE 20mm Target Practice (TP) (20x102 NATO) 20mm Semi-Armor Piercing High Explosive Incendiary (SAPHEI) (20x102 NATO) 20mm Target Practice Tracer (TPT) 25mm Target Practice (TP) (25x137mm NATO) 25mm High Explosive Incendiary (HEI) (25x137mm NATO) 30mm High Explosive Incendiary (HEI) (30x173mm NATO) 30mm Armor Piercing Incendiary (API) 30x173mm NATO) 30mm Target Practice (TP) (30x173mm NATO) 40mm High Explosive Incendiary-Plugged (HEI-P) (L-60 NATO) 105 mm Training Practice (TP) 105mm High Explosive (HE) (105mm NATO Artillery) 105mm High Explosive/High Fragmentation (HE/HF) (105mm NATO Artillery) Proximity Fuze Fuze Point Detonating (PD) Fuze Point Detonating (PD)/Delay

17-1 17-2 17-3 17-4 17-5 17-6 17-7 17-8 17-9 17-10 17-11 17-12 17-13 17-14 17-15 17-16

CHAPTER EIGHTEEN - Aircraft Rocket Systems 2.75 Inch and 5.0 Inch MK 66 M423/427 M439 RC M442 M151 WTU-1/B M274 M229 M257 M278 M261 M267 M255A1

2.75-inch Rocket Motor Point Detonating (PD) Fuze Variable Time Delay, Remotely Settable Fuze Fuze HE Warhead Training Warhead Smoke Signature Training Warhead HE Warhead Illumination Warhead Infrared (IR) Illumination Warhead HE Multi-Purpose Sub-munition (MPSM) Multi-Purpose Sub-munition (MPSM) Smoke Signature (Training) Flechette Warhead

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18-1 18-5 18-6 18-7 18-8 18-9 18-10 18-11 18-12 18-13 18-14 18-16 18-18

CHAPTER EIGHTEEN - Aircraft Rocket Systems 2.75 Inch and 5.0 Inch (Cont) M264 M156 MK 146 Mod 0 WDU-4A/A MK 71

Smoke, Red Phosphorous White Phosphorous (WP) HE Frag Warhead Flechette Warhead Zuni Rocket

18-19 18-20 18-21 18-22 18-23

CHAPTER NINETEEN - Army Artillery Munitions M198 M177A1, A2 M109A6 M107 M549A1 M712 M804A1 M898 M483A1 M692/M731 M718, M718A1/M741, M741A1 M795 M864

155mm Towed Howitzer 155mm Lightweight Towed Howitzer 155mm Paladin Self Propelled (SP) Howitzer 155mm HE Round 155mm Rocket Assisted Projectile (RAP) 155mm HE, Guided Cannon Launched, Copperhead 155mm Practice Round 155mm SADARM (Sense and Destroy Armor) 155mm Dual Purpose Improved Conventional Munition (DPICM) Area Denial Artillery Munition (ADAM) 155mm Remote Anti-Armor Mine System (RAAMS)

155mm HE Round 155 mm Extended Range (ER) Dual-Purpose Improved Conventional Munition (DPICM) M864 Recap Program M110, M110A1, M110A2 155mm White Phosphorus (WP) M825A1 155mm Smoke M485A2 155mm Illumination XM982 155mm Guided, HE, ER-DPICM, EXCALIBUR M119A1/A2 105mm Towed Howitzer M102 105mm Towed Howitzer M1 105mm High Explosive (HE) M60A2 105mm Smoke Cartridge M84A1 105mm Smoke Cartridge M314A3 105mm Illuminating Cartridge M444 105mm High Explosive (HE) Improved Conventional Munition (ICM) M760 105mm High Explosive (HE) M913 105mm High Explosive Rocket Assisted (HERA) M915 105mm Dual Purpose Improved Conventional Munition (DPICM) M927 105mm High Explosive Rocket Assisted (HERA) M546 105mm Anti-Personnel Projectile with Tracer (APERS-T) M557 Fuze Pont Detonating (PD) M564, M565 Fuze, Mechanical Time (MT) M565 and Mechanical Time Superquick (MTSQ) M564 M577A1 Fuze, Mechanical Time and Superquick (MTSQ) M582A1 Fuze, Mechanical Time Superquick (MTSQ) M728 Proximity Fuze M732 Series Proximity Fuze

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19-1 19-2 19-4 19-6 19-7 19-8 19-9 19-10 19-11 19-12 19-13 19-14 19-15 19-16 19-17 19-18 19-19 19-20 19-22 19-23 19-24 19-25 19-26 19-27 19-28 19-29 19-30 19-31 19-32 19-33 19-34 19-35 19-36 19-37 19-38 19-39

CHAPTER NINETEEN - Army Artillery Munitions (Cont) M732A2 M739 M739A1 M762A1/M767A1 M782 MK339 Mod 1

Proximity Fuze Fuze Point Detonating (PD)/Delay Fuze point Detonating (PD)/Delay Electronic Time Fuze Artillery Multi Option Fuze Artillery (MOFA) Point Detonating (PD)/Delay Fuze

19-40 19-41 19-42 19-43 19-44 19-45

CHAPTER TWENTY - Army Mortar Munitions M120/121 M934A1 M934A2 M933A1 M929 M930 M983 M931 M224 M720A1 M768 M888 M722A1 M721 M767 M769 XM1061 M252 M821A1/M889A1 M821A2/M889A1E1 M821A2E1/XM1058 M819 M853A1 M816 M879 XM784/XM785

120mm Mortar 120mm High Explosive (HE) Cartridge 120mm HE Insensitive Munition (IM) Cartridge 120mm High Explosive (HE) Cartridge 120mm White Phosphorus (WP) Smoke Cartridge 120mm Visible Light (VL) Illuminating Cartridge 120mm Infrared (IR) Illuminating Cartridge 120mm Full Range Practice Cartridge (FRPC) 60mm Mortar 60mm High Explosive (HE) Cartridge 60mm High Explosive (HE) Cartridge 60mm High Explosive (HE) Cartridge 60mm White Phosphorus (WP) Smoke Cartridge 60mm Visible Light (VL) Illuminating Cartridge 60mm Infrared (IR) Illuminating Cartridge 60mm Full Range Practice Cartridge (FRPC) 60mm Enhance Fragmentation Mortar Cartridge 81 mm Mortar 81mm High Explosive (HE) Cartridge 81mm High Explosive (HE) Cartridge 81mm High Explosive (HE) Cartridge 81mm Red Phosphorous (RP) Cartridge 81mm Visible Light (VL) Illuminating Cartridge 81mm Infrared (IR) Illuminating Cartridge 81mm Full Range Practice Cartridge (FRPC) 81mm Electronic Time (ET) Fuze

20-1 20-2 20-3 20-4 20-5 20-6 20-7 20-8 20-9 20-10 20-11 20-12 20-13 20-14 20-15 20-16 20-17 20-18 20-19 20-20 20-21 20-22 20-23 20-24 20-25 20-26

CHAPTER TWENTYONE - Army Rockets and Missiles M270A1 M142 M30/XM31 M39,M39A1, M48, M57

Multiple Launch Rocket System (MLRS) High Mobility Artillery Rocket System (HIMARS) Guided Multiple Launch Rocket System (GMLRS) Army Tactical Missile System (ATACMS)

21-1 21-3 21-5 21-7

CHAPTER TWENTYTWO - Test Equipment AN/GYQ-79A Test Common Munitions Built-in-Test Reprogramming Program Set Equipment (CMBRE) A-10A/C Armament Test Equipment B-52H Multi-User System Tester Next Generation (MUSTANG) F-15 Armament Test Equipment Cruise Missile Automatic Test Equipment TTU-584/E Common Organizational Level Tester (COLT)

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22-1 22-3 22-7 22-9 22-12 22-15

CHAPTER TWENTYTHREE - Aircraft B-1B B-2A B-52H A-10 F-15A-D F-15E F-16 F-22A F-35 F/A-18A/D F/A-18E/F EA-18G AV-8B EA-6B P-3C AC-130H/U HC-130P/N MC-130E/H/W C-130 C-17 CV-22 AH-64D AH-6A AH-1W/Z OH-58D HH-60G MH-60 UH-60A/L CH-53D CH-53E UH-1N/Y H-46 CH-47

Lancer Spirit Stratofortress Thunderbolt II Eagle Strike Eagle Fighting Falcon Raptor Joint Strike Fighter (JSF) (Lightning II) Hornet Super Hornet Airborne Electronic Attack Aircraft (Growler) Harrier II Prowler Orion Maritime Patrol and Anti-Submarine Warfare Aircraft Gunship Hercules Combat Talon I/II Hercules (Cargo) Globemaster III Osprey Longbow Apache Little Bird Super Cobra Kiowa Warrior Pave Hawk Pave Hawk Black Hawk Sea Stallion Super Stallion Iroquois Sea Knight Chinook

23-1 23-3 23-5 23-7 23-10 23-12 23-14 23-17 23-20 23-22 23-25 23-27 23-29 23-31 23-33 23-35 23-37 23-39 23-41 23-44 23-46 23-48 23-50 23-51 23-53 23-54 23-56 23-58 23-60 32-62 23-64 23-66 23-68

CHAPTER TWENTYFOUR - Unmanned Aerial Vehicles (UAV) MQ-1B MQ-1C MQ-9 RQ-4 RQ-5A/MQ-5B/C RQ-7B RQ-8B MQ-11B TBD TBD RQ-16A

Predator Sky Warrior Reaper Global Hawk Hunter Shadow Fire Scout Raven Wasp ScanEagle T-Hawk

24-1 24-3 24-5 24-7 24-9 24-11 24-13 24-15 24-17 24-19 24-21

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CHAPTER TWENTYFIVE - Test and Training Instrumentation AN/ARQ-52B (V)17 - Pod Advanced Range System (ARDS) AN/ARQ-52C (V)17 - Pod New AN/ARQ-52B (V)18 - Plate AN/ASQ-T50(V)1, (V)2 P5 Combat Training System/Tactical Combat Training System Common Range Integrated Instrumentation System (CRIIS)

APPENDIXES Aircraft and Weapons Matrix Aircraft Guns/Racks Matrix Aircraft Launchers Matrix Missile Designations Munitions Designations

A1 A-7 A-9 A-10 A-11

Acronym List

B1

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25-5 25-6

CHAPTER ONE 1 June 2009

AIR INTERCEPT MISSILES (AIM)

FOR OFFICIAL USE ONLY

INTENTIONALLY LEFT BLANK

Nomenclature: AIM-7

Name: Sparrow

Capability: Medium Range Air-to-Air Missile provides Neutralization of Fixed-Wing Aircraft, Rotary Helicopter, and Cruise Missile Airborne Targets. Description: The AIM-7 Sparrow is a radar-guided air-to-air missile with a high-explosive warhead. The versatile Sparrow has all-weather, all-altitude operational capability and can attack highperformance aircraft and missiles from any direction. It is a deployed missile used by some North Atlantic Treaty Organization (NATO) forces. The missile has four major sections: guidance; warhead; control; and rocket motor. It has a cylindrical body with four wings at midbody and four tail fins. Although external dimensions of the Sparrow remained relatively unchanged from model to model, the internal components of newer missiles represent major improvements with vastly increased capabilities. Characteristics: CRD Weapons Code Z07FC Z07FB Z07FD Z07MA

MISSILE AIM 7 F TRAINER MISSILE AIM 7 F CAPTIVE MISSILE AIM 7 F/M LOAD TRAINER MISSILE AIM 7 M TRAIN/CAP

Guidance Control Autopilot Class Weight (lbs.) Length (in.) Diameter (in.) Warhead Explosive (NEW) Fuze Propulsion Carriage Options: Aircraft: F-15A-E F-16A-B F/A-18A-F

Z07FA M07FB M07HA M07HB

MISSILE AIM-7M-F1 WAU-10 AUR MISSILE AIM-7M-F1 WAU-17 AUR MISSILE AIM-7M-H WAU-10 AUR MISSILE AIM-7M-H WAU-17 AUR

Semi-Active radar and Home-On-Jam (HOJ) (H Build) (WGU-6, WGU-23) Wing, Hydraulic (WCU-5, WCU-15) Roll Rate Air Intercept Missile 510 147 8 86 lbs.; Continuous Rod (WAU-10); Blast/Frag (WAU-17) PBXN-3, 26 lbs. (WAU-10); 36 lbs. (WAU-17) Proximity RF and active radar; contact Rocket Motor, MK 58

Launcher: LAU-106 16S1501

Contractor / Status / Improvements / Special Equipment: Contractor Raytheon Missile Systems Company, Tucson, AZ Status Inventory, (Proposed DEMIL of remaining AF inventory by FY08) Notes Joint Navy/Air Force (Navy lead) Special Equipment DSM-162 Field Test Set TO 33D9-30-36-1 Support Equipment TO 33D9-1-392

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Management/Engineering: NAVAIRSYSCOM PMA-259, NAS Patuxent River, MD (AF) - 575 CBSS/GBLD, Robins AFB, GA Technical Order: 21M-AIM7M-2

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Nomenclature: AIM-9M

Name: Sidewinder

Capability: Short Range Air-to-Air Missile provides Neutralization of Fixed-Wing Aircraft, Rotary Helicopter, and Cruise Missile Airborne Targets. Description: The sidewinder is a supersonic, heat-seeking, air-to-air missile carried by fighter aircraft. It has a high-explosive warhead and an active infrared guidance system. The missile is comprised of five major components: the Guidance Control Section (GCS), Target Detector (TD), Safety Arming Device (S-A), Warhead, and Rocket Motor. Four fin assemblies attach to the GCS and four wings assemblies attach to the Rocket Motor. An optional TMU-72 Coolant Tank, used by the Air Force, provides on-board source of coolant (argon) used to cool the Refrigerated Detector Unit (RDU) in the GCS during captive carriage phase of flight. Characteristics: CRD Weapon Code M09MA M09MB Z09WA M09MC Z09LD Z09LE Z09LC Z09LF Z09LA

MISSILE AIM-9M-1 AUR MISSILE AIM-9M-7 AUR AIM-9M AUR WSEP AIM-9M-9 AUR CATM-9L-10 (AUR) CATM-9L-10 (MBA) CATM-9L-3 (AUR) CATM-9L-7 (AUR) CATM-9L-9 (AUR)

Z09LB Z09MA SZRAA Z09MD Z09ME Z09MC Z09MB Z09MF

CATM-9L-9 (MBA) CATM-9M-9(AUR) STAMP AIM-9-9 CATM-9M-10 CATM-9M-10 (MBA) CATM-9M-3 (AUR) CATM-9M-3 (MBA) CATM-9M-7 (AUR)

Guidance Control -

Passive Infrared Homing Four Stabilizing Wing and Rolleron Assemblies and four Movable Canards with Servo Assembly Class Air Intercept Missile Weight (lbs.) 191.7 Length (in.) 113 Diameter (in.) 5 Fin/Wing Span (in.) - 25.0 Warhead 20.8 lbs. Annular Blast / Fragmentation Explosive (NEW) - 7.9 lbs. PBXN-3 Fuze Contact and Active Optical (DSU-15A/B, B, B/B) Propulsion MK 36 Solid Rocket Motor Carriage Options: Aircraft: A -10 F-15A-E F-16A-D F/A-18A-F AV-8B

Launcher: LAU-105 LAU-128 LAU-129, 16S210 LAU-7D/A and LAU-127A/A and LAU-127B/A

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Contractor / Status / Improvements / Special Equipment: Contractor Raytheon Missiles Systems Company, Tucson, AZ Status FMS/Inventory (40+ Countries) Special Equipment GCU-30 Recharging Unit and TS 4044 Test Set Management/Engineering: (AF) - 575 CBSS/GBLD, Robins AFB, GA AIM-9M - NAVAIRSYSCOM PMA-259, NAS Patuxent River, MD Technical Order: 21M-AIM9M-2

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Nomenclature: AIM-9X

Name: Next Generation Sidewinder

Capability: Short Range Air-to-Air Missile provides Neutralization of Fixed-Wing Aircraft, Rotary Helicopter, and Cruise Missile Airborne Targets. Description: The AIM-9X Sidewinder is a 5th generation supersonic, air-to-air guided missile that has full day/night capability and employs a passive infrared (IR) target acquisition system, proportional navigational guidance, a closed-loop position servo Fin Actuator Unit (FAU), and a Target Detector (TD). A solid-propellant Rocket Motor (RM) propels the missile and incorporates a manual SAFE-ARM selector assembly. The AIM-9X is configured with an Annular Blast Fragmentation (ABF) warhead controlled by an Electronic Safe-Arm Device (ESAD). Four forward mounted fixed wings provide aerodynamic lift and stability. Airframe maneuvering is accomplished by four control fins, mounted in line with the fixed wings, and activated by the FAU. The Jet Vane Control (JVC) provides enhanced maneuverability by deflecting rocket motor thrust to aid in turning. Characteristics: CRD Weapons Code M9XB MISSILE AIM 9X AUR (-10) M9XA MISSILE AIM 9X AUR (-20) M9WA MISSILE AIM 9X CATM Guidance Imaging Focal Plane Array (FPA) Infrared (IR) sensor with improved Infrared Counter-Countermeasures (IRCCM) Seeker - high off-boresight acquisition/launch Control Fixed forward wings with new tail Control Actuation Section (CAS) incorporating Jet Vane Control (JVC), within visual range to near beyond visual range Class Air Intercept Missile Weight (lbs.) - 188 Length (in.) 119 Diameter (in.) - 5 Wing Span (in.) -13.9 Fin Span (in.) - 17.5 Warhead 20.8 lbs. Annular Blast/Fragmentation (WDU-17/B) Explosive 7.9 lbs. PBXN-3 Fuze Contact and Active Optical (DSU-36/B and DSU-37/B) Propulsion Supersonic MK 139 MOD 0/MOD 1 Solid Rocket Maneuverability - Thrust Vector Control Carriage Options: Threshold Aircraft: F-15C-D F/A-18C-D Objective Aircraft: F-16C-D F-15E (est 2015) F/A-18E-F F-22A (Internal) (est 2014) F-35 (External) (est 2013)

Launcher: LAU-128A/A LAU-127E/A LAU-129A/A LAU-128A/A, D/A LAU-127C/A, F/A LAU-141/A Advanced Rail Launcher

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Contractor / Status / Improvements / Special Equipment: Contractor Raytheon Missile Systems Company, Tucson, AZ Status Full Rate Production, FMS (8 Countries) Improvements AIM-9X BLK II, DT FY09, OT FY10 Special Equipment - TTU-574 Test Program Set and GYQ-79 Common Munitions Bit Reprogramming Equipment (CMBRE) Management/Engineering: OPR: Joint USAF/USN Program, USN Lead Service USN - NAVAIRSYSCOM PMA-259, NAS Patuxent River, MD USAF - 328 ARSG (AF), Eglin AFB, FL, Support Activity: USN - NAWC-WD, Code: 47J320D, China Lake CA USAF - 575 CBSS/GBLD, Robins AFB GA Technical Order: 21M-AIM9X-2

AIM-9X-1

AIM-9X-2

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Nomenclature: AIM-120

Name: Advanced Medium Range Air-to-Air Missile (AMRAAM)

Capability: Provides all frontline USAF and Navy and many FMS fighter aircraft with the ability to attack airborne targets at beyond visual range, in all weather, in a launch and leave mode. The missile is currently used in FMS ground launch systems and is planned for integration with an US Army ground launch system. Description: The AIM-120 missile is a medium range, radar guided air-to-air missile with ground-to-air potential. The missile is 12 ft long; weighs about 350 lbs.; has four mid-body fixed wings; four moveable rear fins; and an umbilical connection which allows communication with the launch platform for targeting and initialization. The missile consists of four sections: guidance, armament, propulsion, and control. The guidance section includes the hardware and software necessary for target acquisition and track, navigation, data link processing, and electrical power distribution. The guidance section contains the: seeker/servo electronics, transmitter/electrical conversion unit (ECU), electronics unit, inertial reference unit (IRU), and quad/target detection device (QTDD). The QTDD antennas are mounted in the aft portion of the guidance section and are covered with a fiberglass wrap. Alpha codes located after guidance section part numbers define software for AIM-120A missiles. The AIM-120B and AIM-120C guidance sections are reprogrammable and do not use alpha codes. The armament section includes a warhead assembly and a MK44 MOD 1 booster threaded onto a safe and arming fuze (SAF) device. The high performance propulsion section uses a single, reduced-smoke hydroxyl-terminated polybutadiene (HTPB) solid propellant in a boost-sustain configuration encased in an asbestosfree insulated steel case (an integral part of the airframe). It is also equipped with an integral aft closure/blast tube/nozzle assembly with a removable exit cone. Beginning with the AIM-120C-5 the missile has an enhanced motor with an additional 5 inches of propellant and is commonly referred to as the +5 rocket motor. The control section consists of control electronics, actuator batteries, and four independently controlled servo-actuators. A shortened control actuation section (SCAS) is used with the +5 rocket motor. Characteristics: CRD Weapons Code M12AA M12BA M12CA TBD Guidance Control Class

MISSILE AIM-120A AUR MISSILE AIM-120B AUR MISSILE AIM-120C AUR MISSILE AIM-120D AUR

M12CB M12CC SZRBB --------------

MISSILE AIM-120C-4 AUR MISSILE AIM-120C-5/6 AUR STAMP AIM-120 (32 MX PACKAGE) -----------------------------------------------

- Inertial/Command Inertial and Active Radar - Fixed mid-body mounted wings with electric motor driven tail fins - Air Intercept Missile

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AIM - 120A

Lots 1 - 5

AIM - 120B

Lots 6 - 7

AIM - 120C3

Lots 8 -10

AIM - 120C4

Lot 11

Adds an improved warhead

AIM - 120C5

Lot 12

Includes the +5 rocket motor and shortened control actuation Section (SCAS)

AIM - 120C6

Lots 13 - 15

Provides improved fuzing via new quadrant target detection device (QTDD)

AIM - 120C7

Lots 16 -19

AIM - 120D

Lots 20 & up

Weight (lbs.) Length (in.) Diameter (in.) Wing Span Control Fin CG (Nom) Warhead Propulsion Fuze -

Baseline missile, not field reprogrammable Provides electrically erasable programmable read only memory (EEPROM) for software updates via field level reprogramming Introduces clipped wing and fin design for compatibility with F 22A internal carriage

Improved guidance section for improved Electronic Protection (EP) Improved kinematics, improved high off bore-sight (HOBS) capability, GPS, and two way enhanced data-link

358 max 144 7 AIM-120A/B - 21 inches; AIM-120C - 17.5 inches (C/D) AIM-120A/B - 25 inches; AIM-120C - 17.5 inches (C/D) 82.2 inches back from radome tip. 45 lbs. Blast/Fragmentation Boost/Sustain, Reduced Smoke Active radar Target Detection Device (TDD/QTTD)

Carriage Options: Aircraft: F-15 A-E F-16 A-D F/A-18 C-F F-35 F-22A AV-8B Sea Harrier / Harrier II EF2000 EuroFighter Tornado JAS 37 Viggen JAS 39 Gripen

Launcher: LAU-106 (F-15 eject), LAU-128 (F-15 rail) LAU-129 (F-16 rail) LAU-116 (F/A-18 eject), LAU-127 (F/A-18 rail) LAU-147/A (F-35 eject), ARL (F-35 rail) LAU-142/A (F-22)

Ground Launch Systems: NASAMS (FMS) SLAMRAAM (US Army) CLAWS (US Marines)

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Contractor / Status / Improvements / Special Equipment: Contractor Raytheon Missile Systems Company, Tucson AZ Status Inventory/Rate Production for USAF/USN/FMS (120-A/B/C) System Design Development (120D) Special Equipment Common Field-Level Memory Reprogramming Equipment (CFMRE) AN/GYQ-75A (V) (USAF) and (USN) Test Set, Guided Missile Circuitry, TS-4108/G Missile Bit Test Set (MBTS) (USAF) Management/Engineering: OPR Joint USAF/USN Program, USAF Lead Service 328th ARSW (USAF), Eglin AFB, FL NAVAIRSYSCOM PMA-259, (USN) NAS Patuxent River, MD Support Activities 575 CBSS/GBLA, Robins AFB, GA (USAF) NAWCWD - Pt Mugu (USN) Technical Order:

21-AI120A-2 (USAF), NAVAIR 01-120-2 (USN)

Guidance Section (GS)

Armament Section (AS)

Propulsion Section (PS) +5” Motor

AIM-120A/B

AIM-120C (clipped Wing)

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Control Section (CS)

INTENTIONALLY LEFT BLANK

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CHAPTER TWO 1 June 2009

AIR-TO-GROUND MISSILES (AGM)

FOR OFFICIAL USE ONLY

INTENTIONALLY LEFT BLANK

Nomenclature: AGM-65 Series

Name: Maverick

Capability: Close Air Support/Interdiction/Suppress Enemy Air Defense (SEAD) with a lock on before launch day or night capability. Description: Although the Maverick is a modular design weapon, it is delivered to the services as an all-up round (AUR). A different combination of the guidance package and warhead can be attached to the rocket motor section to produce a different weapon. The Maverick has three different seekers and two different warheads. The solid-rocket motor propulsion section is common to all variants. The seeker options are electro-optical (EO) imaging, imaging infrared (IIR) or a laser guidance package. The warhead is in the missile's center-aft section (CAS). Either a 125pound shaped-charge warhead or a 300-pound penetrator warhead can be used. A contact fuze in the base of the warhead fires the shaped-charge. The penetrator uses a delayed-fuze, allowing the warhead to penetrate the target with its kinetic energy before firing. The latter is very effective against large, hard targets. The AGM-65 has a cylindrical body with long-chord delta wings and tail control surfaces mounted close to the trailing edge of the wing of the aircraft using it. Maverick A has an electro-optical television guidance system. After the protective dome cover is automatically removed from the nose of the missile and its video circuitry activated, the scene viewed by the guidance system appears on a cockpit television screen. The pilot selects the target, centers cross hairs on it, locks on, and then launches the missile. Maverick B is similar to the A model, although the television guidance system has a screen magnification capability that enables the pilot to identify and lock on to smaller and more distant targets. Maverick D has an imaging infrared (IIR) guidance system, operated much like that of the A and B models, except that infrared video overcomes the daylight-only, adverse weather limitations of the other system. The infrared Maverick D can track heat generated by a target and provide the pilot a pictorial display of the target during darkness and hazy or inclement weather. Maverick E model is the only version having the laser-guided seeker section. It uses the heavyweight penetrator warhead. This variant is used by the U.S. Marine Corps, Navy, and Air Force against fortified ground installations, armored vehicles, and surface combatants during Close Air Support missions. Used in conjunction with ground or airborne laser designators, the missile seeker searches a sector 7 miles across and over 10 miles ahead. If the missile loses track of the laser spot it flies up and over the target. A safety feature on the missile prevents the warhead from detonating high order. Instead, the warhead duds. Maverick F is a naval variant of the D/G model (IIR) currently in use by the U.S. Navy. It also uses the 300-pound penetrator warhead. Maverick G model essentially has the same guidance system as the D, with some software modifications that track larger targets. The G model's major difference is its heavyweight penetrator warhead, while Maverick B and D models employ the shaped-charge warhead. Maverick H model uses an optical Charged Coupled Device (CCD) guidance system. The CCD system is an upgrade of the old TV system used in the A and B models. The CCD camera provides improved haze penetration, increased target contrast and longer range target identification; and improves the missiles’ ability to maintain centroid track steering when locked onto very small targets. The H model, operated much like the other Maverick variants, contains the shaped charge warhead used on the A, B and D models.

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Maverick K model uses the H’s CCD guidance system and the heavyweight penetrator warhead used on the E and G models. Characteristics: CRD Weapons Code M65AA M65BA M65DA M65EA M65FA M65GB M65GA M65KA SZKCA SZKDA M65HA SZKEA Z65AA

MISSILE AGM-65A MISSILE AGM-65B MISSILE AGM-65D MISSILE AGM-65E MISSILE AGM-65F AGM-65G-2 AGM-65G AGM-65K AGM-65G-2 AGM-65H AGM-65H AUR AGM-65K MISSILE TGM-65A CAPTIVE

Z65DA Z65TD Z65TE Z65GA P65DA P65DB P65GA P65GB SZKAA SZKBA

MISSILE TGM-65D CAPTIVE MISSILE TGM-65D LOAD TRAINER MISSILE TGM-65D MAINT TRAINER MISSILE TGM-65G CAPTIVE PREPO ISO AGM-65/D PREPO ISO AGM-65/D PREPO ISO AGM-65/G PREPO ISO AGM-65/G2 STAMP AGM-65D STAMP AGM-65G

Guidance -

TV (A, B, H, K); IIR (D, F, G2); Laser (E); Charged Coupled Device (CCD) Imaging TV (H, K) Control Tail, Hydraulic Pneumatic Actuators Autopilot - Proportional Navigation Class Anti-Armor / Penetration Missile AGM-65E (LASER) AGM-65 A/B (TV) AGM-65 D (IR) Weight (lbs.) - 628.3 Weight (lbs.) - 462.0 Weight (lbs.) - 484.47 Length (in.) - 97.70 Length (in.) - 97.70 Length (in.) - 97.70 Diameter (in.) - 12.00 Diameter (in.) - 12.00 Diameter (in.) - 12.00 AGM-65 F/G/G2 (IR) Weight (lbs.) - 670 Length (in.) - 97.70 Diameter (in.) - 12.00 Warhead Explosive Fuze Stabilizer Propulsion -

AGM-65 H Weight (lbs.) - 461.0 Length (in.) - 97.70 Diameter (in.) - 12.00

AGM-65 K Weight (lbs.) - 672 Length (in.) - 97.70 Diameter (in.) - 12.00

125 lbs. Shaped Charge Jet and Blast (A, B, D, H) 300 lbs. Penetrator/Blast-Frag (E,F,G,K) 86 lbs Comp B / 80 lbs PBX(AF)-108 SAF (A, B, D,H); FMU-135/B (E, F, G,K) Wings / Control Surfaces Boost Sustain

Carriage Options: Aircraft: A-10 F-15E F-16A-D F/A-18A-F AV-8B P-3C

Launcher: (All Aircraft use same) LAU-88A (3 ea) LAU-117A (1 ea) LAU-117A (1 ea) LAU-117A (1 ea) LAU-117A (1 ea) LAU-117A (1 ea)

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Contractor / Status / Improvements / Special Equipment: Contractor - Raytheon Missile Company Status AGM-65A, B, D, F, G, E, H, K Inventory Special Equipment - AN/DSM-157 Guided Missile Test Set (A, B, D, G, H, K); TTU-519/E Guided Missile Test Set (E, F); AN/DSM-129 Guided Weapon Test Set Target Simulator (A, B, H, K); SM-787/DSM Test Set Target Simulator (D, F, G); SMU-127/E Test Set Target Simulator (E). For a complete list of AGM-65 Guided Missile Ground Equipment, refer to T.O. 35D-1-281. Management/Engineering: 507 CBSS/GBLA, Hill AFB, UT NAVAIRSYSCOM PMA-242, NAS Patuxent River, MD Technical Order: 21M-AGM65A-2 (A & B), 21M-AGM65D-2 (D & G), 21M-AGM65K-2 (H&K&E)

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Nomenclature: AGM-84D

Name: Harpoon

Capability: All-Weather Standoff Anti-Ship Missile. Description: The AGM-84D Harpoon is an all-weather, over-the-horizon, anti-ship missile system effective against moving/stationary surface ships of sizes from patrol boat to capital assets. It offers the capability for low level cruise trajectory and terminal mode sea-skim or pop-up maneuvers. This feature along with active radar guidance and warhead design assure high survivability and effectiveness. The Harpoon missile is designed as an anti-ship cruise missile. It has the capability to cruise just above the surface toward its target, and just before impact, execute a terminal pop-up maneuver to counter close-in defenses and enhance warhead penetration. There are two variants in use today, the AGM-84D Air Harpoon version which is used on F/A-18, and P-3C platforms, and the RGM-84D Surface variant which is carried in canisters aboard DDG 51-78 and CG-47 ships. Characteristics: CRD Weapons Code - ZC61C Guidance INS mid-course, Active Radar Terminal Control Tail Autopilot INS Class Air-to-Ground Missile Weight (lbs.) - 1,160 Length (in.) 151 Diameter (in.) - 13.5 Warhead 500 lbs. Explosive Destex Fuze Contact Propulsion Turbojet Sustainer Engine Carriage Options: Aircraft: F/A-18A-F P-3C

Launcher Rack:

Contractor / Status / Improvements Contractor: Contractor - Boeing, IBM and Raytheon Status Inventory. Decertification (Air Force Only) per AFI 63-104 complete. Management/Engineering: NAVAIRSYSCOM PMA-201, NAS Patuxent River, MD Technical Order: NAVAIR 01-AGM84A-2-1

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Nomenclature: AGM-84K

Name: Standoff Land Attack Missile-Expanded Response (SLAM-ER)

Capability: Adverse-Weather-Day/Night-Land and Sea Precise Air-to-Ground Weapon. Description: The Standoff Land Attack Missile-Expanded Response (SLAM-ER) is a long-range weapon system designed to provide day, night and adverse weather precision strike capability against high value land and sea targets. SLAM-ER is an effective, long-range, network enabled precision strike option for pre-planned and target of opportunity attack missions against both moving and stationary land and ship targets. SLAM-ER has a 500 lb. warhead, an IR sensor system, a datalink and a modified GPS receiver. SLAM-ER employs numerous operating modes which make it effective against a broad range of targets. For fixed targets, SLAM-ER can be launched as either an autonomous fire-and-forget weapon, or as a man-in-the loop (MITL) weapon utilizing the missile advanced datalink which communicates with the launch or control aircraft via the AWW-13 Data Link Pod. Pilots and controllers view live missile seeker IR video to target impact and can abort or redirect after launch if required. SLAM-ER hits targets with JDAM near-precision accuracy utilizing GPS updates alone. With optional target imagery, Automatic Target Acquisition (ATA) enhances autonomous accuracy even more. Characteristics: Propulsion Length (in.) Diameter (in.) Wingspan (ft) Weight (lbs.) Speed Range Guidance System -

Warhead Carriage Options: Aircraft: F/A-18A-F P-3C

Teledyne Turbojet; Thrust is greater than 600 lbs. 172 (4.4 m) 13.5 (34.3 cm) 7.2 (2.2 m). 1,488 (674.5 kg) High Subsonic Over-the-horizon, in excess of 150 nautical miles Ring Laser Gyro Inertial Navigation System (INS) with multi-channel GPS; infrared seeker for terminal guidance with Man-in-the-Loop control data datalink from the controlling aircraft. Upgraded missiles incorporate Automatic Target Acquisition (ATA). 543 lbs.

Launcher/Rack: BRU-32

Contractor / Status / Improvements / Special Equipment: Contractor - Boeing and Raytheon Status Inventory Management/Engineering: NAVAIRSYSCOM PMA-201, NAS Patuxent River, MD

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Technical Order: NAVAIR 01-AGM84A-2-1

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Nomenclature: AGM-86/B

Name: Air Launched Cruise Missile (ALCM)

Capability: Defeat strategic targets from outside enemy defenses. Description: The AGM 86-B ALCM is a long range, autonomous, nuclear capable, stand-off weapon. It has a turbofan engine and inertial guidance system with a terrain-contour matching (TERCOM) update feature. Characteristics: CRD Weapons Code - None Guidance Inertial Navigation Control Operational Flight Program Software Autopilot Analog Autopilot Class Air-to-Ground Missile Weight (lbs.) - 2850 Length (in.) 249 Diameter (in.) - 25 Warhead W80 Fuze Impact Sensors or Commanded Air Burst Propulsion F107-WR-100 Carriage Options: Aircraft: B-52H

Launcher: 30 in. lugs

Contractor / Status / Improvements / Special Equipment: Contractor - Boeing Defense and Space Group Status Inventory (Partial demilitarization of fleet in process) Management/Engineering: 705 MSUS, Tinker AFB, OK Technical Order: Technical Order - 21M-AGM86-2-1

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Nomenclature: AGM-86/C&D

Name: Conventional Air Launched Cruise Missile (CALCM)

Capability: Defeat heavily defended high-value targets from outside theater defenses. Description: The AGM-86C and AGM-86D missiles are collectively referred to as CALCMs. The AGM-86C provides an adverse weather, day/night, air-to-surface, accurate, stand-off outside of theater defenses strike capability. It has a range greater than 500 miles and a 3,000 lb. class blast/fragmentation warhead. The AGM-86D’s AUP-3(M) penetrator warhead provides a cost-effective, stand-off outside theater defenses capability against a wide range of hardened and deeply buried targets. CALCMs are equally effective for stand-alone, clandestine/punitive strikes and fully integrated theater warfare. The AGM-86C and AGM-86D were successfully used in Operation Iraqi Freedom. Characteristics: CRD Weapons Code - None Guidance Inertial Navigation integrated with GPS Control Operational Flight Program Software Autopilot N/A Class Air to Ground Missile Weight (lbs.) - 3,250(C) 3,280(D) Length (in.) 249 Diameter (in.) - 24.5 Warhead 3,000 lb. Class Blast/Fragmentation(C) 1,000 lb. Class Advanced Unitary Penetrator (AUP-3M) (D) Explosive Block 0A (C) - AFX-760, Block 1A (C) - PBXN-111, PBXN-109(D) Fuze FMU-139 A/B (2)(C), FMU-159/B(D) Detonation Impact or Proximity (C), Programmable Burst Point Control (D) Propulsion F107-WR-100 Carriage Options: Aircraft: B-52H

Launcher: 30 in. lugs

Contractor / Status / Schedule / Improvements / Special Equipment: Contractor - Boeing Defense and Space Group Status Inventory (Demilitarization of the AGM-86D is pending official directive) Management/Engineering: 705 MSUS, Tinker AFB, OK Technical Order: 21M-AGM86-2-3(C), 21M-AGM86-2-4 (D)

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Nomenclature: AGM-88B&C

Name: High Speed Anti-Radiation Missile (HARM)

Capability: Suppression of mobile, fixed and re-locatable enemy air defense systems. Description: The AGM-88 HARM is a supersonic air-to-surface missile designed to seek and destroy enemy radar equipped air defense systems. HARM has a proportional guidance system that homes in on enemy radar emissions through a fixed antenna and seeker head in the missile nose. The missile consists of four sections; guidance section, warhead, control section, and rocket motor. Characteristics: CRD Weapons Code Z88AB Z88AD M88AB M88AA

MISSILE AGM-88(HARM) CAPTIVE MISSILE AGM-88(HARM) CAPTIVE MISSILE AGM-88B AUR (HARM) MISSILE AGM-88C AUR

P88AA P88CA SZMAA

PREPO ISO AGM-88/B PREPO ISO AGM-88/C STAMP AGM-88C

Guidance Passive Broadband Radio Frequency Control Wing, Electro-Mechanical Autopilot 3 Axis Rate Gyros Class Air to Ground Missile Weight (lbs.) 780 -810 Length (in.) 164 Diameter (in.) 10 Warhead: WAU-27/B (AGM-88C) WAU-7/B (AGM-88/B) Weight 143.5 lbs. Type Direct Fragmentation, Variable Charge-to-Metal Concept Explosive - PBXN-107 NEW 45.2 lbs. Fuze FMU-111/B Proximity/Contact Control Section WCU-2/B Target Detector - DSU-19A/B Electro-Optical Rocket Motor YSR-113-TC-1, Smokeless, Solid-Propellant, Dual Thrust Carriage Options: Aircraft: F-16C-D F/A-18A-F EA-6B Prowler EA-18G (objective)

Launcher: LAU-118A(V)4/A

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Contractor / Status / Improvements / Special Equipment: Contractor - Raytheon Company Status Inventory Special Equipment - MSU-170A/E and AN/GSM-396 Management/Engineering: 575 CBSS/GBLD, Robins AFB, GA NAVAIRSYSCOM PMA-242, NAS Patuxent River, MD Technical Order: 21M-AGM88C-2 (Missile), 33D9-45-42-1 (Test Set)

AGM-88C

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Nomenclature: AGM-88E

Name: Advanced Anti-Radiation Guided Missile (AARGM)

Capability: Lethal destruction of fixed, re-locatable, or mobile Integrated Air Defense Systems (IADS). Description: The AGM-88E AARGM is an upgrade to the legacy HARM missile. AARGM consists of a newly developed guidance section and a modified AGM-88B HARM control section. AARGM uses the existing AGM-88 HARM rocket motor section, warhead section, wings and fins. The new guidance section is equipped with a more sensitive wideband passive digital Anti-Radiation Homing (ARH) receiver, a conformal antenna array, an active Millimeter Wave (MMW) radar, and an Integrated Broadcast Service Receiver (IBS-R). The ARH in combination with the conformal antenna is able to geolocate emitting targets. The ARH can be used to minimize target location error over time allowing the MMW radar to continue to prosecute and attack even when the target radar shuts down. The IBS-R will provide the pilot access to real time intelligence data enhancing situational awareness. The AGM-88E Control Section incorporates a GPS aided inertial navigation suite (INS) and a Weapons Impact Assessment (WIA) transmitter. The GPS/INS provides AARGM a point-to-point capability and provides for missile avoidance and impact zones. The WIA transmitter provides for Battle Damage Assessment cueing capability. Characteristics: NALC (Navy Ammunition Logistic Code) TBD Guidance Control Weight (lbs.) Warhead-

Fuze Control Section Target Detector Rocket Motor -

Passive Broadband Radio Frequency, GPS, and Active Millimeter Wave Radar Wing, Electro-Mechanical Autopilot - 3 Axis GPS/INS Class - Air-to-Ground Missile 780 -810 Length (in.) - 164 Diameter (in.) - 10 WAU-7/B (AGM-88/B) Weight - 143.5 lbs. Type - Direct Fragmentation, Variable Charge-to-Metal Concept Explosive - PBXN-107 NEW - 45.2 lbs. FMU-111/B Proximity/Contact WCU-30/B DSU-19A/B Electro-Optical YSR-113-TC-1, Smokeless, Solid-Propellant, Dual Thrust

Carriage Options: Aircraft: F/A-18C/D (threshold) EA-6B (objective) F/A-18E/F (objective) EA-18G (objective)

Launcher: LAU-118A(V)4/A

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Contractor / Status / Improvements / Special Equipment: Contractor ATK Mission Systems Status In development Special Equipment - CMBRE Management/Engineering: Program Executive Office Unmanned Aviation and Strike Weapons (PMA-242), NAS Patuxent River, MD Technical Order: TBD

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Nomenclature: AGM-114 Series

Name: Hellfire

Capability: Air-to-Ground missile system designed to defeat individual hard point targets and minimize exposure of the delivery vehicle to enemy fire. Description: The missile is a rocket-propelled, laser guided, supersonic weapon designed to defeat individual hard point targets. It consists of a guidance section housing a semi-active laser seeker, a warhead section containing either a conical shaped charge with a forward precursor warhead (AGM-114K/K2) or a blast-fragmentation/thermobaric warhead (AGM-114M/N), a propulsion (rocket motor) section, and a control section. To expand the Hellfire target set to include softer targets, the Army has added an external fragmenting sleeve to the K-2 variant resulting in the K-2A variant. The USAF delivery platform for the Hellfire is the MQ-1B Predator and MQ-9 Reaper Unmanned Aerial Vehicle. Other delivery platforms include Marine Corps helicopter AH-1W/Z Cobra, the U.S. Army AH-64D Apache Longbow, OH-58D Kiowa Warrior, the AH-6A Little Bird helicopters, as well as the Navy/Army H-60 series helicopters. Hellfire provides precision striking power against tanks, armored personnel carriers, air defense sites, patrol boats, bunkers, buildings, non-tactical vehicles, personnel, and slow-moving fixed and rotary wing aircraft. Characteristics: CRD Weapons Code M14KA AGM-114K, K2 and K-2A M14MA AGM-114M M14PB The Hellfire AGM-114P-2 missile (1410-WH47) differs from the "K" by supporting a digital communication link to the launcher and by the replacement of the attitude gyro. That digital communication link provides targeting data to the missile and enables the missile to inertial-navigate, acquire targets, and hit targets with extremely large lateral offset angles. M14PA The AGM-114P-2A Hellfire (1410-WH48) is identical to the P-2 missile except it has a sleeve around the warhead that increases the fragmentation characteristics. M14PC The AGM-114P-2B Hellfire (1410-WH49) is identical to the P-2A missile except it has a “heavy” sleeve around the warhead that the metallic composition is denser to increase the fragmentation characteristics. M14NA

The AGM-114N Hellfire (1410-WF96), the N missile, has a metal augmented charge (MAC) (thermobaric) blast frag warhead with time delay fuze.

M36E3

Guided Training Missile (M-36) Captive Flight Trainer is used for captive flight training and cannot be launched. It has an operational laser seeker that can search for and lock on to laser energy. For the K Model Guided Training Missile (M-36) Captive Flight Trainer is used for captive flight training and cannot be launched. It has an operational laser seeker that can search for and lock on to laser energy. For the P Model Guided Training Missile (M-34) Maintenance (Ground Handling) Trainer assists with load handling training and aircraft testing.

M36E6

M-34

Guidance - Laser (K, K-2, M, N) - Ka-band millimeter wave (L) Control Tail, Pneumatic Actuation System

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Class -

Anti-Armor/ Anti-Material

UAS Missile Variants: Hellfire-II AGM-114K, K-2, K-2A, (Laser) Platforms supported - Rotary Wing Platforms (Multi-Service), USAF Predator Weight (lbs.) 100.0 Length (in.) 64.0 Diameter (in.) 7.0 Hellfire II (P) AGM-114P-2, P-2A, P-2B, M-6, N-6 Platforms supported: Currently USAF UAS Only Warhead -

19.8 lbs. Dual Shaped Charge (K, K-2, K2A, L) 24 lbs. Blast Fragmentation (M) 27.6 lbs. Thermobaric (N) Explosive - 14.50 lbs. LX-14 (K) 14.50 lbs. PBXN-9 (K-2, L) 5.0 lbs. PBXN-109 (M) 5.0 lbs PBXN-112/4.1 lbs. Pressed Al Powder (N) Fuze Electronic Safe Arm Firing (ESAF) Assembly (K, K-2, L); ESAF and Time Delay Fuze Assembly (TDFA) (M/N) Stabilizer - Strakes, wings and fins Propulsion - Solid fuel propellant minimum smoke, single grain, boost motor Carriage Options: Aircraft: AH-64D Apache Longbow Army/Navy H-60 Series OH-58D Kiowa Warrior AH-6A Little Bird AH-1W/Z Cobra MQ-1B Predator Unmanned Aerial Vehicle (UAV) MQ-9 Reaper UAV

Launcher: M299

Modified M299 Missile Launcher Rail Modified M299 Missile Launcher Rail

Contractor / Status / Improvements / Special Equipment: Contractor Lockheed Martin Status AGM-114B, K, K2 K-2A, M, N Inventory Special Equipment - None; All-Up-Round BIT checked on MQ-1B Predator UAV Management/Engineering: Joint Attack Munition Systems (JAMS) Project Office, Redstone Arsenal, AL 507 CBSS/GBLC, Hill AFB, UT NAVAIRSYSCOM PMA-242, NAS Patuxent River, MD Technical Order: 21-AGM114

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Nomenclature: AGM-129A

Name: Advanced Cruise Missile (ACM)

Capability: Defeat heavily defended high-value targets from outside theater defenses. Description: Embodying stealth technology, the AGM-129A is an air-launched, strategic cruise missile with significant improvements over the AGM-86B in range, accuracy and survivability. Armed with a W-80 warhead, it is designed to evade air and ground-based defenses in order to strike heavily defended hardened targets at any location within an enemy’s territory. Characteristics: CRD Weapons Code - None Guidance Inertial Navigation Control Operational Flight Software Autopilot N/A Weight (lbs.) - 3,600 Length (in.) 250 Warhead W80 Fuze N/A Propulsion F112-WR-100 Turbofan Range 2,000 Nautical Miles Carriage Options: Aircraft: B-52H

Launcher: 30 inch lugs

Contractor / Status / Improvements / Special Equipment: Contractor - (Prime) Raytheon Status Inventory (demilitarization of fleet in process) RAA 1 Oct 1992 Management/Engineering: 498 Missile Sustainment Group (MSUG), Tinker AFB, OK Technical Order: TO - 21-AG129-2-1

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Nomenclature: AGM-130

Name: Powered Standoff Weapon

Capability: Destroy high value, vertical or horizontal fixed targets at enhanced standoff ranges, during adverse weather, day or night. Description: Derived from the GBU-15, it has since been extensively modified to an advanced, precision guided weapon used against high value fixed targets. It features Inertial Navigation System/Global Positioning System (INS/GPS), man-in-the-loop capabilities and has a propulsion section enabling enhanced standoff capability. There are two versions of the weapon: the AGM-130A model utilizes the MK-84 warhead and the AGM-130C model utilizes the BLU-109 penetration warhead. Both versions have advanced control sections and new Switchable Datalinks (SDL) for horizontal target attack profiles. The datalink pod transmits command signals to the weapon receiver/transmitter (RxTx) and receives video signal from the weapon RxTx. The command signal allows the WSO to control and redirect the weapon during delivery to the target. There are two improved guidance sections for day and night extended capability: Television Guided Section (TVGS) and Improved Modular Infrared Sensor (IMIRS). The AN/GJM-64 Test System tests all GBU-15 and AGM-130 configurations; it is completely menu driven featuring minimal manual operator intervention. The software can be readily modified to facilitate testing/updating of new weapon versions, enhancements, improvements and modifications. Characteristics: CRD Weapons Code ZMG5C M309G M309H M306A M306B M304G M304H M30GA M30GB ZMGMB

AGM-130 LC&FTD INRT IMIRS SDL AGM-130 TAC, BLU-109, IMIRS, SDL AGM-130 TAC, BLU-109, TVGS, SDL AGM-130 TAC, INERT, IMIRS, SDL AGM-130 TAC, INERT, TVGS, SDL AGM-130 TAC, MK-84, IMIRS, SDL AGM-130 TAC, MK-84, TVGS, SDL AGM-130 TAC/INRT IMIRS SDL AGM-130 TAC/INRT TVGS SDL AGM-130(I) A-1 DATM DUMMY TRN TV

M304E M304F M309E M309F SZNBA SZNDA ZM45A ZMG5A ZMG5B ZM45B

AGM-130A-11 TAC MK-84 SDL AGM-130A-12 TAC MK-84 IR SDL AGM-130C-11 TAC BLU-109 TV SDL AGM-130C-12 TAC BLU-109 IR SDL STAMP AGM-130A-12 STAMP AGM-130C-12 CATM-130-109 TVGS L/W F-15E CATM-130A-109 TVGS F-15E CATM-130A-110 IMIRS F-15E CATM-130A-110 IMIRS L/W F-15E

Guidance - Autonomous GPS/INS - TVGS or IMIR Seeker - Precise Adverse Weather, day or night - Accurate All Weather - Vertical and Horizontal Targets Control Automatic or manual (WSO with AXQ-14 or ZSW-1 Datalink System) Autopilot - Digital Class 3,000 lb. Standoff Weapon Warhead - MK84 or BLU-109 (adapter kit required) Explosive - Tritonal - 945 lbs. (MK84); 535 lbs. (BLU-109) Fuze - FMU - 124A/B (MK84); FMU-143 (BLU-109) FMU-152 (potential) Stabilizer - Strakes (canards), Wings, and Control Surfaces Propulsion - Solid Propellant Rocket Motor

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Range Weight Length Diameter -

15 to 30+ NM AGM-130A-11 (MK84, TV) 2978 lbs. AGM-130A-12 (MK84, IR) 3001 lbs. AGM-130C-11 (BLU-109, TV) 3064 lbs. AGM-130C-12 (BLU-109, IR) 3087 lbs. 158.8 in. Mk-84 Warhead 18.0 in. BLU-109 Warhead 16.0 in. Rocket Motor 9.0 in. Guidance Section 15.0 in. Control Section 16.0 in. Tail Section (Wings) 59.0 in.

Carriage Options: Aircraft: F-15E

Launcher/Rack: BRU-47 (30 in. Lug Spacing)

Contractor / Status / Improvements / Special Equipment: Contractor - (AGM-130) Boeing Company; (AXQ-14/ZSW-1) Raytheon; (AN/GJM-65) BAE Status Inventory (AGM-130-9/-10 replaced by -11/-12 Apr - 99) Improvements - Potential Integration of FMU-152 (JPF) Fuze & BLU-121 Warhead Special Equipment - AN/GJM-64 Field Test System (33D7-77-81-1), Ground Support Equipment (33D9-148-3-1), and Shipping and Storage Containers (35E20-2-43-2) Mangement/Engineering: 507 CBSS/GBLB, Hill AFB, UT Technical Order: 21M-AGM130-2

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Nomenclature: AGM-154

Name: Joint Stand-Off Weapon (JSOW)

Capability: Autonomous, low observable, standoff outside point defenses, all weather, day/night multiple kills per pass, launch and leave, effective against area and stationary targets and provides a moving maritime interdiction capability. Description: The JSOW is a low observable, 1,000 lb. class, INS/GPS guided, family of air-toground glide weapons. JSOW consists of a common airframe and avionics that provides for a modular payload assembly to attack stationary and moving massed light-armored and armored vehicle columns, surface-to-air targets and personnel. JSOW provides combat forces with an all weather, day/night, multiple kills per pass, launch and leave, and a standoff capability. Characteristics: CRD Weapons Code M541A AGM-154A JSOW SZPBA SZPAA AGM-154A JSOW Z54BA AGM-154A-1 JSOW (FMS Only) Guidance Class Weight (lbs.) Length (in.) Diameter (in.) Warhead Propulsion Range Carriage Options: Aircraft: B-2A F-16C-D F/A-18A+C/D/E/F F-35

AGM-154B JSOW (Navy Only) DATM-154 AGM-154C (Navy Only) AGM-154C (Navy Only) AGM-154A&B (B version Navy Only) INS/GPS AGM-154A-1 (FMS Only) INS/GPS AGM-154C (Navy Only)-INS/GPS w/IIR Seeker AGM-154C-1 (Navy Only) INS/GPS with Link-16 W/IIR Seeker Standoff Outside Point Defense (SOPD) Missile 1,065 max 160 16 x 22; Wings Extended -106 AGM-154A -145 BLU-97 Combined Effects Munitions (CEM) Bomblets AGM-154A-1 (FMS Only) BLU-111 AGM-154B (Navy Only) - 6 BLU-108s (24 Skeets) Note: Production Halted AGM-154C/AGM-154-C-1 (Navy Only) - BROACH Penetrator Warhead None, Glide Weapon (~12:1 glide ratio) 15nm at Low Altitude; >70nm at High Altitude

Launcher/Rack: BRU-57 BRU-32

Contractor / Status / Improvements / Special Equipment: Contractor - Raytheon Status Production complete; Program in sustainment Notes Joint USAF/USN Program (USN lead service) Reference - JMEM Special Equipment - AN/GYQ-79 Common Munition Bit Reprogrammable Equipment (CMBRE)

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Management/Engineering: 507 CBSS/GBLB, Hill AFB, UT OPR - NAVAIRSYSCOM PMA-201, NAS Patuxent River, MD Technical Order: 21-AGM154-2-2

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Nomenclature: AGM-158

Name: Joint Air-to-Surface Stand-Off Missile (JASSM)

Capability: Standoff outside area defense to strike critical, high value, heavily defended targets. Description: JASSM is a precision cruise missile designed for launch from outside area defenses to kill hard, medium-hardened, soft and area type targets. The weapon is capable of attacking both fixed and relocatable targets at ranges beyond enemy air defenses. The AGM-158A-2 contains a Selective Availability Anti-Spoofing Module (SAASM). Initial production (Lot 1) AGM 158A missiles do not contain Selective Availability Anti-Spoofing Module (SAASM). SAASM was incorporated into Lot 2 and beyond and missiles are identified as AGM-158A-2 (a block upgrade). Although distinguished by NSN and marking, missiles are interchangeable and as such, NSNs are linked (Master/Sub) and the Complete Round Code (CRC) is the same for both. AGM-158B, the extended range (ER) variant is being developed. It retains the same outer mold line of the basic missile. Key design differences are additional fuel and different engine which combined provide a significant increase to its operation range. Characteristics: CRD Weapons Code M58HA AGM-158A (JASSM) AGM-158B CRC: TBD Guidance Class Weight (lbs.) Length (in.) Height (in.) Width (in.) Warhead Explosive Propulsion Fuel -

Z58HA

DATM-158A (JASSM)

IIR 2,000 lb. Standoff Missile AGM-158A - 2,150 AGM 158B - 2,350 < 168 <21 (tail closed) <25 (wings closed) Unitary blast frag/penetrator AFX-757 (Insensitive fill) AGM-158A - Teledyne J370 Series Engine AGM-158B - Williams F107-WR-105 Series Engine AGM-158A - approx 40 gallon JP-10 AGM 158B - approx 47 gal JP-10

Carriage Options: Aircraft: B-1B B-2A B-52H F-16 Block 40/50 Objective: F-15E F-35

Launcher: 30 in. lugs (no lanyard) BRU-56 (AGM-158A/A-2/B) BRU-44 (only AGM-158A/A-2) MAU-12 (only AGM-158A/A-2) MAU-12 (only AGM-158A/A-2) BRU-57 TBD

(only AGM-158A/A-2)

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Contractor / Status / Improvements /Special Equipment: Contractor Lockheed Martin Status Full Rate Production, IOC: F-16, B-1B, B-2A, B-52H Improvements The extended range variant, AGM-158B, JASSM-ER, is being developed. Special Equipment - JASSM Weapon Load Adapter – NSN 1450-01-502-3256DM for Bomber units only, and JASSM adapter (trailer chock) – NSN 1730-01-511-2907 optional trailer accessory for bomber units. Allow JASSM container to sit on/be transported on MHU- 110 rail assembly (or new aluminum rail system) which allows weapon loaders to extend JASSM off side of trailer to gain access to bottom of container for loading (eliminates any double handling on flight line). Management/Engineering: 308th ARSG, Eglin AFB, FL Reference - JASSM Program Office System Support Office: 507 CBSS/GBLC, Hill Air Force Base Technical Order: Maintenance 21-AG158A-2

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CHAPTER THREE 1 June 2009

DIRECTED ENERGY (DE) TECHNOLOGIES

FOR OFFICIAL USE ONLY

INTENTIONALLY LEFT BLANK

Nomenclature: TBD

Name: Active Denial System (ADS)

Capability: Counter-personnel with non-lethal tactical directed energy. Description: The Active Denial System (ADS) uses millimeter-wave electromagnetic energy to stop, deter and turn back an advancing adversary from a relatively long range. The specific range is classified, but the current ADS hardware can engage a single individual at a distance that outranges small arms fire. The Active Denial System uses a transmitter to send a narrow beam of 95 GHz electromagnetic energy towards an identified subject. Traveling at the speed of light, the energy reaches the subject and is absorbed in a very thin layer of tissue less than 1/64 of an inch deep. The absorbed energy quickly heats up water molecules in this thin layer of tissue, causing the body‟s nerve endings to signal an intense burning sensation. An individual feels this burning sensation until the transmitter is shut off or when the individual moves out of the beam. A 2-second burst from the system can heat a thin layer under the skin to a temperature of 130° F. On being engaged with the ADS beam, the pain reflex makes an individual pull away automatically in less than a second. However, because only a very thin layer of tissue is being heated, the total energy needed per unit area is actually small substantially less than the threshold for causing permanent injury. An individual would have to stay in the beam for more than an order of magnitude longer before it caused a burn to the skin. Applications include: - Disperse a crowd - Direct/contain/stop a crowd - Separate belligerents/isolate individuals - Distract an individual or group - Render an individual incapable of performing an activity - Deny an area to personnel - Separate combatants/non-combatants in open area - Control access/exit to a facility or structure - Clear an open area - Deter/warn away attackers/intruders - Stop/delay/disrupt attackers/intruders including those inside moving vehicles/boats Characteristics: Currently there are three sets of ADS hardware: (1) System 0 is a 100 kW system that is a fixed site, AC-powered system; (2) System 1 is a mobile 100 kW self-contained system, mounted on a hybrid electric High Mobility Multipurpose Wheeled Vehicle (HMMWV) chassis; and (3) System 2 is a ruggedized, transportable (on HEMTT or similar trucks), self-contained system built into 463L compatible containers. This hardware was developed and extensively field tested under the ADS Advanced Concept Technology Demonstration (ACTD), which was successfully completed in FY07. General characteristics include: - Frequency: 95 GHz - Operation: Capable of continuous operation; nominal engagements are typically less than 5 seconds in duration. Given duty limits, magazine depth is constrained only by vehicle fuel capacity. - Aperture size: ~2 meters - Range: Classified; out-ranges small arms fire

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- Target identification and designation: Visible and IR optical sensors, bore sighted, on the center of the 95 GHz beam. Operator executes aiming and firing. Capable of engaging single individuals and small groups at range without affecting other nearby personnel. Carriage Options: Hybrid-HMMWV chassis: System 1 is currently at Kirtland AFB under AFRL/RDHA operations and continues to do training, assessment, demonstration, and research activities. 463L Pallet compatible containers: System 2 (transportable on HEMTT-type platforms) completed government evaluation (including successful C130 loading/transport test) and was delivered to the government in late FY08. It is currently awaiting deployment decisions. The services are interested in integrating the ADS technology on to a Mine Resistant-Ambush Protected (MRAP) vehicle. System concepts are also being considered for airborne applications. Within AFRL, component technology development is underway to enable a 2.5 MW airborne Active Denial System, intended to provide substantially greater range in a gunship-type application. A demonstration of integrated technologies for this application, on a ground-based test stand, is planned for FY15. Technology alternatives are also being evaluated to reduce the weight of the current 100 kW system by 50%, with the goal to enable more modular configurations and possibly rotary wing aircraft (unfunded). Contractor / Status: Contractor - Multiple Status Successfully completed ACTD with residual hardware/capability; Bridge Program out of AAC working FY12 POM and other preparations, AFRL technology for longer-range and lighter weight systems is in or just entering development. Management/Engineering: AAC/808 ARSG, Eglin AFB, FL AFRL/RD, Kirtland AFB, NM Technical Order: TBD

ADS ACTD Hardware System Concept

ADS System 2 MRAP Active Denial System

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Nomenclature: TBD

Name: Advanced Tactical Laser (ATL)

Capability: Airborne precision engagement of tactical ground targets. Description: The Advanced Tactical Laser (ATL) is a high energy laser system, based on a Chemical Oxygen-Iodine Laser (COIL) device, installed in a NC-130H aircraft. The ATL effort began as an Advanced Concept Technology Demonstration (ACTD) that was concluded 30 September 2008. The ATL effort was transitioned to the Air Force and is being managed by the Air Armament Center (AAC) as an Extended User Evaluation (EUE). The objective of the EUE is to demonstrate the military utility of an airborne tactical laser weapon against ground targets. The ATL will provide enhanced capabilities by increasing targeting precision, decreasing collateral damage, and reducing reconstitution costs. It will also serve as a springboard for future directed energy technology development. The large aperture (50 cm), stabilized beam control system and sensors will be capable of high-resolution imagery of the target area, providing an unprecedented capability for long-range situational awareness. During the EUE, ATL testing will concentrate on exercising and understanding system performance as a function of engagement range, altitude, bearing to the target, and atmospheric/weather conditions. This testing will also evaluate the ISR capabilities of the ATL optical system and help develop contingency operations (CONOPS)/Tactics Techniques and Procedures (TTP) for airborne tactical laser weapons. Characteristics: The current ATL ACTD system has the following general characteristics: - Laser power: Classified - Aperture diameter: 50 cm, in a retractable turret on the bottom of the aircraft - Wavelength: 1.315 µm - Residual beam jitter on target: less than 5 micro-radians - Overall system weight: approximately 40,000 lbs. (C-130 payload) - Nominal laser shot duration: 6 seconds - Total lase time available: approximately 36 seconds, sufficient for 6 nominal laser shots - Recycle time between laser shots: approximately 4 minutes - Target recognition and aimpoint designation/maintenance: operator executed, using a stabilized, high-resolution target image in real time, provided by precision optical line-of-sight stabilization, high-bandwidth target tracking, and high-resolution optical sensors in visible and MWIR wavelength bands. Carriage Options: NC-130 aircraft. A goal of on-going and planned technology development and demonstration programs (see above) is to both improve laser system performance and to significantly reduce overall system weight, to enable a tactical laser weapon system for a next-generation gunship application, at a size/weight which allows the necessary gunship sensors, communications, and combat equipment plus still allows room for additional weapons besides the laser system.

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Contractor / Status: Contractor - Prime contractor for the ATL EUE is The Boeing Company Status - (as of March 2009) - Weapon system has been integrated and flight tested in nonlasing mode. The initial air-to-ground high power target engagements are planned for June 2009. Technology development under AFRL, DARPA, and other service‟s investment is planned to provide technology which can support spiral development of the ATL laser system (if funding is available). Efforts are underway to improve COIL device and beam control technology in order to increase COIL device power, increase magazine depth, reduce the time between laser shots, allow re-generation of spent laser fuels after a mission, and increase laser spot intensity on target (which allows an increase in lethal range). In the longer term, the development and scaling of several electric laser concepts, along with the development of prime power and thermal management technologies, should enable the upgrade to the ATL to install a higherpower electric laser. Along with the integration of advanced beam control technologies, this should increase the ATL lethal range, greatly increase the number of laser shots possible per mission, and reduce logistics requirements. Finally, the performance and scalability of nextgeneration electric laser and tactical beam control technology is planned to be demonstrated in integrated ground testing, enabling further improvements in tactical laser system performance and a significant reduction (greater than a factor of 2) in laser weapon system size and weight. Management/Engineering: ATL ACTD Manager: USSOCOM, MacDill AFB, FL ATL EUE Manager: AAC/308 ARSW, Eglin AFB, FL Advanced Technology Development: AFRL/RD, Kirtland AFB, NM Technical Order: TBD

Advanced Tactical Laser

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Nomenclature: YAL-1A

Name: Airborne Laser (ABL)

Capability: Kill ballistic missiles (BM) during boost phase and provide early BM launch warning. Description: The ABL weapon system consists of a megawatt-class high-energy, chemical oxygen iodine laser (COIL) mounted on a modified 747-400F (freighter) aircraft to detect, track and destroy theater ballistic missiles in their boost phase of flight. ABL also can pass information on launch sites, target tracks and predicted impact points to other layers of the global ballistic missile defense system. A crew of four, including pilot and copilot, would be required to operate the airborne laser, which would patrol in pairs at high altitude, about 40,000 feet, flying in orbits over friendly territory, scanning the horizon for the plumes of rising missiles. Capable of autonomous operation, the ABL would acquire and track missiles in the boost phase of flight, illuminating the missile with a tracking laser beam while computers measure the distance and calculate its course and direction. After acquiring and locking onto the target, a second laser - with weapons-class strength - would fire a three- to five-second burst from a turret located in the 747's nose, destroying the missiles over the launch area. The Boeing Company provides the aircraft, battle management and overall systems integration and testing. Northrop Grumman supplies the high-energy laser, and Lockheed Martin provides the beam control/fire control system. Characteristics: Carriage Options: Aircraft: 747-400F (YAL-1A) Contractor / Status / Improvements / Special Equipment: The Boeing Company Lockheed Martin Northrop Grumman Management/Engineering: MDA/AL, Kirtland AFB, NM Technical Order: TBP

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Nomenclature: TBD

Name: Counter-electronics HPM Advanced Missile Project (CHAMP)

Capability: Defeat electronic systems with non-lethal tactical directed energy weapon. Description: The joint Combatant Commands are facing increased limitations in creating effects on the adversary due to the desire to reduce casualties, preserve historic, religious, and health care facilities, and limit escalation. This has created a growing list of theater no-strike facilities, which can shelter an adversary‟s war making systems. With the increased use of electronic command, control, communications, and computers (C4) to provide battlespace awareness, and command force movements, an adversary may become more vulnerable to non-kinetic techniques to degrade, disrupt or destroy their warfighting systems. The Joint Combatant Commands require a non-kinetic option to engage these systems. The Counter-electronics High Power Microwave Advanced Missile Project (CHAMP) Joint Capability Technology Demonstration (JCTD) will provide a multi-shot and multi-target HPM missile system to negate electronic systems that play a key role in present day and future conflicts. The CHAMP JCTD will integrate, demonstrate, and assess an HPM multi-shot and multi-target cruise missile to degrade, damage, or destroy electronic systems. For this JCTD, a compact HPM payload will be integrated into an appropriate cruise missile to create the HPM cruise missile demonstrator. Five cruise missiles will be produced. One appropriately instrumented cruise missile without the HPM payload will be developed for a flight test to demonstrate delivery, controllability, and fuzing. The remaining four cruise missiles with the integrated HPM payload will be developed for flight testing, demonstration, and HPM effects tests. Of these four HPM cruise missiles, one will be used for HPM effects test on the ground, two shall be used for flight tests, and the remaining one shall be used as a back-up for the flight test. The ground test vehicle will be used to address target effectiveness and collateral damage to surrounding buildings by characterizing key sensitivities such as (target distance, attack geometry, target construction, physical/functional layout, etc). The ground testing could also provide key, cost effective data against targets not demonstrated in the flight tests. The CHAMP JCTD will consist of two Operational Utility Assessments (OUAs). The first OUA will demonstrate: 1) the ability to accurately navigate to a target building; and 2) illuminate the building to ensure effects on the internal electronic components at a distance from the target to be a viable military option. The second OUA will demonstrate the ability to attack multiple targets by illuminating two target buildings geographically separated in addition to demonstrating the same abilities as in the first OUA. Characteristics: The HPM cruise missile will have the following general characteristics: - Frequency: 1.3 GHz - Operation: Capable of multi-shots and multi-targets. Magazine depth is constrained only by cruise missile fuel capacity. - Effective range: Classified Carriage Options: Aircraft: B-52H

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Contractor / Status: Contractor - TBD Status - The CHAMP Broad Agency Announcement (BAA) will be awarded April 09 timeframe. Management/Engineering: Technical Manager: AFRL/RDH, Kirtland AFB, NM Operational Manager: PACOM, Camp Smith, HI Transition Manager: ACC/A8D, Langley AFB, VA Technical Order: TBD

NOTIONAL

CHAMP Concept of Employment

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Nomenclature: TBD

Name: DE Airbase/Area Protection

Capability: Provides protection from all aerial threats to an airbase or perimeter from rockets, artillery and missiles (RAM), Man-Portable Air Defense Systems (MANPADS), Unmanned Aerial Vehicles (UAVs), and cruise missiles. Description: MANPADS have become a significant threat to military and civilian aircraft. Illicit trade of MANPADS and their use by non-state organizations is well documented. Because of predictable flight paths, slow speed, and high Infrared (IR) signatures, large aircraft are particularly at risk during landing and takeoff. Encounters with MANPADS threats since 2000 have demonstrated the need to protect large body aircraft, rotor wing aircraft, and fighter aircraft. The validated threat in the US, at Tinker AFB, clearly highlights the need to address this growing problem. Examples of MANPADS threats include the FIM-92 Stinger, SA-7 Strella, SA-14, SA-16, Blowpipes, and SA-18. The Department of Defense (DOD) has made progress in addressing the MANPADS threat by employing on board defensive systems. The Department of Homeland Security (DHS) is addressing the issue by investigating the use of current systems employed by DOD. However, these systems cannot defend against all threats. Given current fiscal and technological limitations it is unfeasible to equip all military and civilian aircraft with on board counter-MANPADS protection systems. RAM has continued to be a constant threat to our deployed forces. Additionally, UAVs have recently become a significant threat identifying our soldier‟s positions and movements and eventually being armed and attacking those positions. To defend against these threats the DOD community is evaluating the feasibility of developing a ground-based airbase and area Protection capability. The ground-based Airbase Protection System using a directed energy (DE) defeat mechanism would defeat the more robust threats and protect our forces and aircraft from these threats. The ground-based Airbase Protection system consists of three interconnected elements: integrated threat detect, declare and track system, a command and control system (C2), and the DE defeat mechanism. Currently USAF has decided to use a high-energy laser (HEL) for the DE kill mechanism. Characteristics: 2008 tests at Tonopah Test Range against MANPADS and China Lake at a Black Dart V against numerous UAVs showed that we can detect, track and hold a low-powered laser on these threats. In 2009 plans are to integrate a HEL capable of defeating the softer UAVs and Black Dart VI. Progress will be updated as greater laser power capability matures. Carriage Options: None, this is a ground-based defense system inside the perimeter of the airbase or area of regard. Contractor / Status: Numerous contractors have been working this capability and will provide names once a more mature system goes into testing and demonstration. Management/Engineering: AFRL/RD, Kirtland AFB, NM AAC/XR, Eglin AFB, FL

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Nomenclature: TBD

Name: Tactical Relay Mirror System

Capability: Precision engagement of tactical targets. Description: Fundamentally, a relay mirror system is a precision optical system with a receive telescope and a transmit telescope, integrated with an intervening beam control system. The relay mirror system accepts a high energy laser beam from a distant laser source and then re-directs the beam, along a different line of sight, to an intended target. The Tactical Relay Mirror System concept deploys a relay mirror system suspended from a moderate-altitude aerostat. The laser source is a ground-based high energy laser system. A Tactical Airborne Relay Mirror System can be used in a variety of missions, from 24/7 ISR to attacking time-critical targets. The relay effectively puts the High Energy Laser (HEL) source at the location of the relay, increasing the laser‟s field of regard, and allowing the high-value HEL source to be located where it is safer from attack and more easily maintained and re-supplied. With a cooperative laser beacon onboard the relay platform, high performance adaptive optics can be used on the uplink to the relay, maximizing the relay throughput. Thus, a tactical airborne relay extends the range, field of regard, and target set of ground, sea-based, or airborne HEL sources. Relays also enhance the self-defense capabilities of HEL sources, from airborne attack, by providing alternate engagement geometries for the beam and thus enabling high aspect-angle (“crossing-shot”) engagements with the airborne threats. A relay can reduce the HEL beam propagation distance through turbulent, high-density air, such as in maritime environments, and allow high performance adaptive optics to be used on the uplink to the relay. The large transmit aperture can provide high resolution, persistent ISR, while an onboard low power laser can be used for active remote sensing, to identify targets through obscurants and camouflage, and to detect hostile Electro-Optic (EO) targeting systems. A pulsed laser onboard the relay can be used to form a laser “fence” to detect low observable air vehicles, such as low-flying cruise missiles, from their wake or hard body returns. Validated hostile EO systems, cruise missiles, or ground targets could be attacked at optimal times by relaying a HEL beam, damaging or destroying the target, or holding it (ground targets) in place until conventional munitions can be employed. Using a relay can also reduce the impact of clouds on HEL weapon access to a target since the relay (and possibly the source, if it is mobile) can be positioned to avoid transmission through them. The laser weapon system could also provide significant capability for long-range target identification in addition to laser tracking and designation for smart weapons delivery. Potential targets/applications include the following - Ballistic targets: Destroy rockets, artillery, and mortars - Airborne targets: Destroy cruise missiles, UAVs, helicopters, MANPADS - Ground fixed or mobile targets: Destroy, degrade, or delay ground targets, including movers.

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Characteristics: The Tactical Relay Mirror System currently under development is planned with the following characteristics: - Platform altitude: 2,500 to 15,000 feet - Aperture: 30 cm - Relay platform weight: 2,000 lbs. - Laser beam pointing accuracy: 3 microradians - Adaptive optics: uplink only - Laser source power level: up to 60 kW - Range: up to 20 km (target and laser source dependent) - Time on station: up to 2 weeks Carriage Options: Moderate-altitude aerostat; UAV Contractor / Status: Contractor - The Tactical Relay Mirror System is currently under development through a contract with The Boeing Company. Status - Important milestones are integrating laboratory testing in FY09 and low-power integrated field testing in FY10. If a suitable high-power laser source is available, high-power field testing and lethality demonstrations could be conducted in FY11. A concept for mid-term tactical relay mirror spiral development would reduce the weight of the relay mirror payload so that it could be integrated on a UAV, such as the MQ-9 Reaper. This would increase the employment flexibility and capability because the relay mirror system could be easily moved to an advantageous position for engagement in a selected target area. Management/Engineering: AAC/XR, Eglin AFB, FL AFRL/RD, Kirtland AFB, NM Technical Order: TBD

Tactical Relay Mirror System Concept

Concept for a UAV-based Tactical Relay Mirror System

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Nomenclature: TBD

Name: MAX POWER

Capability: Mobile Counter-IED Prototype. Description: MAX POWER is a counter improvised explosive device (IED) prototype using high power microwaves to neutralize various IEDs. The prototype is integrated onto a palletized loading system (PLS) and is capable of carrying out its mission while traveling at speeds of up to 50 MPH. The prototype requires two personnel to operate; a driver for the PLS and the operator of the high power microwave source. Applications include: - Convoy Protection Mission - Route Clearance Mission - Personnel and Vehicle Checkpoint Screening Characteristics: General characteristics include: - Operation: The operator holds down the fire trigger to have the system repeatedly fire; the repetition rate is based upon the speed of the vehicle. - Range: Classified; safe from blast and frag - Target identification and designation: Visible and IR camera slaved to the bore sight of the antenna. Carriage Options: Currently this technology has only been integrated onto a PLS platform. Contractor / Status: Contractor - SAIC (Prime) Status Currently finishing integration of the prototype and will begin testing for the Army Test and Evaluation Command to determine future military utility. Management/Engineering: AFRL/RD, Kirtland AFB, NM Technical Order: TBD

MAX POWER Operational Prototype

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Nomenclature: MX-20DLI

Name: Standoff Intelligence Detection (SID)

Capability: Short-Wave Infrared (SWIR) laser-imager for nighttime high-resolution imaging. Description: The Standoff Intelligence Detection (SID) program has produced a Short-Wave Infrared (SWIR) laser-imager for nighttime high-resolution imaging. This technology has been incorporated into an L-3 Wescam MX-20 IR/EO turret ball, now known as the MX-20DLI (Designator/Laser Imager). This technology is described as Flash Laser Detection and Ranging (LADAR) that uses a short-pulse laser to flash-light a scene to produce a short-exposure controlledillumination intensity image. These images are photographic-like and are displayed as real-time video. The MX-20DLI contains a Military Specification (MILSPEC) Northrop Grumman laser and Intevac Complementary metal–oxide–semiconductor (CMOS) sensor. The wavelength chosen for imaging is “eye-safe” and cannot be seen by any other military sensor such as Forward Looking Infrared Radar (FLIR) or Night Vision Goggles (NVGs). In addition, the laser can be used to designate a target while the sensor images the scene. The SWIR laser-imager is meant to enhance nighttime imaging and complement the passive FLIR sensor with additional intelligence gathering capability. Applications for this technology include: - Intelligence, Surveillance, and Reconnaissance (ISR) - Counter-Improvised Explosive Device (C-IED) - Positive Identification (PID) - Reconnaissance, Intelligence, Surveillance, Target Acquisition (RISTA) - Detect, Classify, and Positively Identify - Laser designation Characteristics: The current MX-20DLI prototype was designed for installation into a DHC-6 DeHavilland Twin Otter with a crew of three: turret operator, SWIR operator, and mission lead/communications officer. This prototype has been successfully flight tested in 2006 and 2007 resulting in over 100 flight hours. - Sensor Suite: Simultaneous 4-Field of View (FOV) FLIR, 4-FOV SWIR Laser-Imager, and Wide-FOV Color TV - Operational Ranges: 10 km laser imaging, 15 km passive imaging, and 10 nm laser designation - INTEL Image Quality: National Imagery Interpretability Rating Scale (NIIRS) 5-8 depending on wavelength and range

MX-20DLI Turret

MX-20DLI mounted onto DHC-6 DeHavilland Twin Otter

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Carriage Options: This system was incorporated into a MILSPEC MX-20 so that it could be easily integrated into a myriad of platforms. The MX-20DLI prototype was designed to operate in a DHC-6 DeHavilland Twin Otter. There are currently over 250 MX-20s in the DOD inventory on the following platforms: C-130 and P-3C. In addition, the Army has funded AFRL/DES to purchase two MX-20DLIs to upgrade their Persistent Threat Detection Systems (PTDS) that are deployed to Operation Iraqi Freedom (OIF) and Operation Enduring Freedom OEF. The PTDS consists of a tethered aerostat with multiple payloads to provide persistent ISR for base defense. For additional customer base, SID is developing the same capability into an MX-15, which is a smaller version of the MX-20 that can be fitted onto many more platforms. The DOD inventory includes more than 600 MX-15s installed on the C-130, MQ-1BPredator, P-3C, and C-12 and is capable of fitting onto just about any rotary-wing. Contractor / Status: Contractor - Textron Systems Status Successfully completed MX-20DLI prototype flight tests in 2006 and 2007, verified to a Technology Readiness Level (TRL) 6 by the US Army. Management/Engineering: AFRL/RD, Kirtland AFB, NM Technical Order: TBD

Persistent Threat Detection System with MX-20 payload deployed to OIF.

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Nomenclature: Laser Dazzler

Name: Personnel Halting and Stimulation Response (PHaSR)

Capability: Hand-held laser dazzler for non-lethal engagements to repel/disrupt aggressive behaviors Description: The Personnel Halting and Stimulation Response (PHaSR) defends against ground-based threats. It is capable of fielded deployment for non-lethal force protection, crowd control, and access denial at a far greater range than small arms fire and current less-than-lethal options. The PHaSR uses a laser device to both dazzle and/or cause an effect severe enough to disrupt hostile actions. The PHaSR system is the first man-portable laser weapon of its kind. High-efficiency non-lethal semiconductor and fiber lasers and innovative thermal management technology are keys to this advanced non-lethal weapon. All materials used in the development and fabrication of the device are commercial off-the-shelf (COTS) items, significantly reducing overall cost. Characteristics: Platform Self-contained, lightweight, ruggedized casing attaches to rifle scope rail Laser range - Beyond small arms range Laser power - Classified Weight Head 8.3 lbs.; Backpack 30 lbs. Technology Readiness Level 6 (TRL-6) Carriage Options: Man-portable backpack Contractor / Status: Contractor Status - Funding by Joint Non-Lethal Weapons Directorate and National Institute of Justice - Conducting human effects testing by AFLR Human Effects Directorate - Integrating range finder into system for laser power safety - Performing legal review - Upgrading technology Management/Engineering: Technology development: AFRL/RD, Kirtland AFB, NM Technical Order: TBD

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Nomenclature: Laser Dazzler

Name: Aircraft Countermeasures (ACCM)

Capability: Provide a non-lethal option for engaging potential threats within restrictive rules of engagement (ROEs) that increase risk to U.S. rescue forces Description: The Aircraft Countermeasures (ACCM) system reduces the amount of small arms fire received by helicopter crews on Combat Search and Rescue (CSAR) missions. The goal is to close the “weapons engagement zone gap” by disrupting the adversary‟s kill-chain prior to hostile actions. The ACCM uses ocular obstruction of enemy combatants approaching CSAR aircraft. A laser light disorients and disrupts the aim of ground adversaries firing small arms at an aircraft. This technology is commonly referred to as a “dazzler.” A nonlethal, coaxial laser works in conjunction with helicopter gunnery. The aircrew gunner can switch between lethal and nonlethal options within seconds. Characteristics: Power box supplies laser light to two gun mounted lenses through fiber optic cables Power Box Size - 1„x 1„x 5" Weight: ~ 30 lbs. Effective Range - 50m -1km Target Range - 300m (This is nominal design range but there are measured effects from 50m-1km) Carriage Options: Compact packaging for mobility on ground or airborne platforms using semiconductor laser technology Contractor / Status: Contractor Status - Completed vibration testing - Completed human effects testing - Technology upgrades include automatic detection of threats through optical augmentation Management/Engineering: Technology development: AFRL/RD, Kirtland AFB, NM Technical Order: TBD

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Nomenclature: TBD

Name: Advanced Tactical DE System (ATADS)

Capability: Aircraft self-protection laser system. Description: The Advanced Tactical DE System (ATADS) is a low cost, compact, robust, continuous wave multi-band semiconductor laser source for jamming infrared missiles. The three band source is completely self-contained in a 13” diameter by 2” high package that fits directly in the Large Aircraft Infrared Countermeasure (IRCM) system. Next generation builds are fiber coupled to allow flexibility in location and in configuration for podded systems. This design will make the ATADS ideal for a variety of platforms. Characteristics: Core laser attributes include: - Versatility of wavelength - High average power source - Good quality of beam - Continuous wave and pulsed operation - Highly compact - Mass producible - Robust technology Carriage Options: Retrofit into existing IRCM systems Contractor / Status: Contractor Status - In development via a Cooperative Research and Development Agreement (CRADA) Management/Engineering: Aculight Corp, The Boeing Company AFRL/RD, Kirtland AFB, NM Technical Order: TBD

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Nomenclature: TBD

Name: Imaging Seeker Countermeasures

Capability: Aircraft self-protection laser system Description: Next generation threats to aircraft will be based on imaging seekers that cannot be jammed with conventional infrared countermeasure techniques. A pulsed solid-state laser to damage the seeker missiles‟ focal plane array is the science behind the Imaging Seeker Countermeasure system. The laser source is in-band to the seeker optics to take advantage of the optical gain ensuring that sufficient energy is delivered to damage the focal plane array causing the seeker to lose track of the aircraft. Characteristics: Core laser attributes include: - In-band wavelengths - High peak power - Good quality of beam - Pulsed operation Carriage Options: Integrated into next generation IRCM systems for jamming and damage capability Contractor / Status: Contractor Status - Laser effects testing and modeling and simulation to optimize source parameters Management/Engineering: AFRL/RD, Kirtland AFB, NM Technical Order: TBD

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Nomenclature: TBD

Name: Proactive Infrared Countermeasures

Capability: Aircraft self-protection laser system Description: The Combat Missions Infrared Countermeasure (CMIRCM) system will provide proactive countermeasures to defeat missiles as early in the kill chain as possible. System will demonstrate end-to-end IRCM concept in a relevant operational environment including: proactive EO/IR sensor/seeker detection and discrimination; threat handoff to countermeasure system from both proactive detector and missile warning sensor; active track and closed loop interrogation to identify threat type; threat location in three dimensions; threat engagement with layered countermeasures; threat location and ID handoff to targeting system for prosecution by weapon system. System will be designed for compatibility with fighter/attack platforms executing operational maneuvers and scenarios. Characteristics: Focus on cost, performance, reliability Low size, weight and power requirement High reliability, modular, open architecture Threat adaptive jammer - CLIRCM techniques and power to defeat MANPADS, AAM, Imaging Seekers Upgrade path to “PROACTIVE IRCM” threat detection Carriage Options: Designed against fighter/attack requirements Can support Mobility and SOF Aircraft Contractor / Status: Contractor Status - Commissioned ATD with ACC Management/Engineering: AFRL/RY, Wright Patterson AFB Technical Order: TBD

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CHAPTER FOUR 1 June 2009

UNGUIDED MUNITIONS, BOMBS and PENETRATORS

FOR OFFICIAL USE ONLY

INTENTIONALLY LEFT BLANK

Nomenclature: BDU-33D/B

Name: 25 lb. Practice Bomb

Capability: Training ordnance to simulate the 500 lb. MK 82 and 2000 lb. MK 84 general purpose, nonguided bombs in a low drag configuration. Description: The BDU-33 is a tear dropped shaped practice bomb that simulates a MK 82 low drag configuration. It utilizes a spotting charge to display target marking. When the bomb is released from the aircraft it free falls until impact. Upon impact the bomb drives a firing pin assembly against a primer activating the signal charge. The resulting flash and puff of smoke permits visual evaluation of accuracy. The Navy’s bomb configuration with similar function is the MK 76; however, this bomb has different dimensions than the BDU-33. Characteristics: CRD Weapons Code ZP61A ZP61B

BDU 33 D/B W/MK4 BDU 33D/B CXU3/B

Guidance Class Weight (lbs.) Length (in.) Diameter (in.) -

ZP61C ZP61D

BDU 33D/B W/LUGS/MK 4 SPOT BDU33/W LUG/CXU3/B

Ballistic 25 lb. Practice Bomb 25 22.90 4.00

Carriage Options: Aircraft: A-10 B-1B F-15 F-16 AV-8B F/A-18A-D

Launcher/Rack: TER-9 / SUU

Contractor / Schedule / Improvements / Special Equipment: Contractor - Del Fasco Status Full Rate Production Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A3-3-7 (Bomb); 11A4-4-7 (CXU-3A/B)

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Nomenclature: BDU-38

Name: Practice Bomb

Capability: Ordnance to train aircrews on delivery by providing a practice shape of the parent weapon system. Description: The BDU-38 consists of a nose section, center section, and aft section. The nose section is a cylinder of sand-cast iron tapered to a point at the forward end. The center section is a cylinder rolled and welded aluminum with a cast iron ballast. Suspension lugs are attached to this section. The aft section consists of the aft section, rear extension, and parachute assembly. The BDU-38 is used to provide a practice shape like the parent weapon system to train air crews on delivery. Characteristics: CRD Weapons Code Z38AA

PRACTICE BOMB BDU-38 (RETARDED)

Guidance Class Weight (lbs.) Length (in.) Diameter (in.) -

Z38AB

PRACTICE BOMB BDU-38 (SLICK)

Ballistic Practice Bomb 715 +/- 15 141.642 13.30

Carriage Options: Aircraft: B-2A B-52H F-15E F-16A-D

Launcher/Rack:

Contractor / Schedule / Improvements / Special Equipment: Contractor Status Inventory Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A3-8-7

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Nomenclature: BDU-45

Name: Practice Bomb

Capability: Navy training bomb that simulates a variety of 500 lb. service bomb configurations that can be used in day and night exercises. It uses a signal cartridge to mark the point of impact. Description: The BDU-45 has a slender body made of steel. It has a case 61.38 inches long with a diameter of 10.75 inches. It has a well in the nose section for a nose fuze and a well in the aft section for a tail fuze. There are three wells centrally located on the top of the body, two (14 inches apart) for the suspension lugs, and one for the charging receptacle in the middle of the MK 122 arming safety switch. The aft portion of the bomb has two receptacles on the side located 180 degrees apart for installation of two signal cartridges. It is filled with an inert material and is compatible with proximity, mechanical and electrical fuzing. A B-groove around the aft end of the bomb body is provided for assembly of either a conical or retarding fin or a laser guidance airfoil group. The bomb is blue with stenciling on it for identification. Characteristics: CRD Weapons Code Guidance Class Weight (lbs.) Length (in.) Diameter (in.) Fuze Signal Cartridges Carriage Options: Aircraft: F-18A-F AV-8B P-3C

Ballistic 500 lb. Practice Bomb 500 61.38 10.75 FMU-139 or M904E4 CXU-3, MK 4, and CXU-4A/B (for day use only)

Launcher/Rack: BRU-32 BRU-36

Contractor / Schedule / Improvements / Special Equipment: Contractor - Empty Bomb Assy - General Dynamics Ordnance and Tactical Systems formerly Intercontinental Manufacturing Co., Garland, Texas / Loaded Bomb Assy McAlester Army Ammunition Plant, McAlester, OK Status Inventory (Navy) Contractor / Schedule / Improvements / Special Equipment: Contractor - Intercontinental Manufacturing Co., Garland, Texas Status Inventory (Navy) Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT and NAVAIRSYSCOM PMA-201, NAS Patuxent River, MD and Naval Air Warfare Center Weapons Division, China Lake, CA

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Technical Order: NAVAIR 11-40-5, 11-140-10, or 11-5A-32

4-4

FOUO

Nomenclature: BDU-48

Name: 10 lb. Practice Bomb

Capability: Training ordnance to simulate the 500 lb. MK 82 and 2000 lb. MK 84 general purpose, nonguided bombs in a high drag configuration. Designed to be carried and dropped from a level horizontal position on the aircraft. Description: The BDU-48 is a thin cased cylindrical shaped practice bomb used to simulate retarded weapon delivery that utilizes a spotting charge to display target marking. It is composed of a bomb body, a retractable suspension lug, a firing assembly and box-type conical fins. It utilizes the MK 4 or CXU-3 signal cartridges as a spotting charge to display target marking. When the bomb is released from the aircraft it free falls until impact. Upon impact the bomb drives a firing pin assembly against a primer activating the signal charge. The resulting flash and puff of smoke permits visual evaluation of accuracy. Characteristics: CRD Weapons Code ZP91B

PRACTICE BOMB RETARD, BDU 48/CXU3

Guidance Class Weight (lbs.) Length (in.) Diameter (in.) -

ZP91A

PRACTICE BOMB RETARD, BDU 48/MK 4

Ballistic 10 lb. Practice Bomb 10 21.00 3.875

Carriage Options: AV-8B F/A-18A-F Contractor / Schedule / Improvements / Special Equipment: Contractor - Currently None, Previously Delfasco Inc., Afton, TN Status Inventory Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT; NAVAIRSYSCOM PMA-201, NAS Patuxent River, MD and Naval Air Warfare Center Weapons Division, China Lake, CA Technical Order: 11A3-3-7 (Bomb and CXU-3A/B) NAVAIR 11-5A-32

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Nomenclature: BDU-50

Name: 500 lb. Practice Bomb

Capability: Training ordnance representative in size and weight of an explosive filled bomb to simulate the 500 lb. MK 82 general purpose bomb. Description: The BDU-50 is a 500 lb. practice bomb, an inert version of the MK 82. This inert “heavyweight” bomb is dropped either with a parachute for “High Drag” or “Slick,” which has no drag device. Delivery of a BDU-50 High Drag Bomb from a low altitude, low dive angle results in the bomb impacting at or near the target and has very little or no ricochet, due to the aerodynamic effect of the high drag retard device. However, when the high drag system fails to deploy, the weapon takes on the characteristics of a low drag weapon and has a significantly increased slant range to impact (up to 4,000 ft longer under certain conditions). The bomb is manufactured as a forged configuration and manufactured as a cast ductile iron configuration as well. Characteristics: CRD Weapons Code ZL5CA BL2CM

Guidance Class Weight (lbs.) Length (in.) Diameter (in.) -

LGB GBU-12 PW-II BDU-50 F117 LGB GBU-12 PW-II FMU139A/B (T)

Ballistic Practice Bomb 521.00 (+-5) 89.44 10.80

Carriage Options: Aircraft: B-1B, B-2A, B-52H, F-15E

Launcher/Rack:

Contractor / Status / Improvements / Special Equipment: Contractor - General Dynamics, Garland, Texas (Forged Config.) and Allied Mechanical Greenville, Wisconsin (Cast Ductile Iron Config.) / Loaded Bomb Assy McAlester Army Ammunition Plant, McAlester, OK Status Inventory Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT and Naval Air Warfare Center Weapons Division, China Lake, CA Technical Order: 11-A3-4-7

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Nomenclature: BDU-56

Name: 2000 lb. Practice Bomb

Capability: Training ordnance representative in size and weight of an explosive filled bomb to simulate the 2000 lb.MK 84 general purpose bomb. Description: The BDU-56 is a 2,000 lb. practice bomb and an inert version of the MK 84. This inert “heavyweight” bomb is dropped either with a parachute for “High Drag”, or “Slick”, which has no drag device. Delivery of a BDU-56 High Drag Bomb from a low altitude, low dive angle results in the bomb impacting at or near the target and has very little or no ricochet, due to the aerodynamic effect of the high drag retard device. However, when the high drag system fails to deploy, the weapon takes on the characteristics of a low drag weapon and has a significantly increased slant range to impact (up to 4,000 ft longer under certain conditions). The bomb is manufactured as a forged configuration and manufactured as a cast ductile iron configuration as we. Characteristics: CRD Weapons Code ZL6CA ZL6CB ZE65B BE65B ZE65A BE65A BG6GA

LGB GBU-10 PW-II BDU-56 F117 LGB GBU-10 PW-II BDU-56 GBU-15 BDU-56 GPS IR CAP F-15E GBU-15 BDU56 GPS IR TAC INRT F15 GBU-15 BDU-56 GPS TV CAPT F-15E GBU-15 BDU56 GPS TV TAC INRT F15 GBU-15 IR BDU-56/TAC/INERT

ZL6BF ZL6BE BG6GB BG6TA BG6TB BG6TC BG6TD

LGB GBU-10 PW-1 /B BDU-56 LGB GBU-10 PW-1 A/B BDU-56 GBU-15 IR/BDU-56/TAC/INERT GBU-15 TV/BDU-56/TAC/INERT GBU-15 TV/BDU-56/TAC/INERT GBU-15 TV/BDU-56/TAC/INERT GBU-15 TV/BDU-56/TAC/INERT

Guidance - Ballistic Class 2,000 lb. Practice Bomb Weight (lbs.) - 2,168.42 (+-15) Length (in.) 291.84 Diameter (in.) - 18 Carriage Options: Aircraft: B-1B, B-2A, B-52H, F-15E

Launcher/Rack:

Contractor / Status / Improvements / Special Equipment: Contractor - General Dynamics, Garland, Texas (Forged Config.) and Allied Mechanical Greenville, Wisconsin (Cast Ductile Iron Config.) / Loaded Bomb Assy McAlester Army Ammunition Plant, McAlester, OK Status Inventory Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT and Naval Air Warfare Center Weapons Division, China Lake, CA Technical Order: 11-A3-4-7

4-7

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Nomenclature: BLU-109/B, A/B, B/B and C/B

Name: Hard Target Penetrator Warhead

Capability: Penetrate bunkers, aircraft (A/C) shelters and concrete structures. Description: The BLU-109 is a 2,000 lb. class hard target penetrator warhead. The BLU-109/B and C/B are used by the Air Force; the BLU-109A/B is the Navy version and the B/B is FMS use only. The A/B has the BLU-109/B's Tritonal explosive replaced with PBXN-109 (more insensitive to shock and heat), is fitted with a permanent external hardback, and has an external thermal protective coating. The B/B is physically the same as the -/B but has PBXN-109 as the explosive. The BLU-109C/B in an Air Force version that uses AFX-757 explosive and IM hardware (ventplate) The BLU-109 body is a 25.4 mm (1 in.) thick casing of forged gun-barrel hardened steel. This body is approximately twice the thickness of the MK 84. It is typically detonated by an FMU-143 series tail fuze. The absence of a nose fuze well (cavity) makes the nose stronger and, additionally, the weapon’s base plate is reinforced to better protect the fuze from the shock of impact. The BLU-109 is not used as a stand-alone free fall bomb; it is a warhead for the following guided bombs and missile: GBU-10, -15, -24, -27 and -31(V)3/B, and AGM-130. Characteristics: CRD Weapons Code BC91A

BLU-109 FMU-143

Class Length (in.) Diameter (in.) Warhead (lbs.) Explosive (NEW) Fuze -

SZBCA

STAMP BLU-109 BOMB

2,000 lb. Penetrator, Blast/Fragmentation 98.85 14.50 1950 535 lbs. Tritonal (BLU-109/B); 524 lbs. PBXN-109 (BLU-109A/B, B/B); 600 lbs. AFX-757, IM hardware (ventplate) (BLU-109C/B) FMU-143 Series

Contractor / Schedule / Improvements / Special Equipment: Contractor - Empty Bomb Assy - Ellwood National Forge Company / Loaded Bomb Assy McAlester Army Ammunition Plant, McAlester, OK Status Inventory/Production Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT; NAVAIRSYSCOM PMA-201, NAS Patuxent River, MD; and Naval Air Warfare Center Weapons Division, China Lake, CA Technical Order: 11A1-11-7, NAVAIR 11-5A-32

BLU-109A/B

BLU-109/B

4-8

FOUO

Nomenclature: BLU-110/B, A/B , B/B, and C/B

Name: General Purpose (GP) Bomb

Capability: Attack soft fragment sensitive targets, troops, POL, radars, and aircraft in the open. Description: The BLU-110 General Purpose Bomb is identical to the MK 83 MOD 5 bomb, with the exception of the explosive filler. It is used by the Navy and Air Force. The Navy version is thermallyprotected to extend the cook-off times and has three yellow bands on the bomb. The Air Force version has only one yellow band. This bomb has a slender body made of steel with a well in the nose section for a proximity sensor, mechanical fuze and adapter booster, or a penetrating nose plug; and a well in the aft section for a tail electric fuze. It is compatible with proximity sensor, mechanical, and electrical or electronic fuzes. It uses either a conical or retarding fin, or laser/GPS guidance airfoil kit, or a mine kit. The BLU-110B/B (Air Force) and C/B (Navy) have vented base plates for better IM reaction. Characteristics: CRD Weapons Code Guidance Ballistic Control Low and High Drag Fins; Airfoil Groups (Laser Guided Bombs) Class 1,000 lb. General Purpose Bomb Body with Casing Bomb with Fin (ME-83) Bomb with Retarded Fin (BSU-85) Weight (lbs.) 903 905 995 Length (in.) 72.47 114.07 110.25 Diameter (in.) 14.22 Warhead (lbs.) 1,000 lb. Blast/Fragmentation Explosive (NEW) - 385 lbs. PBXN-109 Fuze FMU-139; M904E4 with thermally-protected adapter-booster M148E1 Sensor DSU-33 Stabilizer MK83 CFA/BSU-85 Carriage Options: Aircraft: AV-8A F/A-18A-F A-10 F-15E F-16A-D

Launcher/Rack: Multiple (14 in. Lug Spacing)

Contractor / Schedule / Improvements / Special Equipment: Contractor - Empty Bomb Assy - General Dynamics, Garland, Texas / Loaded Bomb Assy McAlester Army Ammunition Plant, McAlester, OK Status Inventory (Navy, A/B Config. and AF, /B Config.) / Future Inventory (Navy, C/B Config. and AF, B/B Config.)

4-9

FOUO

Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT and NAVAIRSYSCOM PMA-201, NAS Patuxent River, MD and Naval Air Warfare Center Weapons Division, China Lake, CA Technical Order: 11A1-6-7 / NAVAIR 11-5A-17, 11-140-5, 11-5A-32

BLU-110 Typical Configuration (Navy), Air Force version has only 1 yellow band

4-10

FOUO

Nomenclature: BLU-111/B, A/B, B/B, and C/B

Name: General Purpose (GP) Bomb

Capability: Attack soft fragment sensitive targets, troops, POL, radars, and aircraft in the open. Description: The BLU-111 General Purpose Bomb is identical to MK 82 MOD 2 bomb, with the exception of the explosive filler. This bomb has a slender body made of steel with a well in the nose section for a proximity sensor, mechanical fuze and adapter booster, or a penetrating nose plug; and a well in the aft section for a tail electric fuze. It is compatible with proximity sensor, mechanical, and electrical or electronic fuzes. It uses either a conical, non-retard, or retarding fin, or laser/GPS guidance airfoil kit, or a mine kit. The BLU-111B/B (Air Force) and C/B (Navy) have vented base plates for better IM reaction. The Navy BLU-111 bomb bodies have a thermal protective coating applied to the surface to extend the cook-off times. The Air Force version will not be thermally coated. The BLU-111/B nomenclature was originally established for the Air Force but has not been procured or used. Characteristics: CRD Weapons Code Guidance - Ballistic Control Low and High Drag Fins; Airfoil Groups (Laser Guided Bombs) Class 500 lb. General Purpose Bomb Body with Casing Bomb with Fin (BSU-33, MAU-93) Bomb with Retarded Fin (BSU-86) Weight (lbs.) 460 485 530 Length (in.) 60.57 85.30 91.30 Fin span (in.) N/A 15.06 18.5 (BSU-86) Diameter (in.) 11.05 Warhead (lbs.) - 500 lb. Blast/Fragmentation Explosive (NEW) - 190 lbs. PBXN-109 Fuze MU-139; M904E4 with thermally-protected adapter-booster M148E1 Sensor DSU-33 Stabilizer BSU-33 Conical fin, BSU-49 Retard Fin, BSU-86 Retard Fin Carriage Options: Aircraft: AV-8A F/A-18A-F P-3C

Launcher/Rack: (14 in. Lug Spacing)

Contractor / Schedule / Improvements / Special Equipment: Contractor - Empty Bomb Assy - General Dynamics, Garland, Texas / Loaded Bomb Assy McAlester Army Ammunition Plant, McAlester, OK Status Inventory/Production (Navy, A/B Config., Future C/B Config.), Future Inventory RY10 (AF, /B and B/B Config.)

4-11

FOUO

Management/Engineering: NAVAIRSYSCOM PMA-201, NAS Patuxent River, MD and Naval Air Warfare Center Weapons Division, China Lake, CA Technical Order: 11A1-6-7 / NAVAIR 11-5A-17, 11-140-5, 11-5A-32

BLU-111A/B Typical Navy Configuration

4-12

FOUO

Nomenclature: BLU-113A/B

Name: Desert Storm Special Penetrator Warhead

Capability: Penetration weapon used for deeply buried and hardened targets. Description: The BLU-113A/B is a 5,000 pound class penetrator. The case is made from HP9420 alloy steel to provide target penetration capabilities. The bomb body is loaded with 80/20 (TNT/aluminum) tritonal explosives and utilizes a single fuze. The BLU-113A/B is not used as a stand-alone free fall bomb. It is a warhead used in the GBU-28A/B, B/B. Characteristics: CRD Weapons Code - See Chapter 5 Class 5000 lb. Penetrator, Blast/Fragmentation Weight (lbs.) 4,500 Length (in.) 1 53.0 Diameter (in.) 14.5 Explosive 625 lbs. Tritonal Fuze FMU-143 Series and FMU-152 Contractor / Schedule / Improvements / Special Equipment: Contractor - Lockheed (BLU-113/B), Ellwood National Forge (BLU-113A/B) Status Inventory/Production Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A1-11-7

4-13

FOUO

Nomenclature: BLU-116A/B

Name: Special Purpose Bomb

Capability: Attack soft fragment sensitive targets, troops, POL, radars, and aircraft in the open. Description: The BLU-116A/B is a Navy 2000 lb. class Special Purpose Bomb consists of an explosive filled hardened steel penetrating case surrounded by an aerodynamic airframe, fuze well, and associated hardware. It has the same external profile as the BLU-109A/B minus the thermal coating with similar mass properties. The explosive fill is a minimum of 115 lbs. of PBXN-109. The weight of the bomb is 1869 + 46 lbs. The bomb consists of two major subassemblies, the airframe subassembly and the penetrator subassembly. The airframe subassembly is comprised of the airframe tube, the airframe nose, forward and aft pallet supports, and the lug adapter subassembly, which interfaces the bomb case to the lug sleeve for the GBU-24 and react to the swaybrace loads. The penetrator case subassembly consists of the case, the fuzed well and the fuze retaining ring. The BLU-116A.B has a shelf life of 20 years and a service life of 10 years. An inert filled bomb body is available for training purposes. The bomb is identified by blue color code banding vice yellow and the presence of filler “E” markings. Characteristics: CRD Weapons Code - N/A Guidance Ballistic Control Airfoil Groups (Laser Guided Bombs) Class 2,000 lb. Special Purpose Bomb Body with Casing Weight (lbs.) 1869 + 46 Length (in.) 95 Fin span (ins.) N/A Diameter (in.) 14.5 Warhead (lbs.) 2,000 lb. Penetrator Explosive (NEW) - 115 lbs. PBXN-109 Fuze FMU-143 Series Sensor DSU-33 Stabilizer MK84 Conical Designation Warhead

GCU

Airfoil Group

Fuze

User

GBU-24G/B BLU-116A/B

WGU-39A/B

BSU-84B/B

FMU-143 Series USN

Carriage Options: Aircraft: F/A-18A-F

Launcher/Rack: (30 in. Lug Spacing)

Contractor / Schedule / Improvements / Special Equipment: Contractor - Naval Air Warfare Center Weapons Division, China Lake, CA, and MCAAP Status Inventory (Navy) Management/Engineering: NAVAIRSYSCOM PMA-201, NAS Patuxent River, MD and Naval Air Warfare Center Weapons Division, China Lake, CA

4-14

FOUO

Technical Order: NAVAIR 11-5A-17

4-15

FOUO

Nomenclature: BLU-117/B, A/B, B/B, and C/B

Name: General Purpose (GP) Bomb

Capability: Attack soft fragment sensitive targets, troops, POL, radars, and aircraft in the open. Description: The BLU-117 General Purpose Bomb is identical to the 2,000 pound class MK 84 MOD6 bomb, with the exception of the explosive filler. It is in the Navy inventory now and expected to be added to the AF inventory in FY10. The Navy version is thermally-protected. This bomb has a slender body made of steel with a well in the nose section for a proximity sensor, mechanical fuze and adapter booster, or a penetrating nose plug, and a well in the aft section for a tail electric fuze. It is compatible with proximity sensor and mechanical/electrical/electronic fuzes. It uses a conical fin, or laser/GPS guidance airfoil kit, or a mine kit. The BLU-117C/B (Thermally Protected) or BLU-117B/B (Non- Thermally Protected) has a vented base plate for better IM reaction. The Navy bomb bodies have a thermal protective coating applied to the surface to extend the cook-off times. The interior of the bomb houses the forward and rear charging tubes and the explosive filler PBXN-109 in BLU-117A/B or AFX-795 in BLU-117C/B and BLU-117B/B. The BLU-117/B nomenclature was originally established for the Air Force but has not been procured or used. Characteristics: CRD Weapons Code - N/A Guidance Ballistic Control Low and High Drag Fins; Airfoil Groups (Laser Guided Bombs) Class 2,000 lb. General Purpose Bomb Body with Casing Bomb with Conical Fins (MK84) Weight (lbs.) 1880 2025 Length (in.) 97.34 145.18 Fin span (ins.) N/A 25.31 Diameter (in.) 18.30 Warhead (lbs.) 2,000 Blast/Fragmentation Explosive (NEW) - 930 lbs. (PBXN-109 in BLU-117A/B or AFX-795 in BLU-117B/B and BLU-117C/B) Fuze FMU-139; M904E4 with thermally-protected adapter-booster M148E1 Sensor DSU-33 Stabilizer MK84 Conical, BSU-50 Retarder Carriage Options: Aircraft: F/A-18A-F

Launcher/Rack: (30 in. Lug Spacing)

Contractor / Schedule / Improvements / Special Equipment: Contractor - Empty Bomb Assy - General Dynamics, Garland, Texas / Loaded Bomb Assy McAlester Army Ammunition Plant, McAlester, OK (MCAAP) Status Inventory (Navy, A/B Current, C/B Future), Future Inventory (AF, B/B Configuration)

4-16

FOUO

Management/Engineering: NAVAIRSYSCOM PMA-201, NAS Patuxent River, MD and Naval Air Warfare Center Weapons Division, China Lake, CA Technical Order: NAVAIR 11-5A-17, 11-140-5, 11-5A-32

BLU-117 Typical Navy Configuration

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FOUO

Nomenclature: BLU-119/B

Name: CrashPAD

Capability: Defeat Fixed Soft/Semi-Hardened Chem Bio Targets. Description: The BLU-119/B is designed to defeat fixed semi-hardened Chem Bio targets. It is a 2,000 pound Class Bomb based upon the MK 84 bomb body with a unique explosive fill. The bomb body is loaded with explosives to provide fragmentation and white phosphorus to provide dispersion and create an intense fire when the bomb explodes to neutralize aerosolized agent. The name CrashPAD refers to the Prompt Agent Defeat (PAD) system first created under a crash program. The BLU-119/B is not used as a stand-alone free fall bomb. It is a warhead used in the GBU-31(v)5/B. Characteristics: Class 2,000 lb. General Purpose Bomb, Blast/Fragmentation Weight (lbs.) 1,970 Length (warhead only) (in.) - 98.76 Diameter (in.) 18.00 Warhead (lbs.) 2,000 - Modified MK 84 Blast/Fragmentation with PBXN-109 HE (170 lbs.) and three canisters of White Phosphorus (420 lbs.) Fuze FMU-139, FMU-152 Contractor / Schedule / Improvements / Special Equipment: Contractor - ATK Status Inventory Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A1-7-7

BLU-119/B

4-18

FOUO

Nomenclature: BLU-121A/B

Name: Enhanced Blast Weapon

Capability: Functional Defeat of Hard and Deeply Buried Targets (HDBT) focused on Tunnels. Description: The BLU-121A/B is a 2,000 lb. class warhead similar to the MK 84 with a high-strength steel bomb case and filled with an enhanced energetic explosive (AFX-757). The bomb was initially designed as a tunnel defeat weapon, entering tunnel openings, detonating and propagating overpressures down the tunnel. However, the warhead design is based on MK 84 and should be physically interoperable with any MK 84 compatible guidance kit. The aft closure plate and the nose guidance kit interface are similar to the BLU-109 warhead. The BLU-121A/B is not used as a stand-alone free fall bomb. It is a warhead used in the GBU-15XXX. Characteristics: Guidance -

Warhead only - currently used with EGBU-15 software (v. 6.4 or later) modified for low angle delivery (LAD) Class 2,000 lb. Blast/Fragmentation Length (in.) 98.5 Diameter (in.) 18 Weight (lbs.) 2025 Explosive (NEW) - 978 lb. AFX-757 Fuze FMU-143N/B Carriage Options: Aircraft: F-15E

Launcher/Rack: BRU-47 (30 in. Lug Spacing)

Contractor / Schedule / Improvements / Special Equipment: Contractor - Air Armament Center Status Limited Inventory Management/Engineering: Development - DTRA/CXSH, Ft Belvoir, VA - 685 ARSS, Eglin AFB, FL Sustainment - 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A1-11-7

BLU-121A/B

4-19

FOUO

Nomenclature: BLU-122/B

Name: Hard Target Munition Penetrator Warhead

Capability: Penetrate Hard and Deeply Buried Targets (HDBT). Description: The BLU-122 is a 5,000 pound class penetrator. The case is made from Eglin Steel (ES-1) to provide deeper target penetration capabilities and survivability over the BLU-113. The bomb body is loaded with AFX-757 explosive and utilizes an auxiliary booster explosive, PBXN-110. The BLU-122 improves upon the BLU-113 in terms of penetration, survivability, lethality, explosive insensitivity (IM), and targets held at risk. The BLU-122/B is not used as a standalone free fall bomb. It is a warhead used in the GBU-28C/B. Characteristics: Class 5,000 lb. Penetrator, Blast/Fragmentation Weight (lbs.) - 4,450 Length (in.) 159.0 Diameter (in.) - 15.3 Explosive 781 lbs. AFX-757 and PBXN-110 booster Fuze FMU-143 and FMU-152 Contractor / Schedule / Improvements / Special Equipment: Contractor - General Dynamics-OTS, Niceville, Florida Status Production Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A1-11-7

BLU-122/B

4-20

FOUO

Nomenclature: BLU-126/B

Name: Low-Collateral Damage (LoCo) Bomb

Capability: Attack soft fragment sensitive targets, troops, POL, radars, and aircraft in the open with reduced collateral damage. Description: The Navy thermally-protected BLU-126/B is identical to the BLU-111A/B with the exception of the amount of PBXN-109 explosive filler. The aft end of the bomb is filled with approximately 27 pounds of PBXN-109; the remainder of the bomb is filled with PBXN-109 inert stimulant. The BLU-126/B Bomb is identical to the MK 82 MOD 2 bomb, with the exception of the explosive filler. This bomb has a slender body made of steel with a well in the nose section for a proximity sensor, mechanical fuze and adapter booster, or a penetrating nose plug, and a well in the aft section for a tail electric fuze. It is compatible with proximity sensor, mechanical, and electrical or electronic fuzes. It uses either a conical, non-retard, or retarding fin, or laser/GPS guidance airfoil kit, or a mine kit. The bomb bodies have a thermal protective coating applied to the surface to extend the cook-off times. The BLU-126/B is in both the Navy and AF inventories. Characteristics: CRD Weapons Code - N/A Guidance Ballistic Control Airfoil Groups (Laser Guided Bombs) JDAM KMU-572 Class 500 lb. General Purpose Bomb Body with Casing Weight (lbs.) 460 Length (in.) 60.57 Diameter (in.) 11.05 Warhead (lbs.) - 500 Blast/Fragmentation Explosive (NEW) - 27 lbs. PBXN-109 Fuze FMU-139 Sensor None Stabilizer 500 lb. Guidance Kits Carriage Options: Aircraft: AV-8A F/A-18A-D

Launcher/Rack: (14 in. Lug Spacing)

Contractor / Schedule / Improvements / Special Equipment: Contractor - Empty Bomb Assy - General Dynamics, Garland, Texas / Loaded Bomb Assy McAlester Army Ammunition Plant, McAlester, OK (MCAAP) Status Inventory (Navy) Management/Engineering: NAVAIRSYSCOM PMA-201, NAS Patuxent River, MD and Naval Air Warfare Center Weapons Division, China Lake, CA

4-21

FOUO

Technical Order: NAVAIR 11-5A-17, 11-140-5, 11-5A-32

BLU-126/B (LoCo Bomb)

PBXN-109

Inert

Felt Pad/Air Gap

4-22

FOUO

Nomenclature: M117

Name: 750 lb. GP Bomb

Capability: Attack soft fragment sensitive targets, troops, POL, radars, and aircraft in the open. Description: The M117 is a 750 pound class bomb used primarily in the same way as a MK 82 and was designed primarily for the B-52 to allow more weapons to be carried inside the aircraft. The M117R w/retard is the high drag variant of the original M117 and uses the MAU-91 retarding tail fin. Characteristics: CRD Weapons Code ZR74H ZC74B BC77B BC77A BR74J BR71J BR77A BC71A BC74D BC71F BC74F BC71D ZC71B ZC74A

M117 AIR B-52 M117 CONICAL B-52 M117 W/FMU-139A/B (T) B-2 M117 W/M904/905 B-2 M117/MAU-91 FMU-139 (T) B-52 M117/MAU-91 FMU139A/B(T) M117/MAU-91 W/FMU-139A/B (T) B-2 M117C 113 NS M117C 904 NS B-52 INT M117C 904/905 M117C 904/905 B-52 INT M117C FMU 139A/B (T) M117C 113 NS M117C 904/905 N/T B52

BC71R BC71S BC71P BC74C BC74B BC74G BR74I BR74Q BR74S ZR71H BR71E BR74G ZR74E BC71B

M117C DSU-33A/B FMU139 M117C DSU33B/B FMU139 M117C FMU-113/M905 M117C FMU-113/M905 B-52 M117C MAU-103 904/905 B-52-INTER M117C/FMU-113/M905 B-52 M117R/BSU-93 FMU-139 T B-52 M117R/BSU-93 FMU139 TL B52 M117R/BSU-93 M904 B52 M117R/BSU93B/FMU139 M117R/MAU-91 M904 NS M117R/MAU-91 M904 NS B52 M117R/MAU91 904 54/B N/T B52 BMB GP M117A2 FMU 139A/B (N)

Guidance Ballistic Class 750 lb. Blast/Fragmentation Weight (lbs.) - 737 Length (in.) 51.5 Diameter (in.) - 16 (22 w/fin installed) Warhead (lbs.) - 737 Explosive 386 lbs. Tritonal, 383 lbs. Minol II Fuze Mechanical or Electrical Stabilizer Fins, M131 or MAU-103 (Conical); MAU-91 or BSU-93/B (Retard) Carriage Options: Aircraft: A-10 B-52H

Launcher/Rack: (14 in. Lug Spacing)

Contractor / Schedule / Improvements / Special Equipment: Contractor - Pacific Missile Test Center, China Lake, CA Status Inventory

4-23

FOUO

Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A1-2-7

M117

4-24

FOUO

Nomenclature: M129/MJU-1

Name: Leaflet / Chaff Bomb

Capability: Dispense leaflets behind enemy lines. Description: The M129 Leaflet Bomb is a fiberglass reinforced container split longitudinally into two sections and held together by four latch assemblies on each side. When joined, the halves form a cylindrical body with an oval shaped nose. When the bomb is released from the aircraft the fuze is armed permitting the timing mechanism to start. The fuze functions at a preset time detonating an adapter booster which initiates detonating cord. The detonating cord separates the two bomb halves dispersing the load (leaflets). Characteristics: CRD Weapons Code L29AH L29AF L29AG

M129 LEAFLET 107/B M129 LEAFLET M909 M129 LEAFLET MK339

Guidance Class Weight (lbs.) Length (in.) Diameter (in.) Payload (lbs.) Explosive Fuze Stabilizer -

SZVMA ZLBAB

M129 LEAFLET BOMB M129 LEAFLET M339

Ballistic 200 lb. Canister 92 empty, 203 full (depends on paper weight) 90.00 16.00 (22.00 w/fin installed) 110 paper rolls or chaff bundles Fuze booster ignited detonating cord which cuts canister Timer: FMU-107, M909, Mk 339 Fins, M148

Carriage Options: Aircraft: A-10 B-52H F-15E F-16A-D

Launcher/Rack: Multiple (14 in. Lug Spacing)

Contractor / Schedule / Improvements / Special Equipment: Contractor - TBD Status Inventory Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A1-2-7/TO 1-1M-34

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M129/MJU-1

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Nomenclature: MK 56

Name: Moored Mine

Capability: Aircraft laid; underwater mine is used against high-speed and deep-operating submarines. Description: The MK 56 Moored Anti-Ship Warfare (ASW) mine (the oldest still in use) was developed in 1966. The MK 56, a 2000-pound aircraft-laid moored mine containing an explosive charge of 360 lbs. of HBX-3, designed specifically for effectiveness against highspeed and deep-operating submarines. Consisting of a nonmagnetic stainless-steel case and a cast-steel anchor, the Mk 56 is equipped with flight gear for launching from aircraft. When laid, the mine sinks to the bottom where case and anchor separation take place. Should the mine become embedded in bottom sediment before case/anchor separation and mooring take place, a slow burning propellant in the anchor is ignited which frees the mine from any mud it may be buried in. As the case raises, a hydrostat, which clamps to an 18-foot loose bight in the mooring cable, senses the preset mooring depth and falls free to release the loose bight, thus permitting the tension on the cable to relax and cause a pawling mechanism in the anchor to lock and stop further cable payout. Should the mooring mechanism allow the mine to rise to a depth which is too shallow, the case will scuttle. This feature reduces the possibility of compromise and eliminates a navigational hazard. Scuttling will also occur on sterilization or if the mooring cable breaks. Characteristics: Weight (lbs.) Length (in.) Diameter (in) Warhead Carriage Options: Aircraft: F/A-18A-D P-3C

2,000 114.3 22.4 360 lbs. HBX-3 Launcher: 30 inch lugs (no lanyard)

Contractor / Status / Improvements /Special Equipment: Contractor Status Inventory (Navy) Management/Engineering: NAVSEA PMS-495, Washington Navy Yard Technical Order:

MK 56 Moored Anti-Ship Warfare (ASW) Mine

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Nomenclature: MK 58 MOD 1

Name: Marine Location Marker

Capability: Mark locations on the ocean for tactical purposes. Description: MK 58 MOD 1 Marine Location Marker is designed for day or night use in any condition calling for long-burning, smoke and flame reference-point marking on the ocean's surface. In addition to being used for antisubmarine warfare, it is used for search-and-rescue operations, man-overboard markings, and as a target for practice bombing at sea. The marker produces a yellow flame and white smoke for a minimum of 40 minutes and a maximum of 60 minutes. It is visible for at least 3 miles under normal operating conditions. The MK 58 MOD 1 marine location marker consists of a cylindrical tin can. The can contains two pyrotechnic candles of a red phosphorus composition. The ignition end of the marker has three holes-two for smoke and flame emission and one for water to enter the MK 72 MOD 1 seawater-activated battery. Adhesive foil disks hermetically seal the two emission holes. A reinforced adhesive foil strip with a rectangular pull ring hermetically seals the battery cavity hole. The adhesive foil seals are protected during handling and shipping by a replaceable polyethylene protective cover. When the marker is released from the bomb rack, the arming wire retains the pull ring and removes the foil strip covering the battery's cavity. When submerged, the Mk 72 MOD 1 battery is activated by seawater. Current from the battery initiates a MK 13 electric squib, which ignites the starter composition of the first pyrotechnic candle. The composition ignites the starter pellet, which, in turn, ignites the first candle. When the first candle is nearly burned out, its heat ignites the transfer time fuze, which carries ignition to the second candle starter composition. This starter composition initiates the second pyrotechnic candle. Characteristics: Weight (lbs.) - 11+0.5 Length (in.) 21.7 Diameter (in.) - 4.9 Carriage Options: Aircraft: F/A-18A-D AV-8B

Launcher: IMER/ITER

Contractor / Status / Improvements /Special Equipment: Contractor - Kilgore Flares Status Inventory/Production (Navy) Management/Engineering: PMA-242 / NSWC Crane Technical Order:

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MK 58 MOD 1 Marine Location Marker

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Nomenclature: MK 62

Name: Quick Strike Mine

Capability: Primarily used against surface targets in shallow water. Description: The MK-62 underwater mine is an aircraft laid, influence -actuated bottom mine which is used against surface targets in shallow water. The MK62 is a conversion of General Purpose Bomb Bodies MK 82 or BLU-111, which is a 500 pound weapon. All mines have the capability of making arming-delay, sterilization, selfdestruct, and other operational settings. The newest Quick Strike mines are programmable and modular, allowing them to be updated to keep abreast of emerging threat targets. Ongoing Quick Strike work includes the development of new Target Detecting Devices (TDDs) and target processing algorithms. TDDs control the actuation of explosives in underwater mines. Design expertise centers on the three major areas of TDD development: (1) target influence sensors, (2) sensor signal processing and target logic, and (3) timing and control logic. These major areas include those functions necessary to control the weapon, such as trajectory, arming, and end-of-life functions. A representative sample of state-of-the-art target influence sensor technologies currently under development includes: (1) advanced signal processing techniques applied to sensor outputs to determine if a valid target is present, or if the detected influence signal(s) is being generated by a countermeasure device; and (2) state-of-the-art, low power, microprocessor and gate array technologies employed for timing and control functions. Characteristics: Guidance None Weight (lbs.) - 576 Length (in.) 89 Diameter (in.) - 15.1 Carriage Options: Aircraft: Launcher: B1B, B-52H, F/A-18A-D, P-3C Contractor / Status / Improvements / Special Equipment: Contractor Status - Inventory Management/Engineering: NAVSEA PMS-495, Washington Navy Yard Technical Order: 11A1-6-7

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Nomenclature: MK 63

Name: Quick Strike Mine

Capability: Aircraft laid; underwater mine is used against logistic/landing craft, amphibious vessels, and patrol craft. Description: The MK63 is an aircraft-laid bottom mines for use against submarines and surface targets. The MK-63 is an influence -actuated bottom mine which is used against logistic/landing craft, amphibious vessels, and patrol craft. The MK63 is a conversion of General Purpose Bomb Bodies MK 83 or BLU-111, which is a 1000 pound weapon. All mines have the capability of making arming-delay, sterilization, self-destruct, and other operational settings. The newest Quick Strike mines are programmable and modular, allowing them to be updated to keep abreast of emerging threat targets. Ongoing Quick Strike work includes the development of new Target Detecting Devices (TDDs) and target processing algorithms. TDDs control the actuation of explosives in underwater mines. Design expertise centers on the three major areas of TDD development: (1) target influence sensors, (2) sensor signal processing and target logic, and (3) timing and control logic. These major areas include those functions necessary to control the weapon, such as trajectory, arming, and end-of-life functions. A representative sample of state-of-the-art target influence sensor technologies currently under development includes: (1) advanced signal processing techniques applied to sensor outputs to determine if a valid target is present, or if the detected influence signal(s) is being generated by a countermeasure device; and (2) state-of-the-art, low power, microprocessor and gate array technologies employed for timing and control functions. Characteristics: Guidance None Weight (lbs.) - 1061 Length (in.) 113 Diameter (in.) - 22.9 Carriage Options: Aircraft: F/A-18A-D, B-52H, P-3C

Launcher:

Contractor / Status / Improvements / Special Equipment: Contractor Status - Inventory Management/Engineering: NAVSEA PMS-495, Washington Navy Yard Technical Order: 11A1-6-7

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Nomenclature: MK 65

Name: Quick Strike Mine

Capability: Aircraft laid; underwater mine is used against logistic/landing craft, amphibious vessels, and patrol craft. Description: The MK 65 is an aircraft-laid bottom mine for use against submarines and surface targets. The MK-65 is an influence-actuated bottom mine which is used against logistic /landing craft, amphibious vessels, and patrol craft. The Mk 65 is a 2000-pound weapon, employing a distinctively different, new concept, thin-walled, mine-type case, as opposed to the thick-walled bomb-type case of the Mk 62 and 63. Older Quick Strike versions (MK62 and MK63) were converted streamlined bombs of the 500 lb. and 1000 lb. sizes. Other differences in the Mk 65 include a special arming device, a nose fairing, and a tail section adaptable to parachute option. All mines have the capability of making arming-delay, sterilization, self-destruct, and other operational settings. The newest QUICKSTRIKE mines are programmable and modular, allowing them to be updated to keep abreast of emerging threat targets. Ongoing QUICKSTRIKE work includes the development of new Target Detecting Devices (TDDs) and target processing algorithms. TDDs control the actuation of explosives in underwater mines. Design expertise centers around the three major areas of TDD development: (1) target influence sensors, (2) sensor signal processing and target logic, and (3) timing and control logic. These major areas include those functions necessary to control the weapon, such as trajectory, arming, and end-of-life functions. A representative sample of state-of-the-art target influence sensor technologies currently under development includes: (1) advanced signal processing techniques applied to sensor outputs to determine if a valid target is present, or if the detected influence signal(s) is being generated by a countermeasure device; and (2) state-of-the-art, low power, microprocessor and gate array technologies employed for timing and control functions. Characteristics: Guidance None Weight (lbs.) - 2390 Length (in.) - 128 Diameter (in.) - 29 Carriage Options: Aircraft: Launcher: B-1B, F/A-18A-D, B-52H, P-3C Contractor / Status / Improvements / Special Equipment: Contractor Status - Inventory Management/Engineering: NAVSEA PMS-495, Washington Navy Yard Technical Order: 11A1-6-7

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Nomenclature: MK 76 MOD 5

Name: 25 lb. Practice Bomb

Capability: Training bomb that simulates the MK 82 bomb in a low drag configuration. Description: The MK 76 is a tear dropped shaped practice bomb that simulates a MK 82 low drag configuration used by the Navy. It is similar to the AF BDU-33. The MK 76 is a 25 lb. subcaliber Practice Bomb with a tear drop shaped cast metal body and sheet metal fins. It utilizes the MK 14 suspension lug for suspension on the bomb racks. It also utilizes the MK 4 or CXU-3 signal cartridges as a spotting charge to display target marking. When the bomb is released from the aircraft it free falls until impact. Upon impact the bomb drives a firing pin assembly against a primer activating the signal charge. The resulting flash and puff of smoke permits visual evaluation of accuracy. Characteristics: CRD Weapons Code - N/A NSN: 1325-01-071-2561 NALC: E973 P/N: 2193779 Guidance Ballistic Class 25 lb. Practice Bomb Weight (lbs.) - 25 Length (in.) 24.64 Diameter (in.) - 4.00 Carriage Options: Aircraft: Launcher/Rack: AV-8B ITER BRU-42, IMER BRU-41, F/A-18A-F Practice Multiple Bomb Rack (PMBR), Contractor / Schedule / Improvements / Special Equipment: Contractor - Del Fasco Inc., Afton, TN Status Full Rate Production Management/Engineering: NAVAIRSYSCOM PMA-201; NAS Patuxent River, MD; and NAWCWD, China Lake, CA Technical Manuals: NAVAIR 11-140-5, NAVAIR 11-5A-32

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Nomenclature: MK 77 MOD 5, 6

Name: Fire Bomb

Capability: Defeat dug-in troops, supply installations, wooden structures, and land convoys. Description: The MK 77 MOD 5, 6 Fire Bomb is a thin skinned container of that ruptures on impact and spreads burning fuel gel on surrounding objects. MK 13 Mod 0 igniters are used to ignite the fuel gel mixture upon impact. The Mk-77 is the only fire bomb still in service. The MK 77 is 750-lb.incendiary bomb carrying 110 U.S. gallons of a fuel gel mix which is the direct successor to napalm. The MK-77 is the primary incendiary weapon currently in use by the United States military. Instead of the gasoline and the benzene fuel used in napalm, the MK-77 uses kerosene-based fuel, which has a lower concentration of benzene. The MK-77 has less impact on the environment than napalm. The mixture reportedly also contains an oxidizing agent, making it more difficult to put out once ignited. MK 77 MOD 6 casing was redesigned without the arming wire guides (no longer used) for economical production. Characteristics: Weight (lbs.) - 520 (filled) Length (in.) 81.2 Diameter (in.) - 18.6 Carriage Options: Aircraft: AV-8B F/A-18A-D

Launcher: 14 in. lugs (no lanyard)

Contractor / Status / Improvements /Special Equipment: Status - Inventory (Navy) Management/Engineering: PMA-201, Patuxent River, MD Technical Order: NAVAIR 11-140-5

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Nomenclature: MK 81

Name: 250 lb. GP Bomb

Capability: Attack soft fragment sensitive targets, troops, POL, radars, and aircraft in the open. Description: MK 81 GP BOMB: The MK 81 is designed for soft, fragment sensitive targets such as troops, POL, and radars. This bomb is relatively thin cased with a slender body design for improved ballistics. Approximately 40 percent of assembled weight of bomb is an explosive charge. This weapon is not intended for hard targets or penetrations. Characteristics: CRD Weapons Code ZC11H MK81/CONICAL FIN BC14A MK81C 904/905 N/T B52 BC11E MK81C 905 T ZC14A MK81C 904/905 N/T B52 BC11D MK81C 113 NS BC11H MK81C DSU33A/B FMU139 BC11C MK81C 904 NS BC11K MK81C DSU-33B/B FMU-139 BC11B MK81C 904/905 N/T Guidance Ballistic Class 250 lb. General Purpose Bomb, Blast/Fragmentation MK 81 Low Drag - Weight (lbs.) - 250 +/- 5% - Length (in.) - 49.30 Warhead (lbs.) 250 Explosive (NEW) - 100lbs Tritonal, or H-6 Fuze Variety for nose and tail. Stabilizer Conical Fin Carriage Options: Aircraft: A-10 F-16A-D

Launcher/Rack: Multiple (14 in. Lug Spacing)

Contractor / Schedule / Improvements / Special Equipment: Contractor - Nad Crane Status Inventory Management/Engineering: 506 CBSS/GBLB, Hill AFB, and NAVAIRSYSCOM PMA-201, NAS Patuxent River, MD and Naval Air Warfare Center Weapons Division, China Lake, CA Technical Order: 11A1-4-7

MK 81

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Nomenclature: MK 82

Name: 500 lb. GP Bomb

Capability: Attack soft fragment sensitive targets, troops, POL, radars, and aircraft in the open. Description: The MK 82 is designed for soft, fragment sensitive targets such as troops, POL, and radars. The Air Force is the primary user. This weapon is not intended for hard targets or penetrations. The targets will include troops, aircraft in the open, etc. Characteristics: CRD Weapons Code BC27D BC27A BC27C BC27B BR27A BR21W BR24G BR27B BR26B BC24B BC24A BC21L BC21H BC21B BC21I ZCE1F ZCE1J ZCE1C BC21T BC21V BC21P ZCE1B BC21S ZCE1E ZCE4A ZRE1L ZBE4E ZRE4H ZRE1G ZBE1A

MK82 DSU33B/B FMU139 B-2 MK82 FMU-139 B-2 MK82 W/DSU-33A/B FMU139 B-2 MK82 W/M904/905 B-2 MK82/BSU-49 FMU-139 B-2 MK82/BSU-49 FMU139A/B (T) MK82/BSU-49 FMU139A/B TL B52 INT MK82/BSU-49 W/FMU-113 (N) B-2 MK82/BSU-49 W/FMU-139 (N) B-1 MK82C 904/905 B-52 MK82C 904/905 B-52 MK82C 113 NS MK82C 904/905 N/T MK82C 113/905 MK82C 26/26 MK82C (I) 904 NS MK82C (I) FMU139 TL MK82C DSU33/FMU139 N/T MK82C DSU33A/B FMU139 MK82C DSU33B/B FMU139 MK82C FMU 139A/B (T) MK82C FMU-113/M905 N/T MK82C FMU139A/B (N) MK82C(I) 904/905 N/T MK82C(I) 904/905 N/T B-52 MK82R FMU-139 MK82R (I) / MK15 FMU139 B-52 INT MK82R (I) BSU-49 FMU-139 B52 MK82R (I) BSU49 904/905 N/T MK82R (I)/MK15 54A/B TL

ZBE1D BR21X BR26C BR21Y BR26D ZRE1E ZBE4A BR26A BR21A BR21B BR24E BR24K BR21L BR24J BR21E BB23D BB25G BB24G BB23L BB21R BB24H BB21K BB25F PR21A PR21B SZBDA SZBAA SZBFA SZVGB

MK82R (I)/MK15 904/54AB N/T MK82R DSU33A/B FMU139 MK82R DSU33A/B FMU139 B-1 MK82R DSU33B/B FMU139 MK82R DSU33B/B FMU139 B-1 MK82R(I) BSU-49 M904 NS MK82R(I)/MK15 54/B TL B-52 INTER MK82R/BSU-49 139 TL B-1 MK82R/BSU-49 904 NS MK82R/BSU-49 905 T MK82R/BSU-49 904 NS B52-INTERNAL MK82R/BSU-49 904/905 B52-INTERNA MK82R/BSU-49 904/905 N/T MK82R/BSU-49 905 TL B52-INTERNAL MK82R/BSU-49 M904 NS FMU-139 T MK82R/MK15 M904 A10 MK82R/MK15 139A/B T F-15E MK82R/MK15 904 NS B52-INTERNAL MK82R/MK15 FMU-139 A/B A10 MK82R/MK15 FMU139A/B (T) MK82R/MK15 FMU139A/B B-52-INTER MK82R/MK15 M904 MK82R/MK15 M904 NS F-15E PREPO ISO MK82 HD W/FMU-139 T PREPO ISO MK82 HD W/M904/M905 NT STAMP MK82 AIR KIT STAMP MK82 BOMB STAMP MK82 LOW DRAG KIT STAMP B-1/B MK82 HIGH DRAG KIT

Guidance - Ballistic Class 500 lb. General Purpose Bomb, Blast/Fragmentation MK82 AIR MK82 Snakeye I Mdl 0, 1 Weight-Full (lbs.) - 533.10 +/- 0.5% Weight-Full (lbs.) - 550.0 +/- 0.5% cg (x) 8.95 in +/- 0.5% cg (x) 9.30 in +/- 0.5% cg (y) -0.06 in +/- 0.5% cg (y) unk +/- 0.5% cg (z) -0.06 in +/- 0.5% cg (z) unk +/- 0.5%

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Length (in.) - 85.86 Length with nose fuze (in.) - 89.66 Length with nose plug (in.) - 91.16 Diameter (in.) - 10.80 Inertia (pitch) 1.50 +/- 10% Inertia (roll) 49.93 +/- 10% Inertia (yaw) 49.89 +/- 10%

MK82 LDGP Mdl 0, 1 Weight-Full (lbs.) - 502.0 +/- .5% cg (x) 6.48 in. +/- .5% cg (y) -.04 in. +/- .5% cg (z) -.06 in. +/- .5% Length (in.) - 89.44 Length with M904 fuze (in.) -93.24 Diameter (in.) - 10.80

Length (in.) - 85.50 Diameter (in.) - 10.80 Inertia (pitch) 2.10 +/- 10% Inertia (roll) 48.00 +/- 10% Inertia (yaw) 48.00 +/- 10% Inertia (pitch) wings deployed 53.0 +/- 10% Inertia (roll) wings deployed unk +/- 10% Inertia (roll) wings deployed 53.0 +/- 10% Drawings - 1380543 MK82 (BSU-49B) Weight-Full (lbs.) - NGT 70 cg (x) 7.0 in +/- 2.0 in aft of forward lug prior to deployment cg (y) unk +/- 0.5% cg (z) unk +/- 0.5% Length (m) - 0.66 Diameter (mm) – 222

Inertia (pitch) unk +/- 10% Inertia (roll) 38.17 +/- 10% Inertia (yaw) 38.22 +/- 10% Drawings Interface Control Drawings Employment Limits Environmental Limits Warhead (lbs.) Explosive (NEW) Fuze Stabilizer Carriage Options: Aircraft: A-10 B-1B B-2A B-52H F-15A-E F-16A-D AV-8B F/A-18A-F P-3C

809194, DL809194-10 4902393, 1380901, 3823738-503 PIDS SP809194 para 3.2.1 PIDS SP809194 para 3.2.5 500 192b lbs. Tritonal, Minol II, or H-6 Variety for nose and tail MAU-93/B, BSU-49/B AIR, BSU-33, BSU-86 Launcher/Rack - Multiple (14 in. Lug Spacing)

Contractor / Schedule / Improvements / Special Equipment: Contractor - Empty Bomb Assy - General Dynamics, Garland, Texas / Loaded Bomb Assy McAlester Army Ammunition Plant, McAlester, OK Status Inventory Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT and NAVAIRSYSCOM PMA-201, NAS Patuxent River, MD and Naval Air Warfare Center Weapons Division, China Lake, CA

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Technical Order: 11A1-5-7, NAVAIR 11-140-5, 11-5A-32

MK 82

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Nomenclature: MK 83

Name: 1,000 lb. GP Bomb

Capability: Attack soft fragment sensitive targets, troops, POL, radars, and aircraft in the open. Description: The MK 83 is designed for soft, fragment sensitive targets such as troops, POL, and radars. The Navy is the primary user. This weapon is not intended for hard targets or penetrations. Characteristics: CRD Weapons Code BC31A MK83C 904/905 N/T ZC31B MK83C 904/905 N/T Guidance Ballistic Control Low and High Drag Fins; Airfoil Groups (Laser Guided Bombs) Class 1,000 lb. General Purpose Bomb Weight (lbs.) 1,000 Length (in.) 115 Diameter (in.) 14 Warhead (lb.) 1,000 Blast/Fragmentation Explosive (NEW) - 445 lbs H-6, Tritonal, or PBXN-109 Fuze Variety of mechanical and electrical Stabilizer Mk 83 Mod 0, BSU-85/B AIR Stabilizer Carriage Options: Aircraft: Launcher/Rack: Multiple A-10 (14 in. Lug Spacing) F-15A-E F-16A-D F/A-18A-F AV-8B Contractor / Schedule / Improvements / Special Equipment: Contractor - Empty Bomb Assy - General Dynamics, Garland, Texas / Loaded Bomb Assy McAlester Army Ammunition Plant, McAlester, OK Status Inventory Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT and NAVAIRSYSCOM PMA-201, NAS Patuxent River, MD and Naval Air Warfare Center Weapons Division, China Lake, CA Technical Order: 11A1-6-7, NAVAIR 11-140-5, 11-5A-32

MK 83

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Nomenclature: MK 84

Name: 2,000 lb. GP Bomb

Capability: Attack soft and intermediately protected targets, buildings, rail yards and lines of communications. Description: The MK 84 is designed to attack soft and intermediately protected targets. The destruction mechanism of the MK 84 is blast and fragmentation. Ideal targets for this weapon are buildings, rail yards, and lines of communication. The Navy and the Air Force both use it intensively. Blast sensitive targets, such as POL, motor pools, and troop concentrations, are the primary targets for this weapon. Characteristics: CRD Weapons Code ZCG1B ZRG1L BC47A BC47C SZBGA BR41A BR41B BC46B BC46A BC47B BR41M BC41C BC41A BC41B BC41P ZCG1C ZCG1L BC41R BC41S

MK84 (I) W/O FUZE MK84 AIR (I) W/ F268 MK84 DSU33A/B FMU139 B-2 MK84 DSU33B/B FMU139 MK84 LOW DRAG KIT MK84 R/BSU-50 904 N MK84 R/BSU-50 905 T MK84 W/FMU-139 (T) B-1 MK84 W/FMU-139A/B (N) B-1 MK84 W/M904/905 B-2 MK84/BSU-50 FMU 139A/B (T) MK84C 904 NS MK84C 904/905 N/T MK84C 905 TL MK84C 113/905 MK84C (I) FMU139 TL MK84C DSU33/FMU139 MK84C DSU-33A/B FMU139 MK84C DSU33B/B FMU139

BC41L ZCG1K BC41G BC41H BC47H BC46C BC46D ZC61C ZCG1G ZRG1B ZRG1G BR41N BR41P ZRG1E BR41H BR41I PR41A PR41B PR41C

MK84C FMU 113/B (N) MK84C FMU113/M905 N/T MK84C FMU139A/B (N) MK84C FMU139A/B (T) MK84C FMU-139A/B (T) B-2 MK84C W/DSU-33A/B FMU-139 MK84C W/DSU33B/B FMU-139 MK84C(I) MK84C(I) 904/905 N/T MK84R (I) BSU-50 54/B TL MK84R (I) 904/905 N/T MK84R DSU33A/B FMU139 MK84R DSU33B/B FMU139 MK84R(I) BSU-50 M904 NS MK84R/BSU-50 904/905 N/T MK84R/BSU-50 M904 NS FMU-139 T PREPO ISO MK84/BSU-50/FMU-139 T PREPO ISO MK84/BSU50/FMU139 T PREPO ISO MK84/BSU-50/M904/M905

Guidance - Ballistic Class -

2,000 lb. General Purpose Bomb, Blast/Fragmentation MK 84 LDGP Weight (lbs.) 1,997.22 Length (with nose fuze) (in.) 149.27 Length (without nose fuze) (in.) - 145.37 Diameter (in.) 18.00 Warhead (lbs.) 2,000 Blast/Fragmentation Explosive (NEW) - 945 lbs. H-6 or Tritonal Fuze Variety of mechanical or electrical Stabilizer BSU-50 AIR; MK 84 Conical Fin

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Carriage Options: Aircraft: A-10 B-1B B-2A B-52H F-15A-E F-16A-D F/A-18A-F

Launcher/Rack - Multiple (30 in. Lug Spacing)

Contractor / Schedule / Improvements / Special Equipment: Contractor - Empty Bomb Assy - General Dynamics, Garland, Texas / Loaded Bomb Assy McAlester Army Ammunition Plant, McAlester, OK Status Inventory Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT and NAVAIRSYSCOM PMA-201, NAS Patuxent River, MD and Naval Air Warfare Center Weapons Division, China Lake, CA

Technical Order: 11A1-7-7, NAVAIR 11-140-5, 11-5A-32

MK 84

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Nomenclature: MK 106

Name: 5 lb. Practice Bomb

Capability: Training ordnance to simulate the 500 lb. MK 82 and 2000 lb. MK 84 general purpose, nonguided bombs in a high drag configuration. Description: The MK 106 is a cylindrical shaped practice bomb that utilizes a spotting charge to display target marking. When the bomb is released from the aircraft it free falls until impact. Upon impact the bomb drives a firing pin assembly against a primer activating the signal charge. The resulting flash and puff of smoke permits visual evaluation of accuracy. Characteristics: CRD Weapons Code ZP81B MK106 PRACTICE BOMB/CXU3/B Class Weight (lbs.) Length (in.) Diameter (in.) -

ZP81A

MK106 PRACTICE BOMB/MK 4

5 lb. Practice Bomb 5 21.00 3.88

Carriage Options: Aircraft: F-15E F-16A-D F/A-18A-D

Launcher/Rack - Multiple

Contractor / Schedule / Improvements / Special Equipment: Contractor - General Dynamics Status Inventory Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A3-3-7 (Bomb and CXU-3A/B)

MK 106

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CHAPTER FIVE 1 June 2009

GUIDED BOMB UNITS (GBU)

FOR OFFICIAL USE ONLY

INTENTIONALLY LEFT BLANK

Nomenclature: BDU-59B/B

Name: Laser Guided Training Round (LGTR)

Capability: Paveway II Laser Guided Training Round. Description: The Paveway II BDU-59 Laser Guided Training Round (LGTR) provides realistic Paveway II Laser Guided Bomb (LGB) (GBU-10/12/16) tactical employment training as an alternative to expending operational Paveway II LGB assets. It emulates the laser guided bomb envelope, flight characteristics and guidance system of the Paveway II system. The LGTR is comprised of two sections (Guidance Control Section and Payload Section). The Guidance Control Section consists of the seeker, the signal processor, control system, and power supply. The Payload Section consists of the ring airfoil at the trailing edge which also houses the signal cartridges (MK 4 Mods or CXU-3A/B2) and the ejector assembly. Live-fire training with the Paveway II LGTR permits aircrews to practice delivery tactics in a real-mission environment and experience actual weapon characteristics with today's range limitations. The Paveway II LGTR emulates the GBU-10, -12, and -16 Paveway II LGBs and replicates mission parameters for realistic tactics and employment of the Paveway II system. Characteristics: Guidance Controls Class Weight (lbs.) Length (in.) Diameter (in.) Wing span (in.) Canard span (in.) Shelf Life -

semi-active laser Pneumatically actuated (nitrogen) Practice Bomb 89.00 (+-5) 75 4 19 13 42 months

Carriage Options (Loadout): Aircraft: F/A-18A-F AV-8B

Launcher/Rack: BRU-41/BRU-42 BRU-42

Contractor / Status / Improvements / Special Equipment: Contractor - Lockheed Martin Status Inventory Management/Engineering: NAVAIRSYSCOM PMA-201, NAS Patuxent River, MD

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Technical Order: NA 11-140-10

Paveway II Laser Guided Training Round

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Nomenclature: GBU-10 Series

Name: Laser Guided Bomb (LGB)

Capability: Precision bombing against non-hardened targets. Description: The GBU-10 C/B is a 2,000 lb. class laser guided bomb that uses the MK 84/BLU-117 warhead. The Paveway II system has folding wings that open upon release for increased aircraft payload and maneuverability. This weapon is primarily used for precision bombing against nonhardened targets. Characteristics: CRD Weapons Code BL4SA ZLGCD ZLGCQ ZLGCI ZLGCP ZLGCN ZL9CA BL9CC BL4EB BL4EK BL4CB BL4EA BL4CI BL4EG

Guidance Control Autopilot Class -

GBU-10 PW-II FOR F-117 GBU-10 (I) PW-II 81/905 GBU-10 (I) PW-II W/ F268 GBU-10 (I) PW-II 81/81 N/T GBU-10 (I) PW-II FMU139 T GBU-10 (I) PW-II NO FUZE GBU-10 BLU-109 GBU-10 PW-II FMU-143 LGB GBU-10 PW-II 139 TL F-15E LGB GBU-10 PW-II 139 NS F-15E LGB GBU-10 PW-II 81 NS LGB GBU-10 PW-II 81 NS F-15E LGB GBU-10 PW-II 81 TL LGB GBU-10 PW-II 81 TL F-15E

BL4CN BL4EC BL4EH BL4CD BL4CA ZL6CB ZL6CA BL4CO BL9EC ZL6BF ZL6BE BL4CF PL4CA SZDBA

LGB GBU-10 PW-II 81/81 N/T LGB GBU-10 PW-II 81/81 N/T F-15E LGB GBU-10 PW-II 81/905 F-15E LGB GBU-10 PW-II 81/905 N/T LGB GBU-10 PW-II 905 TL LGB GBU-10 PW-II BDU-56 LGB GBU-10 PW-II BDU-56 F117 LGB GBU-10 PW-II FMU139A/B (T) LGB GBU-10 PW-II FMU-143 F-15E LGB GBU-10 PW-1 /B BDU-56 LGB GBU-10 PW-1 A/B BDU-56 LGB GBU-10 PW-II 139 NS PREPO ISO GBU-10 PW-II/FMU-139 T STAMP GBU-10E/B KIT

Semi-active laser MAU-169 Series (Paveway II); MAU-209 Series; WCU-10 Series (USN) Bang-Bang Mode 2,000 lb. Paveway II Laser Guided Weapons

GBU-10 Model C/B, D/B, E/B GBU-10 Model G/B, H/B, J/B, K/B Weight (lbs.) - 2,110.25 Weight (lbs.) - 2,129.58 Length (in.) - 169.90 Length (in.) - 166.77 Diameter (in.) - 18.00 Diameter (in.) - 14.50 BLU-109/B warhead MK 84/BLU-117 warhead MXU-651 Series Airfoil Long Wing Paveway II Warhead BLU-109/MK 84/BLU-117; Blast/Fragmentation Explosive (NEW) - 535/945 lbs. Tritonal/H6/AFX-795 Fuze FMU-26B/B, FMU-81 (nose, tail), FMU-139 series, or FMU-143 fuze, FMU-152/B will be used when available. Stabilizer MXU-651 (Paveway II)

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Carriage Options: Aircraft: A-10 B-52H F-15E F-16A-D F/A-18A-F

Launcher/Rack: Multiple (30 in. Lug Spacing)

BRU-32

Contractor / Status / Improvements / Special Equipment: Contractor - Raytheon, Lockheed Martin Status Inventory Management/Engineering: 507 CBSS/GBLC, Hill AFB, UT Technical Order: 11K10-2-7, NA 11-140-10

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Nomenclature: GBU-12 Series

Name: Laser Guided Bomb (LGB)

Capability: Precision bombing against non-hardened targets. Description: The GBU-12 B/B is a 500 lb. class laser guided bomb that uses the MK 82/BLU-111 warhead. The Paveway II system has folding wings that open upon release for increased aircraft payload and maneuverability. This weapon is primarily used for precision bombing against nonhardened targets. Characteristics: CRD Weapons Code BL2CI BL2CD BL2EG BL2CK BL2EE BL2CR BL2ED BL2CP BL2CL BL2CS BL2EK BL2EL

LGB GBU-12 PW-II 81 TL LGB GBU-12 PW-II 81/905 N/T LGB GBU-12 PW-II 139 (N) F-15E LGB GBU-12 PW-II 81 NS LGB GBU-12 PW-II 81 NS F-15E LGB GBU-12 PW-II 81 NS F117 LGB GBU-12 PW-II 81 TL F-15E LGB GBU-12 PW-II 81 TL F117 LGB GBU-12 PW-II 81/81 N/T LGB GBU-12 PW-II 81/81 N/T F117 LGB GBU-12 PW-II 81/81 N/T F-15E LGB GBU-12 PW-II 81/905 F-15E

Guidance Control Air Foil Group Autopilot Class Weight (lbs.) Length (in.) Diameter (in.) Warhead Explosive (NEW) Fuze Stabilizer Carriage Options: Aircraft: A-10 AV-8B B-52H F-15E F-16A-D F/A-18A-F F-35 MQ-9

BL2CC BL2CA BL2EA ZL5CB ZL5CA BL2CM BL2CT BL2EI BL2CB SZEBA PL2CA

LGB GBU-12 PW-II 81/905 NT F117 LGB GBU-12 PW-II 905 TL LGB GBU-12 PW-II 905 TL F-15E LGB GBU-12 PW-II BDU-50 LGB GBU-12 PW-II BDU-50 F117 LGB GBU-12 PW-II FMU139A/B (T) LGB GBU-12 PW-II FMU-139A/B F117 LGB GBU-12 PW-II FMU-139T F-15E LGB GBU-12 PW-II TL F117 STAMP GBU-12E/B KIT PREPO ISO LGB GBU-12/FMU-139 T

Semi-Active Laser MAU-169 Series (Paveway II); MAU-209 Series; WCU-10 Series (USN) MXU-650 Series Bang-Bang Mode 500 lb. Paveway II Guided Weapon 606.67 131.15 10.75 (Warhead) 18 in. (Airfoil Group) MK 82/BLU-111 Blast/Fragmentation Tritonal, H-6, PBXN-109 (192 lbs.) FMU-81 Tail or FMU-139 MXU-650 Series (Paveway II)

Launcher/Rack: Multiple (14 in. Lug Spacing) BRU-36/BRU-42

BRU-32/BRU-33 BRU-15/A (modified)

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Contractor / Status / Improvements / Special Equipment: Contractor - Raytheon, Lockheed Martin Status Inventory Management/Engineering: 507 CBSS/GBLC, Hill AFB, UT Technical Order: 11K1-9-06, NA 11-140-10

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Nomenclature: GBU-12F/B

Name: Dual Mode Laser Guided Bomb (DMLGB)

Capability: Precision bombing against non-hardened targets. Description: The GBU-12F/B is a 500 lb. class laser guided bomb that uses the MK 82/BLU-111 warhead. It enhances existing LGB kits by adding GPS/INS guidance capability. DMLGB Kits consist of a Computer Control Group (CCG), Adapter Group (ADG), and an Airfoil Group. The Paveway II system has folding wings that open upon release for increased aircraft payload and maneuverability. This weapon is primarily used for precision bombing against non-hardened targets. Characteristics: Guidance Control Air Foil Group Autopilot Class Weight (lbs.) Length (in.) Diameter (in.) Warhead Explosive (NEW) Fuze Stabilizer -

Semi-Active Laser, GPS/INS WGU-53/B MXU-650 Series Bang-Bang Mode 500 lb. Paveway II Guided Weapon 610.67 131.15 10.75 (Warhead) 18 in. (Airfoil Group) MK 82/BLU-111 Blast/Fragmentation Tritonal, PBXN-109 (192 lbs.) FMU-139 Series MXU-650 Series (Paveway II)

Carriage Options: Aircraft: F/A-18A-F AV-8B

Launcher/Rack: BRU-32/BRU-55 BRU-36

Contractor / Status / Improvements / Special Equipment: Contractor - Lockheed Martin Status Inventory Management/Engineering: NAVAIRSYSCOM PMA-201, NAS Patuxent River, MD Technical Order: NA 11-140-10

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Nomenclature: GBU-15

Name: Guided Standoff Weapon

Capability: Precision bombing against hardened and non-hardened targets. Description: The GBU-15 is a 2,000 lb. class guided bomb that uses a MK 84 blast fragment or a BLU-109 penetrating warhead fitted with a set of aerodynamic lifting and control surfaces and either a TV seeker or an IR seeker. The GBU-15 is normally deployed in the indirect mode where a weapon is launched towards the target without lock on. The GBU-15 can be used in the buddy mode where one A/C launches the weapon and the other A/C performs the control functions. The datalink pod transmits command signals to the weapon receiver/transmitter (RxTx) and receives video signal from the weapon RxTx. The command signal allows the WSO to control and redirect the weapon during delivery to the target. The AN/GJM-64 test system tests all GBU-15 and AGM-130 configurations; it is completely menu driven featuring minimal manual operator intervention. Characteristics: CRD Weapons Code ZG9GB BG6GA BGHGA BG6GB BG4GA BGGGA BGGGB BG9GB BG4GB BG6TA BG6TB

GBU-15 (T-1)/B IR CAPTIVE CARRY GBU-15 IR BDU-56/TAC/INERT GBU-15 IR BLU109(I)/TAC/INERT GBU-15 IR/BDU-56/TAC/INERT GBU-15 IR/LONG CHORD/MK84 GBU-15 IR/MK84(I)/TAC/INERT GBU-15 IR/MK84(I)/TAC/INERT GBU-15 IR/SHORT CHORD/BLU109 GBU-15 IR/SHORT CHORD/MK84 GBU-15 TV/BDU-56/TAC/INERT GBU-15 TV/BDU-56/TAC/INERT

BG6TC BG6TD BGHTA BGHTB BG4TD BG4TA BGGTA BG4TB BG9TB BG9TA BG4TC

GBU-15 TV/BDU-56/TAC/INERT GBU-15 TV/BDU-56/TAC/INERT GBU-15 TV/BLU-109(I)/TAC/INERT GBU-15 TV/BLU-109(I)/TAC/INERT GBU-15 TV/LC/SFOV/MK84 GBU-15 TV/LONG CHORD/MK84 GBU-15 TV/MK84(I)/TAC/INERT GBU-15 TV/SC/SFOV MK84 GBU-15 TV/SC/SFOV/BLU109 GBU-15 TV/SC/SFOV/BLU-109 GBU-15 TV/SC/SFOV/MK84

Guidance Control -

Electro Optical TV; Imaging IR (day or night), Vertical Targets Automatic or Manual (Weapon System Operator (WSO) via w/ AXQ-14 or ZSW-1 Datalink Pod) Autopilot - Analog Class 2,000 lb. Standoff Warhead - MK 84, BLU-109 (adapter kit required), or BLU-121 Explosive - Tritonal - 945 lbs. (MK 84); 535 lbs. (BLU-109) - AFX-757 - 978 lbs. (BLU-121) Fuze FMU-124A/B (MK 84, nose and tail); FMU-143 (BLU-109 and BLU-121, tail only); Integrating FMU 152 (JPF) tail only with BLU-109 Stabilizer - Strakes/Canards, Wings; Long Chord (LCW) or Short Chord (SCW) and Control Surfaces Datalink OA-8921/AXQ-14 (weapon terminal) Range 5-15+ NM Diameter - (guidance section) 15.0 in. Diameter - (control section) 16.0 in. Diameter - (wing) 59.0 in.

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FOUO

GBU-15(V) 1/B (MK 84, TV, LCW) Weight (lbs.) - 2,476.00 Length (in.) - 156.0 Diameter (in.) - 18.00

GBU-15(V) 1/B (MK 84, TV, SCW) Weight (lbs.) - 2,410.00 Length (in.) - 156.0 Diameter (in.) - 18.00

GBU-15(V) 2/B (MK 84, IR, LCW) Weight (lbs.) - 2,515.00 Length (in.) - 159.0 Diameter (in.) - 18.00

GBU-15(V) 2/B (MK 84, IR, SCW) Weight (lbs.) - 2,449.00 Length (in.) - 159.00 Diameter (in.) - 18.00

GBU-15(V) 31B (BLU-109, TV, SCW) Weight (lbs.) - 2,486.00 Length (in.) - 156.00 Diameter (in.) - 16.00

GBU-15(V) 32B (BLU-109, IR, SCW) Weight (lbs.) - 2,525.00 Length (in.) - 156.00 Diameter (in.) - 16.00

Carriage Options: Aircraft: F-15E

Launcher/Rack: BRU-47 (30 in. Lug Spacing)

Contractor / Status / Improvements / Special Equipment: Contractor Boeing North American Status Inventory Improvements Potential Integration of FMU-152 (JPF) Fuze Real Time Information in Cockpit (RTIC) via Goldstrike POD Special Equipment - AN/GJM-64 Field Test System (33D7-77-81-1), Ground Support Equipment (33D9-148-3-1), and Shipping and Storage Containers (35E20-2-43-2) Management/Engineering: 507 CBSS/GBLB, Hill AFB, UT Technical Order: 11K15-2-7

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Nomenclature: EGBU-15

Name: Enhanced Guided Standoff Weapon

Capability: Global Positioning System aided Internal Navigation System (GAINS) Precision bombing against hardened and non-hardened targets and tunnels. Description: The enhanced versions of the GBU-15 weapon system includes a Global Positioning System/Internal Navigation System (GPS/INS) also known as a GAINS, man-in-the-loop capabilities, and guidance and navigation capability. The primary purpose of the GAINS is to provide enhanced capability in weather. Like the GBU-15 it is normally deployed in the indirect mode where a weapon is launched towards the target without lock on, with the datalink pods transmitting WSO commands and receiving weapon video. The GAINS reduces the WSO workload by allowing the weapon to autonomously fly until the target or target area is within the field of view. The AN/GJM-64 test system tests all EGBU-15 configurations; it is completely menu driven featuring minimal manual operator intervention. The software can be readily modified to facilitate testing/updating of new weapon versions, enhancements, improvements and modification with the AN/GJM-64. Characteristics: CRD Weapons Code ZE65B BE65B ZE65A BE65A ZE95B BE95B ZE95A BE95A ZEG5B

GBU-15 BDU-56 GPS IR CAP F-15E GBU-15 BDU56 GPS IR TAC INRT F15 GBU-15 BDU-56 GPS TV CAPT F-15E GBU-15 BDU56 GPS TV TAC INRT F15 GBU-15 BLU109 GPS IR LD/TRN F-15 GBU-15 BLU-109 GPS IR TACT F-15E GBU-15 BLU109 GPS TV LD/TRN F-15 GBU-15 BLU-109 GPS TV TACT F-15E GBU-15 MK84 GPS IR LD/TRNR F-15E

BE85B BE45B ZEG5A BEG5A BE45A ZE45B ZE45A BEG5B BE85A

GBU-15(V)34/B BLU-118 GPS IR GBU-15 MK84 GPS IR TACT F-15E GBU-15 MK84 GPS TV LD/TRNR F-15E GBU-15 MK84 GPS TV TAC/INRT F-15 GBU-15 MK84 GPS TV TACT F-15E GBU-15 MK84(EMPTY) GPS IR F-15E GBU-15 MK84(EMPTY) GPS TV F-15E GBU-15 MK84 GPS IR TAC/INRT F-15 GBU-15(V)33/B BLU-118 GPS TV

Guidance -

Electro Optical TV; Imaging IR, GPS/INS, Precise Adverse Weather, day or night Accurate all Weather, Vertical Targets Control Automatic or Manual (Weapon System Operator (WSO) via w/ AXQ-14 or ZSW-1 Datalink Pod) Autopilot - Analog Class 2,000 lb. Standoff Warhead - MK 84, BLU-109 (adapter kit required), or BLU-121 Explosive - Tritonal - 945 lbs. (MK 84); 535 lbs. (BLU-109) - AFX-757 - 978 lbs. (BLU-121) Fuze FMU-124A/B (MK 84, nose and tail); FMU-143 (BLU-109 and BLU-121, tail only); Integrating FMU 152 (JPF) tail only with BLU-109 Stabilizer - Strakes; Wings, Long Chord (LCW) or Short Chord (SCW); and Control Surfaces Datalink OA-8921B & C/AXQ-14 (weapon terminal) Range 5-15+ NM Diameter - (guidance section) 15.0 in. Diameter - (control section) 16.0 in. Diameter - (wing) 59.0 in.

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GBU-15(V) 1C/B (MK 84, TV, GPS/INS, SCW) Weight (lbs.) - 2,430.00 Length (in.) - 156.00 Diameter (in.) - 18.00

GBU-15(V) 2C/B (MK 84, IR, GPS/INS, SCW) Weight (lbs.) - 2,469.00 Length (in.) - 159.00 Diameter (in.) - 18.0

GBU-15(V) 31A/B (BLU-109, TV, GPS/INS, SCW) Weight (lbs.) - 2,506.00 Length (in.) - 156.00 Diameter (in.) - 16.0

GBU-15(V) 32A/B (BLU-109, IR, GPS/INS, SCW) Weight (lbs.) - 2,545.00 Length (in.) - 159.00 Diameter (in.) - 16.00

Carriage Options: Aircraft: F-15E

Launcher/Rack: BRU-47 (30 in. Lug Spacing)

Contractor / Status / Improvements / Special Equipment: Contractor Boeing North American; Raytheon Systems for Enhancement Status Inventory Improvements Potential Integration of FMU-152 (JPF) Fuze Real Time Information in Cockpit (RTIC) via Goldstrike POD BLU-121/B Bomb, explosive filler - AFX757, 978 lbs NEW Special Equipment - AN/GJM-64 Field Test System (33D7-77-81-1), Ground Support Equipment (33D9-148-3-1), and Shipping and Storage Containers (35E20-2-43-2) Management/Engineering: 507 CBSS/GBLB, Hill AFB, UT Technical Order: 11K15-2-7

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Nomenclature: GBU-16 Series

Name: Laser Guided Bomb (LGB)

Capability: Precision bombing against non-hardened targets; mobile hard and fixed soft and hard targets. Description: The Guided Bomb Unit-16 (GBU-16) utilizes a 1,000 lb. general purpose warhead. The operator illuminates a target with a laser designator and then the munition guides to a spot of laser energy reflected from the target. The GBU-16 consists of a MK 83/BLU-110 1,000 lb bomb modified with a common Paveway II laser guidance kit. Characteristics: Guidance Control Air Foil Group Autopilot Class Weight Length Diameter Warhead Explosive (NEW) Fuze Stabilizer Carriage Options: Aircraft: F/A-18A-F AV-8B

Semi-Active Laser MAU-169 Series (Paveway II), MAU-209 Series; WCU-10 Series (USN) MXU-667 Series Bang-Bang Mode 1,000 lb. Paveway II Guided Weapon 454kg 3.68m 350mm (Warhead); 18 in. (Airfoil Group) 72m closed, 1.68m extended MK 83/BLU-110 Blast/Fragmentation Tritonal, H-6, PBXN-109 (202kg) FMU-81 Tail or FMU-139 MXU-667 Series (Paveway II)

Launcher/Rack: BRU-32/BRU-33 BRU-36

Contractor / Status / Improvements / Special Equipment: Contractor - Raytheon, Lockheed Martin Status Inventory Management/Engineering: 507 CBSS/GBLC, Hill AFB, UT; NAVAIRSYSCOM PMA-201, NAS Patuxent River, MD Technical Order: 11K1-9-06, NA 11-140-10

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Nomenclature: GBU-24/B

Name: Low Level Laser Guided Bomb (LGB)

Capability: Precision attack to destroy soft and intermediately protected targets, aircraft shelters, and concrete structures. Description: This 2,000 lb. class weapon was designed as a precision guided blast/fragmentation MK 84 bomb, fitted with a nose mounted laser guidance and control unit, and the new Paveway III tail assembly. The GBU-24/B can be released at low, medium or high altitudes. Low altitude can mean “tree top” height if deemed necessary. The laser designation works through a pulsecoding system that supplies the same code for both the seeker and the designator so that the bomb tracks only the intended target. Characteristics: CRD Weapons Code ZL9BD BL4HP BL4HB BL4HR BL4HI BL4HA BL4HS BL4DI BL4HL BL4DN BL4DL BL4HM BL4DO BL4DQ BL9HD BL9HE BL4DP BL4DB BL4HN BL4DD BL4DC BL4HO

GBU-24 A/B GBU-24 PW-III 139 N WGU-39 F-15E GBU-24 PW-III 139 T WGU-39 F-15E GBU-24 PW-III 81 NS WGU-39 F-15E GBU-24 PW-III 81 NT WGU-12 F-15E GBU-24 PW-III 81 NT WGU-39 F-15E GBU-24 PW-III 81 TL WGU-39 F-15E GBU-24 PW-III FMU-139 NS GBU-24 PW-III FMU-139 NS F-15E GBU-24 PW-III FMU-139 NS WGU39/B GBU-24 PW-III FMU-139 TL GBU-24 PW-III FMU-139 TL F-15E GBU-24 PW-III FMU-139 TL WGU-39 GBU-24 PW-III FMU-139 TL WGU-39 GBU-24 PW-III FMU-143 F-15E GBU-24 PW-III FMU-143 F-15E GBU-24 PW-III FMU-81 N/T WGU-39 GBU-24 PW-III FMU-81 NS GBU-24 PW-III FMU-81 NS F-15E GBU-24 PW-III FMU-81 NS WGU-39 GBU-24 PW-III FMU-81 TL GBU-24 PW-III FMU-81 TL F-15E

Guidance Control Autopilot Class Weight (lbs.) Length (in.) Diameter (in.) Warhead Explosive (NEW) Fuze Stabilizer -

BL4DG BL4DA BL9DC BL9DE ZLG1N ZLG1I ZLG1G ZLG1F ZLG1K ZL6DB ZL6DD ZLGDA ZL9BB ZL9BF ZL9DC ZL9HA PL4HA PL9DA SZFDA SZFBA

GBU-24 PW-III FMU-81 TL WGU-39 GBU-24 PW-III FMU-81 (N/T) WGU-12 GBU-24 PW-III WGU-12/FMU-143 GBU-24 PW-III WGU-39/FMU-143 GBU-24 WGU-12 NO FUZE GBU-24/B (I) GBU-24/B WGU12 FMU139 GBU-24/B WGU12 FMU81 TL GBU-24/B WGU-12 NO FUZE GBU-24/B WGU-12 (D-2)/B NO FUZE GBU-24/B WGU-12B/B NO FUZE GBU-24/B WGU-39 NO FUZE GBU-24A/B (I) FMU-143 T GBU-24A/B WGU-39 (D-2)/B FMU-143 GBU-24A/B WGU-39/B GBU-24A/B WGU-39/B FMU-143 F-15 PREPO ISO GBU-24/FMU-139/WGU-39 PREPO ISO GBU-24/WGU-39/FMU-143 STAMP GBU-24/B SUPER BOLT KIT STAMP GBU-24A/B SUPER BOLT KIT

Semi-Active Laser (WGU-12 or WGU-39 Guidance Unit) Nose Fins Proportional Guidance 2000 lb. Blast/Fragmentation 2,256.75 172.76 18.00 MK 84 Blast/Fragmentation 945 lbs. Tritonal FMU-81 Nose & Tail (See Appendix A) SU-84 Fin Assembly

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Carriage Options: Aircraft: F-15E F-16A-D

Launcher/Rack: Multiple (30 in. Lug Spacing)

Contractor / Status / Improvements / Special Equipment: Contractor - Raytheon Status Inventory Management/Engineering: 507 CBSS/GBLC, Hill AFB, UT Technical Order: 11K20-2-7

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Nomenclature: GBU-24A/B

Name: Low Level Laser Guided Bomb (LGB)

Capability: Precision attack to destroy hardened targets, aircraft shelters, and concrete structures. Description: Designed as a precision 2,000 lb. class guided penetration bomb, the GBU-24 A/B is basically a BLU-109 warhead fitted with a nose mounted laser guidance and control unit and the new Paveway III tail assembly. This weapon can be released at low, medium, or high altitudes. Low altitude can mean “tree top” height if deemed necessary. Characteristics: CRD Weapons Code See GBU-24/B (Page 5-12) Control Nose Fins Autopilot Proportional Guidance Class 2,000 lb. Penetrator Weight (lbs.) 2,372.75 Length (in.) 169.69 Diameter (in.) 14.50 Fin. Span (Canards) (in.) 39.25 Fin. Span (wings stowed) (in.) - 36.0 Fin. Span (wings deployed) (in.) - 81.6 Warhead BLU-109/B Hard Target Penetrator Explosive (NEW) 535 (lbs.) Tritonal Fuze FMU-143 Series (Tail); (See Appendix A) Stabilizer BSU-84 Fin Assembly Carriage Options: Aircraft: F-15E F-16A-D

Launcher/Rack: Multiple (30 in. Lug Spacing)

Contractor / Status / Improvements / Special Equipment: Contractor - Raytheon Status Inventory Management/Engineering: 507 CBSS/GBLC, Hill AFB, UT Technical Order: 11K20-2-7

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Nomenclature: GBU-24B/B

Name: Low Level Laser Guided Bomb (LGB)

Capability: Precision attack to destroy hardened targets, aircraft shelters, and concrete structures. Description: Designed as a precision 2,000 lb. class guided penetration bomb, the GBU-24 B/B consists of five major sections: (1) Guidance and Control Unit (CGU) WGU-39/B; (2) Airfoil Group (AFG) BSU-84/B; (3) Adapter Group (ADG) ADG-770/B; (4) Bomb Fuze system FMU-143E/B and (5) 2,000 Pound Penetrator Bomb BLU-109A/B. This weapon can be released at low, medium, or high altitudes. Low altitude can mean “tree top” height if deemed necessary. Characteristics: Control Nose Fins Autopilot Proportional Guidance Class 2,000 lb. Penetrator Weight (lbs.) 2,372.75 Length (in.) 169.69 Diameter (in.) 14.50 Fin. Span (Canards) (in.) 39.25 Fin. Span (wings stowed) (in.) - 36.0 Fin. Span (wings deployed) (in.) - 81.6 Warhead BLU-109A/B Hard Target Penetrator Explosive (NEW) 535 (lbs.) PBXN-109 Fuze FMU-143E/B (Tail) Stabilizer BSU-84/B or BSU-84A/BFin Assembly Carriage Options: Aircraft: F/A-18A-F

Launcher/Rack BRU-32

Contractor / Status / Improvements / Special Equipment: Contractor - Raytheon Status Inventory (Navy) Management/Engineering: NAVAIRSYSCOM PMA-201, NAS Patuxent River, MD Technical Order: NAVAIR 11-140-10

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FOUO

Nomenclature: GBU-24E/B and G/B

Name: Low Level Laser Guided Bomb (LGB)

Capability: Precision attack to destroy hardened targets, aircraft shelters, and concrete structures. Description: Designed as a precision 2,000 lb. class guided penetration bomb, the GBU-24 E/B and GBU24G/B consists of five major sections: (1) Guidance and Control Unit (CGU) WGU-39A/B; (2) Airfoil Group (AFG) BSU-84B/B; (3) Adapter Group (ADG) ADG-770A/B; (4) Bomb Fuze system FMU-143 series and (5) 2,000 Pound Penetrator Bomb BLU-109A/B or BLU-116 A/B. This weapon can be released at low, medium, or high altitudes. Low altitude can mean “tree top” height if deemed necessary. Characteristics: Control Nose Fins Autopilot Proportional Guidance Class 2,000 lb. Penetrator Weight (lbs.) 2,372.75 Length (in.) 169.69 Diameter (in.) 14.50 Fin. Span (Canards) (in.) 39.25 Fin. Span (wings stowed) (in.) - 36.0 Fin. Span (wings deployed) (in.) - 81.6 Warhead BLU-109A/B (GBU-24E/B) or BLU-116A/B (GBU-24G/B) Hard Target Penetrator Explosive (NEW) 535 (lbs.) PBXN-109 (BLU-109A/B) or 115 (lbs.) PBXN-109 (BLU-116A/B) Fuze FMU-143 Series Stabilizer BSU-84B/B Fin Assembly Carriage Options: Aircraft: F/A-18A-F

Launcher/Rack BRU-32

Contractor / Status / Improvements / Special Equipment: Contractor - Raytheon Status Inventory (Navy) Management/Engineering: NAVAIRSYSCOM PMA-201, NAS Patuxent River, MD Technical Order: NAVAIR 11-140-10

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FOUO

Nomenclature: GBU-27/GBU-27A/B

Name: GPS/INS/Laser Guided Bomb (LGB)

Capability: Destroy hardened targets. Description: The Guided Bomb Unit-27 (GBU-27) is a GBU-24 modified for delivery by the F-117A stealth fighter. The operator illuminates a target with a laser designator and then the munition guides to a spot of laser energy reflected from the target. It uses a 2,000 lb. penetrating warhead against hard targets. The GBU-27 is laser guided only; the GBU-27A/B also incorporates a GPS/INS capability. Characteristics: CRD Weapons Code ZL9SD ZL9DB ZL9DA ZL9SA BL9SH BL9SF BL9SA

GBU-27 PW-III INERT W/O FUZ F117 GBU-27 PW-III INERT W/O FUZE GBU-27 PW-III W/FUZE GBU-27 PW-III W/FUZE F117 GBU-27 PW-III WGU25/FMU143 F117 GBU-27 PW-III WGU-39/FMU-143 GBU-27 PW-III WGU-39/FMU143 F117

ZL9SC BL9DA BL9SC BL9SB SZGBA PL9SA SZGDA

GBU-27 W/O FUZE F117 GBU-27/B FMU-157/B GBU-27A/B FMU-143 WGU-39A/B F117 GBU27A/B FMU143B/B WGU39A/B F117 STAMP GBU-27 KIT (F-117) PREPO ISO GBU-27/WGU-39/FMU-143 STAMP ENHANCED GBU-27 KIT

Guidance -

WGU-25/B, WGU-25A/B or WGU-39/B Guidance Unit or WGU-39A/B GPS Laser Guidance Unit Control Nose Fins Autopilot None Class 2,000 lb. GBU Weight (lbs.) 2,185.00 Length (in.) 166.77 Diameter (in.) 14.50 Warhead BLU-109/B Hard Target Penetrator Explosive (NEW) - 535 lbs. Tritonal Fuze FMU-143 Series (See Appendix A) Stabilizer BSU-88 Series Fin Assembly Carriage Options: Aircraft: F-15E F-16C-D

Launcher/Rack: N/A (30 in Lug Spacing)

Contractor / Status / Improvements / Special Equipment: Contractor - N/A Status Inventory Management/Engineering: 507 CBSS/GBLC, Hill AFB, UT Technical Order: 11K25-2-7

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Nomenclature: GBU-28A/B & B/B

Name: GPS/INS/Laser Guided Bomb (LGB)

Capability: Defeat hard and deeply buried targets (HDBT). Description: The Guided Bomb Unit-28 (GBU-28) is a special weapon developed for penetrating hard and deeply buried targets. The GBU-28 is a 5,000 lb. laser-guided conventional munition that uses a 4,500 lb penetrating warhead. The GBU-28 A/B is laser guided only whereas the GBU-28 B/B also incorporates a GPS/INS capability. Characteristics: CRD Weapons Code ZLH5A GBU-28 INERT F-15E BL5DD GBU-28 W/ FMU-143/F BL5DE GBU-28 W/ FMU-143/G BL5DF GBU-28 W/ FMU-143/H Guidance WGU-36 A/B Laser Guidance Unit or WGU-36B/B GPS/Laser Guidance Unit Control Nose Fins Autopilot None Class 5,000 lb. Penetrator Weight (lbs.) 4,800 Length (in.) 229.31 Diameter (in.) 14.50 Warhead BLU-113/B or BLU-113A/B, Blast/Fragmentation Explosive (NEW) - Tritonal 625 lbs. Fuze FMU-143 Series installed in aft end Stabilizer BSU-92 Series Fin Assembly Carriage Options: Aircraft: B-2A (GBU-28 A/B or B/B) B-52H (GBU-28 A/B) F-15E (GBU-28 A/B)

Launcher/Rack: Multiple (30 in. Lug Spacing)

Contractor / Status / Improvements / Special Equipment: Contractor - Raytheon (guidance), Ellwood National Forge (warhead), UNICOR (shipping pallets), McAlester Army Ammunition Plant (explosive load) Status Inventory Management/Engineering: 507 CBSS/GBLC, Hill AFB, UT Technical Order: 11K28-2-7

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Nomenclature: GBU-28C/B

Name: GPS/INS/Laser Guided Bomb

Capability: Defeat hard and deeply buried targets (HDBT). Description: The Guided Bomb Unit-28C/B (GBU-28C/B) is a special weapon developed for penetrating hard and deeply buried targets using an improved 4,450 lb. warhead, the BLU-122/B. The GBU-28C/B is an enhanced PAVEWAY III weapon with laser as well as GPS/INS guidance capability. Characteristics: Guidance Control Class Weight (lbs.) Length (in.) Diameter (in.) Warhead Explosive (NEW) Fuze Stabilizer -

WGU-36 D/B Guidance Control Unit; GPS/INS/Laser Nose Fins 5,000 lb. Penetrator 4,710 233 15.3 BLU-122/B Blast/Fragmentation AFX-757 (785 lbs.) FMU-143 Series and FMU-152A/B BSG-92B/B Air-Foil Group

Carriage Options (Loadout): Aircraft: B-2A F-15E

Launcher/Rack: Rotary Launcher using BRU-44 BRU-47

Contractor / Status / Improvements / Special Equipment: Contractor - Raytheon (Enhanced PAVEWAY III kits), General Dynamics-Ordnance and Tactical Systems (Warhead), Muskogee Metal Works (Pallets) Status Production Special Equipment - N/A Management/Engineering: 507 CBSS/GBLC, Hill AFB, Utah Technical Order: 11K28-2-7, 11A1-11-7

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Nomenclature: GBU-28E/B

Name: GPS/INS/Laser Guided Bomb (LGB)

Capability: Defeat hard and deeply buried targets (HDBT). Description: The Guided Bomb Unit-28 E/B (GBU-28) is a special weapon developed for penetrating hard and deeply buried targets. The GBU-28 E/B is a 5,000 lb. conventional munition that uses a 4,500 lb penetrating warhead. The GBU-28 E/B is laser guided and incorporates GPS/INS, Selective Availability Anti-Spoofing Module (SAASM) and Impact Angle Control capability. Characteristics: Guidance Control Autopilot Class Weight (lbs.) Length (in.) Diameter (in.) Warhead Explosive (NEW) Fuze Stabilizer Carriage Options: Aircraft: B-2A F-15E

WGU-36 E/B Laser Guidance Unit Nose Fins None 5,000 lb. Penetrator 4,800 229.31 14.50 BLU-113/B or BLU-113A/B, Blast/Fragmentation Tritonal 625 lbs. FMU-143 Series installed in aft end BSU-92 D/B Control Fin Assembly Launcher/Rack: Multiple (30 in. Lug Spacing)

Contractor / Status / Improvements / Special Equipment: Contractor - Raytheon (guidance), Ellwood National Forge (warhead), UNICOR (shipping pallets), McAlester Army Ammunition Plant (explosive load) Status Inventory Jan 09 Management/Engineering: 507 CBSS/GBLC, Hill AFB, UT

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Nomenclature: GBU-31

Name: Joint Direct Attack Munition (JDAM)

Capability: Accurate adverse weather guided munitions for use on conventional strike environments to destroy fixed and relocatable targets. Description: The Joint Direct Attack Munition (JDAM) is a Guidance Set, KMU-556, KMU-557, and KMU-558 Series that converts existing unguided free-fall 2,000 lb bombs, MK 84 and BLU-117, and BLU-109 2000 lb. class warheads into accurate, adverse weather "smart" munitions. The Guidance Set consists of a Tail Kit, which contains an Inertial Navigational System (INS) and a Global Positioning System (GPS), a set of Aerosurfaces and an Umbilical Cover, which allows the JDAM to improve the accuracy of unguided, general purpose bombs in any weather condition. The KMU-5XXB/B configurations are equipped with a Selective Availability AntiSpoofing Module (SAASM) added to existing Tail Kits. The SAASM electronics module is capable of utilizing new GPS security features. The KMU-5XXC/B configurations are equipped with Anti-Jamming (AJ) equipment consisting of a new antenna and associated electronics on the Tail Kit. Anti-Jamming variants allow the JDAM to navigate with precision using GPS signals in regions containing active GPS jamming. JDAM can be launched from very low to very high altitudes in a dive, toss and loft or in straight and level flight with an on-axis or off-axis delivery. JDAM enables multiple weapons to be directed against single or multiple targets on a single pass. JDAM is a joint U. S. Air Force and Department of Navy program. Characteristics: CRD Weapons Code BJ41A BJ41B BJ41C BJ41D BJ41E BJ41F BJ41G BJ41H BJ41J BJ41K BJ41L BJ41M BJ45A BJ46A BJ46B BJ46D BJ46E BJ46F BJ46G BJ46J BJ47B BJ47C BJ47E BJ47H

GBU-31(V)1/B FMU-152A/B GBU-31(V)1/B FMU-113 N GBU-31(V)1/B W/FMU-139A/B (T) GBU-31(V)1/B W/FMU-139A/B (N/T GBU-31(V)1/B DSU-33A/B FMU152A GBU-31(V)1/B DSU-33C/B FMU-152 GBU-31(V)1/B DSU-33C/B FMU-139 GBU-31(V)1/B DSU33A/B FMU139 GBU-31(V)1/B AJ, W//FMU-139 C/B GBU-31(V)1 AJ, DSU-33C/B FMU-139 GBU-31(V)1 AJ, DSU-33A/B FMU-152 GBU-31(V)1 AJ, W/FMU-152 GBU-31(V)1/B FMU-139 T F-15 GBU-31(V)1/B W/FMU-139A/B N/T GBU-31(V)1/B W/FMU-139A/B (T) GBU-31(V)1/B DSU33A/B FMU-152A GBU-31(V)1/B FMU-152A/B B-1 GBU-31V1/B DSU-33C/B B/B FMU139 GBU-31V1/B DSU-33C/B FMU-152A GBU-31V1/B DSU-33A/B FMU139 BGBU-31(V)1/B W/FMU-139A/B (T) GBU-31(V)1/B W/FMU-139A/B(N/T) GBU-31(V)1/B FMU-152A/B B-2 GBU-31(V)1/B DSU-33C/B B/BFMU139

BJ91B BJ91C BJ91D BJ91Z BJ96A BJ96B BJ97A BJ97B BJ97C BJ97D BJ97E ZJ61A ZJ91A ZJ91B ZJ91C ZJ91D ZJ96A ZJ96B ZJ96C ZJ97B ZJ97C ZJG1A ZJG1B ZJG1C

5-22

GBU-31(V)3/B FMU-152A/B GBU-31 (V3) AJ, FMU-143B/B GBU-31 (V)3, AJ FMU-152A/B GBU-31(V)3/B W/FMU-143B/B GBU-31(V)3/B W/FMU-143B/B B-1 GBU-31(V)3/B FMU-152A/B B-1 US GBU-31(V)3/B W/FMU-143B/B B2 GBU-31(V)3/B FMU-152A/B B-2 US GBU-31(V)3/B FMU-143H/B B-2 GBU-31(V)3/B FMU-143G/B B-2 GBU-31(V)3/B FMU-143F/B B-2 GBU-31(V)1/B BDU-56 GBU-31(V)3/B W/FMU-139(D-1)A/B GBU-31(V)3/B FMU-152A(D-2)/B GBU-31(V)3/B W/FMU-143B(D-2)B GBU-31(V)3/B GBU-31(V)3/B W/FMU-139(D-2)B B-1 GBU-31(V)3/B W/FMU-143(D-2)B B-1 GBU-31(V)3/B FMU-152A(D-2)/B B GBU-31(V)3/B W/FMU-143(D-2) B-2 GBU-31(V)3/B FMU-152A(D-2)/B B GBU-31(V)1/B W/FMU-139 INERT T GBU-31(V)1 DSU33C/BFMU152A(D-2 GBU-31(V1)/B INERT

FOUO

BJ47K BJ61A BJ65A BJ66A BJ67A BJ91A

GBU-31(V)1/B DSU33A/B FMU139 B GBU-31(V)5/B FMU-139 T GBU-31(V)5/B FMU-139 T F-15 GBU-31(V)5/B FMU-139 T B-1 GBU-31(V)5/B FMU-139 T B-2 GBU-31(V)3/B W/FMU-143B/B

ZJG1D ZJG1E ZJG1F ZJG1G ZJG1H

GBU-31(V)1/B FMU-139(D-2) GBU-31(V)1/B FMU-139(D-2) N/T GBU-31(V)1/B FMU-152A(D-2)/B GBU-31 KMU-556(D-2) FMU-139(DGBU-31 V1 D-2 INERT BDU-56

Guidance Control Autopilot Class Weight (lbs.) -

NS/GPS Tail Aerodynamic Proportional Guidance 2,000 lb. Guided Munition MK 84 (AF-2039), BLU-109 (AF-2118; Navy-2138), BLU-117 (AF-NA; Navy-2059) Length (in.) MK 84 - 152.7; BLU-109 - 148.6; BLU-117 - 152.7 Diameter (in.) - 25 Warhead MK 84, BLU-109, or BLU-117 Explosive MK 84 945 lbs. Tritonal, BLU-109 535 lbs. Tritonal, BLU-117 945 lbs. IM PBXN-109 Fuze FMU-139 or FMU-143 or FMU-152 Sensor DSU-33 (MK 84 Only) JDAM 2,000 LB NOMENCLATURE/ GBU 31: MK 84 BLU-109 USAF (v) 1/ Series (v) 3/ Series Navy (v) 2/ Series (v) 4/ Series Carriage Options: Aircraft: B-1B B-2A B-52H F-15E F-16C-D F/A-18A-F A-10 Projected: F35

BLU-117 N/A (v) 2/ Series

BLU-119 (v) 5 /Series N/A

Launcher/Rack: MPRL RLA HSAB BRU-47 MAU-12 BRU-32 MAU-30

Contractor/Status/Improvements/Special Equipment: Contractor Boeing Status Production / Inventory Improvements - Selective Availability Anti-Spoofing Module - Anti-Jamming Management/Engineering: 678 ARSS, Eglin AFB, FL JDAM Program Office) Sustainment: 507 GBSS/GBLC, Hill AFB, UT Technical Order:

11K31-2-7 11A-1-63 /NA 11-140-10 for Assembly

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JDAM MK 84 GBU-31(V)1 Series (USAF) GBU-31(V)2 Series (USN) BLU-117 GBU-31(V)2 Series (USN) Navy MK84 Thermal coated, IM PBX 109 fill

MK 84 BLU-117 BLU-119 B

BLU-119 GBU-31(V)5 Series (USAF)

JDAM BLU-109 GBU-31(V)3 Series (USAF) GBU-31(V)4 Series (USN) BLU-109

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Nomenclature: GBU-32

Name: Joint Direct Attack Munition (JDAM)

Capability: Accurate adverse weather guided munitions for use on conventional strike environments to destroy fixed and relocatable targets. Description: The Joint Direct Attack Munition (JDAM) is a Guidance Set, KMU-559 Series, which converts existing unguided 1,000 lb. free-fall bombs, MK 83 and BLU-110, into accurate, adverse weather "smart" munitions. The Guidance Set consists of a Tail Kit, which contains an Inertial Navigational System (INS) and a global positioning system (GPS), a set of Aerosurfaces, and an Umbilical Cover, which allows the JDAM to improve the accuracy of unguided, general purpose bombs in any weather condition. The KMU-559B/B configurations are equipped with a Selective Availability Anti-Spoofing Module (SAASM) added to existing Tail Kits. The SAASM electronics module is capable of utilizing new GPS security features. The KMU-559C/B configurations are equipped with Anti-Jamming (AJ) equipment consisting of a new antenna and associated electronics on the Tail Kit. Anti-Jamming variants allow the JDAM to navigate with precision using GPS signals in regions containing active GPS jamming. JDAM can be launched from very low to very high altitudes in a dive, toss and loft, or in straight and level flight with an on-axis or off-axis delivery. JDAM enables multiple weapons to be directed against single or multiple targets on a single pass. JDAM is a joint U.S. Air Force and Department of the Navy program. Characteristics: CRD Weapons Code ZJ31B ZJ31C ZJ31D ZJ31E BJ31A BJ31B BJ31C BJ31D

GBU-32, MK-83 INERT , FMU-139D-2 GBU-32 MK-83 INERT FMU-152 D-2 GBU-32, MK-83 INERT, FMU-139 D-2 GBU-32, MK-83 INERT, FMU-152 D-2 GBU-32(V)1 FMU-139 (T) GBU-32(V)1 DSU-33C/B B/B FMU-139 GBU-32(V)1 FMU-139/FMU-139 GBU-32(V)1 FMU-152

BJ31E BJ31F BJ31G BJ31H BJ31J BJ31K ZJ31A

GBU-32(V)1 DSU-33C/B B/B FMU-152 GBU-32(V)1 AJ FMU-139(T) GBU-32(V)1 AJ DSU-33C/B FMU-139 GBU-32(V)1 AJ FMU-139/FMU-139 GBU-32(V)1 AJ FMU-152 GBU-32(V)1 AJ DSU-33C/B FMU-152 GBU-32(V)1 MK-83 INERT

Guidance - INS/GPS Control Tail Aerodynamic Autopilot Proportional Guidance Class 1,000 lb. Guided Munition Weight (lbs.) - MK 83 (AF-1,014; Navy-1,029), BLU-110 (AF and Navy -1,029) Length (in.) 119.6 Diameter (in.) - 19.6 Warhead MK 83 and BLU-110 Explosive MK 83 - 416 lbs. Tritonal; BLU-110 – 445 lbs. IM PBXN-109 Fuze FMU-152 or FMU-139 (Note MK 83 has 445 lbs. H-6, Tritonal, or PBXN-109) Sensor DSU-33 JDAM 1,000 LB NOMENCLATURE / GBU 32: MK 83 BLU-110 USAF (v) 1 Series N/A USN (v) 2 Series (v) 2 Series

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Carriage Options: Aircraft: AV-8B F/A-18A-F F-22A Projected F-35

Launcher/Rack: BRU-36 BRU-32 BRU-46

Contractor / Status / Improvements / Special Equipment: Contractor Boeing Status Production / Inventory Improvements - Selective Availability Anti-Spoofing Module - Anti-Jamming Management/Engineering: 678 ARSS/CC, Eglin AFB, FL (JDAM Program Office) Sustainment: 507 GBSS/GBLC, Hill AFB, UT Technical Order:

11K31-2-7 11A-1-63 / NA 11-140-10 for Assembly

MK 83 BLU-110

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Nomenclature: GBU-38

Name: Joint Direct Attack Munition (JDAM)

Capability: Accurate adverse weather guided munitions for use on conventional strike environments to destroy fixed and relocatable targets. Description: The Joint Direct Attack Munitions (JDAM) is a Guidance Set, KMU-572 Series, which converts existing unguided 500 lb. free-fall bombs, MK 82, BLU-111 and BLU-126, into accurate, adverse weather "smart" munitions. The introduction of the GBU-38 gives leaders a smaller precision weapon to further decrease the likelihood of collateral damage. This is especially important as forces continue to target insurgents and their meeting places, normally within heavily populated residential areas. The Guidance Set consists of a Tail Kit, which contains an Inertial Navigational System (INS) and a Global Positioning System (GPS), a set of Aerosurfaces, and an Umbilical Cover, which allows the JDAM to improve the accuracy of unguided, general purpose bombs in any weather condition. The KMU-572B/B configurations are equipped with a Selective Availability Anti-Spoofing Module (SAASM) added to existing Tail Kits. SAASM electronics module is capable of decoding new GPS cryptography. The KMU-572C/B configurations are equipped with Anti-Jamming (AJ) equipment consisting of a new antenna and associated electronics on the Tail Kit. AJ variants allow the JDAM to navigate with precision using GPS signals in regions containing active GPS jamming. Characteristics: CRD Weapons Code BJ21A BJ21B BJ21C BJ21D BJ21F BJ21G BJ21H BJ21J BJ21K BJ26A BJ26B BJ26C BJ26D BJ27A BJ27B BJ27C BJ27D

GBU-38(V)1/B FMU-139 GBU-38(V)1/B DSU-33C/B B/B FMU-139 GBU-38(V)1/B FMU-152 GBU-38(V)1/B DSU-33C/B B/B FMU-152 GBU-38C(V)1/B, AJ, FMU-139C/B GBU-38C(V)1/B AJ DSU-33C/B, FMU-139 GBU-38C(V)1/B, AJ, FMU-152A/B GBU-38C(V)1/B AJ DSU-33C/B, FMU-152 GBU-38(V)1/B FMU-139 N/T

BJ27E BJ27F BJ27G BJ27H BJC1A BJC1B BJC1C BJC1D BJC1E GBU-38(V)1/B W/FMU-139 B-1 BJC1F GBU-38(V)1 /B W/DSU-33 W/FMU-139 B-1 ZJE1A GBU-38(V)1/B W/FMU-152 B-1 ZJE1B GBU-38(V)1/B W/DSU-33 FMU-152 B-1 ZJE1C GBU-38(V)1/B FMU-139 B-2 ZJE1F GBU-38(V)1/B DSU-33C/B BBFMU-139 B-2 ZJE1G GBU-38(V)1/B FMU-152 B-2 ZJE7A GBU-38(V)1/B DSU-33C/B BBFMU-152 B-2 ZJ51A

GBU-38C(V)1 C/B AJ FMU-139 B-2 GBU-38C(V)1 C/B AJ, DSU-33FMU-139 B-2 GBU-38C(V)1 C/B AJ, FMU-152 B-2 GBU-38C(V)1 C/B AJ, DSU33 FMU-152 B-2 GBU-38(V)4/B BLU-126 FMU-152 GBU-38C(V)4/B AJ, BLU-126, FMU-152 GBU-38(V)4/B BLU-126 FMU-152/DSU-33C/B GBU-38C(V)4/B AJ BLU-126 FMU-152 DSU-33C/B GBU-38(V)4/B BLU-126 FMU-152 DSU-33A/B GBU-38C(V)4/B AJ BLU-126 FMU-152 DSU-33 A/B GBU-38(V)1 MK-82 (I) GBU-38(V)1 MK-82 (I) FMU-152 GBU-38(V)1 (1) MK-82 FMU-139 GBU-38(V)1/B MK-82(I)FMU-152A(D-2)/B GBU-38(V)1 MK-82(I) FMU-139D2 GBU-38/(V)1/B MK-82 (I) B-2 GBU-38(V)1/B BDU-50

Guidance Control Autopilot Class Weight (lbs.) -

INS/GPS Tail Aerodynamic Proportional Guidance 500 lb. Guided Munitions MK 82 (AF-552 lbs; Navy-558 lbs.), BLU-111 (AF-N/A; Navy- 558 lbs.), BLU126 (AF-558 lbs.); Navy -558 lbs. (Low Collateral War Head)) Length (in.) 95.2 Diameter (in.) - 17

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Warhead Explosive Fuze Sensor -

MK 82, BLU-111, and BLU-126 MK 82 192 lbs. Tritonal, BLU-111 192 lbs. PBXN-109, BLU-126 28 lbs. PBXN-109 FMU-152 or FMU-139 DSU-33

JDAM 500 LB NOMENCLATURE/ GBU 38: MK 82 BLU-111 USAF (v) 1 Series N/A USN (v) 2 Series (v) 2 Series Carriage Options: Aircraft: AV-8B B-1B B-2A B-52H F-15E F-16C-D F/A-18 A- F A-10 Projected: MQ-9

BLU-126 (v) 4 Series (v) 4 Series

Launcher/Rack: BRU-36 MPRL SBRA HSAB BRU-57 MAU-12 and BRU-57 BRU-32 and BRU-55 MAU-40 BRU-15/A (Modified); BRU-71A (Pending Qualification)

Contractor / Status / Improvements / Special Equipment: Contractor Boeing Status Production / Inventory Improvements - Selective Availability Anti-Spoofing Module - Anti-Jamming Management/Engineering: 678 ARSS, Eglin AFB, FL (JDAM Program Office) Sustainment: 507 GBSS/GBLC, Hill AFB, UT Technical Order:

11K31-2-7 11A-1-63/NA 11-140-10 for Assembly

MK 82 BLU-111 BLU-126

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Nomenclature: GBU-39A/B

Name: Small Diameter Bomb Increment I (SDB I) FLM

Capability: Adverse weather, standoff, near precision autonomous attack to deliver lethal effects (neutralize/destroy) against fixed soft non-hardened targets. Focused Lethality Munition (FLM) provides increased load-out (four per aircraft -1760 weapon station), thus increased kills per sortie. Description: FLM is a 250 lb. class weapon designed as a small autonomous, conventional, air-to-ground, precision glide weapon able to strike targets in collateral damage sensitive environments such as urban warfare and Close Air Support. FLM is a variant of the GBU-39/B Small Diameter Bomb. The GBU-39/B‟s steel warhead was removed and replaced with a composite case filled with the Multi-Phase Blast Explosive (MBX). Characteristics: CRD Weapons Code Guidance Control Autopilot Class Weight (lbs.) Length (m) Diameter (mm) Warhead Range Explosive Fuze -

TBD INS/GPS (Augmented by Wide Area Differential GPS) Tail Aerodynamic (plus Diamond-back wing kit) Proportional Guidance 250 lb. Guided Munition 285 1.8 152.4 Blast 40 + nm Standoff AFX 1209 (Multi-Phased Blast Explosive) ESAF (Delivered as All-Up-Round)

Carriage Options: Aircraft: F-15E

Launcher/Rack: BRU-61/A (4-place Miniature Munition Carriage System)

Contractor / Status / Improvements / Special Equipment: Contractor - Boeing Status Development Residuals Fielded Management/Engineering: 681st ARSS, Eglin AFB, FL Operational Manager is CENTCOM J-8 Technical Order: 11K39-2-7

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Nomenclature: GBU-39/B

Name: Small Diameter Bomb Increment I (SDB I)

Capability: Adverse weather, standoff, near precision autonomous attack to deliver lethal effects (neutralize/destroy) against fixed soft non-hardened and hardened targets. SDB I provides increased load-out (four per aircraft -1760 weapon station), thus increased kills per sortie. Description: SDB I is a 250 lb. class weapon designed as a small autonomous, conventional, air-to-ground, precision glide weapon able to strike fixed and stationary re-locatable targets from standoff range. The SDB weapon system consists of the weapon, the BRU-61/A (4-place pneumatic carriage system), shipping and handling containers for a single weapon and the BRU-61/A either empty or loaded and a weapon planning module. The SDB I Advanced Anti-Jam Global Position System aided Initial Navigation System (AJGPS/INS) provides guidance to the coordinates of a stationary target. The payload/warhead is a very effective multipurpose penetrating and blast fragmentation warhead coupled with a cockpit selectable electronic fuze. A proximity sensor provides a height of burst capability. It is compatible with all AF platform internal carriage systems and its low-drag carriage rack characteristics enhance external carriage. Characteristics: CRD Weapons Code Guidance Control Autopilot Class Weight (lbs.) Length (m) Diameter (mm) Warhead Range Explosive Fuze Carriage Options: Aircraft: Threshold: F-15E Objective: Group 1: F-22A F-35 Group 2: A-10 F-16C-D B-52H B-1B B-2A MQ-9

BSDBA INS/GPS (Augmented by Wide Area Differential GPS) Tail Aerodynamic (plus Diamond-back wing kit) Proportional Guidance 250 lb. Guided Munition 285 1.8 152.4 Blast Frag / Penetrator 40 + nm Standoff AFX 757 (Insensitive Munition) ESAF (Delivered as All-Up-Round)

Launcher/Rack: BRU-61/A (4-place Miniature Munition Carriage System)

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Contractor / Status / Improvements / Special Equipment: Contractor - Boeing Status Production Management/Engineering: 681st ARSS, Eglin AFB, FL Equipment Specialist/Item Management: 507 CBSS/GBLC, Hill AFB, UT Technical Order: 11K39-2-7

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Nomenclature: GBU-43/B

Name: Massive Ordnance Air Blast (MOAB)

Capability: To accurately deliver mass-ordnance weapon effects against open-field target set from high altitude. Description: The GBU-43/B, better known as the MOAB, is a precision-guided low altitude blast bomb comprised of a 21,615 pound BLU-120/B warhead, an aluminum cradle, a 28‟ type V pallet assembly, and a KMU-593/B Guidance Control Unit (GCU). It is typically launched at a high altitude and significant standoff range. This weapon's primary purpose is against large formations of troops, equipment, or hardened above-ground bunkers. Characteristics: CRD Weapons Code N/A Guidance KMU-593/B; INS, GPS Guidance Control Unit Control 4 ea. Lattice Grid Fins Autopilot Digital, Bank to Turn Software Navigation Class 22,000 lb. Blast Warhead Weight (lbs.) 22,600 Length (in.) 361.75 Diameter (in.) 40.5 Warhead BLU-120/B, Blast Explosive (NEW) - H6 18,700 lbs. Fuze Dual Nose, M904E2, M-9 delay, M1A1 Fuze Extensions, T45E7 Adapter Boosters Stabilizer Wing Assembly Carriage Options: Aircraft: MC-130H MC-130E

Launcher/Rack: N/A

Contractor / Status / Improvements / Special Equipment: Contractor - Dynetics (Prime), Air Force Research Laboratory, Eglin (Warhead), ASEI (Software), McAlester Army Ammunition Plant (Explosive load) Status Inventory Management/Engineering: 708 ARSG, Eglin AFB, FL Item Management/Equipment Specialist: 507 CBSS/GBLC, Hill AFB, UT Technical Order: 11K43-2-7

GBU-43/B on Pallet and Cradle Assembly

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Nomenclature: GBU-44/B

Name: Viper Strike

Capability: Viper is primarily used in missions that require a flexible angle of attack, either steep or shallow with long stand-off range. Description: The GBU-44/B Viper Strike glide bomb is a GPS-aided laser-guided variant of the Northrop Grumman Brilliant Anti-Tank (BAT) munition which originally had an acoustic seeker. Viper Strike has been integrated onto multiple manned and unmanned platforms for Army, Air Force, SOCOM, and other customers. Viper Strike has also been successfully employed against multiple target sets. Characteristics: Guidance Weight (lbs.) Length (in.) Diameter (in.) Wingspan (in.) Glide Ration Warhead Range -

GPS-midcourse/terminal laser homing 42 36 5.5 36 10:1 Shaped Charge 2.3 lbs. high explosive anti-tank excess of 5 km

Carriage Options: Aircraft: MQ-5A/B/C AC-130J SOCOM Platforms

Launcher/Rack

Contractor / Status / Improvements / Special Equipment: Contractor - Northrop Grumman Status Production Management/Engineering: US Army, PEO Missile and Space, Joint Attack Munition Systems Office, Redstone Arsenal, Huntsville, AL Sustainment: TBD Technical Order: TBD

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Nomenclature: GBU-51/B

Name: Laser Guided Bomb with LOCO Bomb Body

Capability: Precision bombing against non-hardened targets. Description: The GBU-51/B is a 500 lb. class laser guided bomb that uses the BLU-126/B Low Collateral (LOCO) warhead. The Paveway II system has folding wings that open upon release for increased aircraft payload and maneuverability. This weapon is primarily used for precision bombing against non-hardened targets. GBU-51/B consists of a combined Computer Control Group (CCG) and Adapter Group (ADG) and an Airfoil Group MXU-650. Characteristics: Guidance Control Air Foil Group Autopilot Class Weight (lbs.) Length (in.) Diameter (in.) Warhead Explosive (NEW) Fuze Stabilizer Carriage Options: Aircraft: F/A-18A-F AV-8B

Semi-Active Laser WCU-10, MAU-169, MAU-209 MXU-650 Series Bang-Bang Mode 500 lb. Paveway II Guided Weapon 610.67 131.15 10.75 (Warhead) 18 in. (Airfoil Group) BLU-126/B LOCO PBXN-109 (27 lbs.) FMU-139 Series MXU-650 Series (Paveway II)

Launcher/Rack: BRU-32, BRU-33 BRU-36

Contractor / Status / Improvements / Special Equipment: Contractor - Lockheed Martin, Raytheon Status Inventory Management/Engineering: NAVAIRSYSCOM PMA-201, NAS Patuxent River, MD Technical Order: NA 11-140-10

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Nomenclature: GBU-52/B

Name: Dual Mode Laser Guided Bomb (DMLGB)

Capability: Precision bombing against non-hardened targets. Description: The GBU-52/B is a 500 lb. class laser guided bomb that uses the BLU-126 warhead. It enhances existing LGB kits by adding GPS/INS guidance capability. DMLGB Kits consist of a combined Computer Control Group (CCG) and Adapter Group (ADG) WGU-53/B and an Airfoil Group, MXU-650. The DMLGB system has folding wings that open upon release for increased aircraft payload and maneuverability. This weapon is primarily used for precision bombing against non-hardened targets. Characteristics: Guidance Control Air Foil Group Autopilot Class Weight (lbs.) Length (in.) Diameter (in.) Warhead Explosive (NEW) Fuze Stabilizer Carriage Options: Aircraft: F/A-18A-F AV-8B

Semi-Active Laser, GPS/INS WGU-53/B MXU-650 Series Bang-Bang Mode 500 lb. Paveway II Guided Weapon 610.67 131.15 10.75 (Warhead) 18 in. (Airfoil Group) BLU-126/B LOCO PBXN-109 (27 lbs.) FMU-139 Series MXU-650 Series (Paveway II) Launcher/Rack: BRU-32, BRU-55 BRU-36

Contractor / Status / Improvements / Special Equipment: Contractor - Lockheed Martin Status Inventory Management/Engineering: NAVAIRSYSCOM PMA-201, NAS Patuxent River, MD Technical Order: NA 11-140-10

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Nomenclature: GBU-54/B

Name: Laser Joint Direct Attack Munition (LJDAM)

Capability: The GBU-54/B Laser JDAM (LJDAM) adds the flexibility to strike targets of opportunity, including mobile targets, to the already accurate adverse weather GPS/INS guided JDAM. Description: The DSU-38/B, Detector Laser Illuminated Target adds a Precision Laser Guidance Set (PLGS) to inventory JDAMs, giving the weapon system optional semi-active laser guidance in addition to its current GPS/INS guidance. The DSU-38/B is a DSU-33 form factored passive laser seeker that can be easily installed in the field to the front of existing JDAM weapons and is connected to the Guidance Set via an externally mounted strap-on harness kit. The DSU-38/B is compatible with currently fielded laser designator systems and will initially be integrated with the 500-lb. GBU-38, creating a GBU-54 LJDAM. Characteristics: CRD Weapons Code BJ21N GBU-54(V)1/B DSU-38/B FMU-152 BJ21P GBU-54C(V)1/B AJ DSU-38/B FMU-152 BJ21T GBU-54(V)1/B DSU-38 FMU 139(T) BJ21X GBU-54C(V)1/B AJ DSU-38 FMU-139(T) ZJE1J GBU-54A(D-2)/B W/FMU-152(D-2)/B ZJE1M GBU-54A(D-2)/B W/FMU-139(D-2)/B Guidance Semi-Active Laser, INS/GPS Control Tail Aerodynamic Autopilot Proportional Guidance Class 500 lb. Guided Munitions Weight (lbs.) MK 82 (AF - 552 lbs.; Navy - 558 lbs.), BLU-111 (AF - N/A; Navy - 558 lbs.), BLU-126 (AF - N/A; Navy - 558 lbs) Length (in.) 95.2 Diameter (in.) 17 Warhead MK 82, BLU-111, and BLU-126 Explosive MK 82 192 lbs. Tritonal, BLU-111 192 lbs. PBXN-109, BLU-126 28 lbs. PBXN-109 Fuze FMU-152 or FMU-139 Sensor Detector, Laser Illuminated Target (DSU-38) Container CNU-693/B for DSU-38/B and DSU-38 (D-2)/B JDAM 500 LB NOMENCLATURE/ GBU 54: MK 82 BLU-111 USAF (v) 1 Series N/A USN (v) 2 Series (v) 2 Series

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Carriage Options: Aircraft: Launcher/Rack Threshold: F-15E F-16C/D Block 30/40/50 with/without BRU-57 F/A-18A+/C/D BRU-32, BRU-55 AV-8B BRU-36 Objective: A-10 B-1B B-2A B-52H F/A-18E/F MQ-9 Contractor / Status / Improvements / Special Equipment: Contractor - Boeing Status Production Management/Engineering: 678 ARSS, Eglin AFB, FL (JDAM Program Office) Sustainment: 507 CBSS/CBLC, Hill AFB UT Technical Order: 11G7-7-8-7, 11K31-2-7 11A-1-63/NA, 11-140-10 for Assembly

MK 82 BLU-111 BLU-126

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Nomenclature: TBD (Paveway IV)

Name: Dual Mode GPS/INS and Laser Guided Bomb

Capability: Precision bombing against mobile, relocatable, soft and semi-hard targets. Description: The Paveway IV is currently not in the US Air Force or Navy Inventory. It is a British Royal Air Force 500 lb. class MK 82 general purpose bomb with an Enhanced Paveway II Enhanced Computer Control Group (ECCG) kit. The new ECCG contains a Height of Burst (HOB) sensor enabling airburst fusing options, and an improved Anti-Jam, SAASM (Selective Availability Anti Spoofing Module) compliant GPS receiver. It can be launched either IMU (Inertial Measurement Unit) only, given sufficiently good Transfer Alignment, or using GPS guidance. Terminal laser guidance is available in either navigation mode and with airburst fuzing. It is a low-cost, allweather, 24-hour precision bombing capability able to defeat the majority of general-purpose targets. It incorporates an enhanced Mk-82 warhead which, combined with a shock-hardened fuze, enables increased penetration over a standard Mk-82 warhead and can therefore defeat semi-hard targets as well. Post-impact delay settings and airburst height are selectable from the cockpit as are target position and terminal impact/heading angles. The Paveway IV significantly minimizes collateral damage by incorporating a „Late-Arm‟ function, as part of one of the world‟s most advanced fusing systems, to prevent arming of an off-course munition. In addition, the warhead has been designed to meet the latest requirements of NATO Insensitive Munition safety policies. The accuracy of Paveway IV combined with programmable lethal effects, reduces the number of bombs on target which enables a single aircraft to strike more targets in a single pass. On 10 Dec 2008 the UK Ministry of Defense officially declared the Paveway IV as having entered service. Characteristics: Guidance Control Air Foil Group Autopilot Class Weight (lbs.) Length (in.) Diameter (in.) Warhead Explosive (NEW) Fuze Stabilizer -

Dual Mode GPS / Semi-Active Laser WGU-56 MXU-650 Series Bang-Bang Mode 500 lb. Paveway II Guided Weapon 665 (nominal) 131.25 10.75 (Warhead) 18 (Airfoil Group-closed) Enhanced Mk-82 IM Penetrator PBXN-109 (27 lbs.) PGB Fuze MXU-650 Series (Paveway II)

Carriage Options: Aircraft: Harrier GR9 Tornado GR4 Typhoon F2 JSF

Launcher/Rack:

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Contractor / Status / Improvements / Special Equipment: Contractor - Raytheon Status Inventory British Royal Air Force Management/Engineering:

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INTENTIONALLY LEFT BLANK

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CHAPTER SIX 1 June 2009

CLUSTER BOMB UNITS (CBU)

FOR OFFICIAL USE ONLY

INTENTIONALLY LEFT BLANK

Nomenclature: CBU-78

Name: GATOR

Capability: Direct Attack Area Attack Munition that can target troops, trucks, tanks, artillery, SAMs, Radars, POL Tanks, Aircraft on the ground and moving columns. Description: The CBU-78 is an anti-personnel/anti-tank, free fall, folding fin, airburst weapon. The CBU-78/B consists of an SUU-58/B dispenser, loaded with BLU-91/B anti-tank and BLU-92/B anti-personnel mines, kit modification unit BRU-42/B, and a MK 339MOD 1 mechanical time fuze. The CBU-78A/B is delivered from the factory with an FMU-140/B fuze vice the MK 399 and the fin release band retention system vice tail tether. The CBU-78/B weapons retrofitted with the AWC-372 will be redesignated CBU-78B/B. The CBU-78C/B differs from the CBU78A/B in that it has the FMU-140A/B fuze installed. All variants except CBU-78C/B have been removed from USN/USMC inventory. The weapon is delivered to operating activities completely assembled with 14-inch suspension lugs, arming wire extractors, and a removable fuze cover installed. Fins are held in the folded position with a fin retaining band secured by an arming wire and a ground handling safety pin. The CBU-78 GATOR is used by the Navy and is smaller than the CBU-89 GATOR used by the Air Force. Characteristics: Control Autopilot Class Weight (lbs.) Length (in.) Diameter (in.) Warhead Fuze Carriage Options: Aircraft: AV-8B F/A-18A-D

Spin (6 Selections) None Anti-Personnel/Anti-Materiel (AP/AM) 491 92.00 13.2 45 ea BLU-91/B Anti-Tank Mines (4.31 lbs. ea) 15 ea BLU-92/B Anti-Personnel Mines (3.75 lbs. ea) MK 339 Mechanical time nose fuze, FMU-140A/B Proximity Fuze (6 time selections) Launcher/Rack: BRU-36/BRU-42 BRU-32/BRU-33

Contractor / Status / Improvements / Special Equipment: Contractor - Honeywell/Aerojet/Olin/Alliant Status Inventory Management/Engineering/OPR: PMA-201, Patuxent River, MD Technical Order: NAVAIR 11-140-9

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Data for BLU-91/B and BLU-92/B:

CBU-78 Series Bomb Cluster (GATOR)

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Data for BLU-91/B and BLU-92/B: Aeroballistic adapter 5.8 in x 5 in x 2.6 in Minelet height 2.6 in Minelet diameter 4.75 in Weight BLU-91/B - 4.3 lb; BLU-92/B - 3.7 lb Explosive - BLU-91/B 1.3 lb RDX; BLU-92/B - 0.9 lb Composition B-4

BLU-91/B

BLU-92/B

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Nomenclature: CBU-87

Name: Combined Effects Munitions (CEM)

Capability: Direct Attack Area Attack Munition that can target troops, trucks, tanks, artillery, SAMs, Radars, POL Tanks, Aircraft on the ground and moving columns. Description: The CBU-87 is an excellent weapon against armor, personnel, artillery, etc. The weapon dispenses 202 BLU-97 munitions in a pattern with density and sizes of the area covered depending on release parameters and spin rates. When the Wind Corrected Munitions Dispenser (WCMD) kit is added it becomes a CBU-103X/X, see page 6-14 for configurations and CRD weapons codes. Characteristics: CRD Weapons Code CBU-87/B DISPENSER AND BOMB CBU-87A/B DISPENSER AND BOMB C875A CBU-87B/B DISPENSER AND BOMB F-15E C871A CBU-87B/B DISPENSER AND BOMB C878A CBU-87B/B DISPENSER AND BOMB B-2 C876B CBU-87B/B DISPENSER AND BOMB B-1 C875B CBU-87M/B DISPENSER F-15E C876A CBU-87M/B DISPENSER & BOMB B-1

C871B

CBU-87M/B DISPENSER AND BOMB C878B CBU-87M/B DISPENSER B-2 P871A PREPO ISO CBU-87 SZCAB STAMP CBU-87B/B Z871A CBU-87(T-1)/B

Control Spin (6 Selections) Autopilot None Class Anti-Personnel/Anti-Materiel (AP/AM) Weight (lbs.) 949.36 Length (in.) 92.00 Diameter (in.) 15.60 Warhead - 202 ea Combined Effects Bombs (CEB) - BLU-97/B AP/AM Shaped Charge/Frag/ Incendiary Bomblets. These bomblets are soda-can-sized bomblets approximately 20 centimeters long, and has a six centimeter diameter, they are bright yellow when new. The original Cyclotol explosive has been replaced with PBXN-107 explosive in the IM BLU-97. BLU-97/B Data Length Stored - 16.8 cm (6.6 in); deployed (w/o retarder canopy): 22.6 cm (8.9 in.) Diameter (in.) - 2.5 Weight (lbs.) - 3.4 Explosive (lbs.) - 0.63 Cyclotol/PBXN-107 Explosive Fuze -

Integral Part of Dispenser (12 Time Selections) and FZU-39/B Proximity Sensor (10 Height of Burst Selections)

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Carriage Options: Aircraft: A-10 B-1B B-2A B-52H F-15E F-16A-D

Launcher/Rack: 14 in Lug Spacing

Contractor / Status / Improvements / Special Equipment: Contractor - Aero General/Honeywell, Inc. Alliant Tech. Status Inventory Management/Engineering/OPR: 507 CBSS/GBLB, Hill AFB, Utah Technical Order: 11A9-31-7

CBU-87 CEM

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BLU-97/B Bomblet

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Nomenclature: CBU-89

Name: GATOR

Capability: Direct Attack Area Attack Munition that can target troops, trucks, tanks, artillery, SAMs, Radars, POL Tanks, Aircraft on the ground and moving columns. Description: The CBU-89 Gator Mine, a 1,000-pound cluster munition containing anti-tank and antipersonnel mines, consists of a SUU-64 Tactical Munitions Dispenser with 72 anti-tank mines, 22 anti-personnel mines, and an optional FZU-39 proximity sensor. The weapons are dispensed over a predetermined area given the height of function setting selected on the aforementioned FZU-39 proximity sensor. The CBU-89 contains a self destruct mechanism which can be set for three different time delays. When the Wind Corrected Munitions Dispenser (WCMD) kit is added it becomes a CBU-104X/X, see page 6-14 for configurations and CRD weapons codes. Characteristics: CRD Weapons Code C898A Z891A C896A C897A C895B SZCBA C891B

CBU89 B2 CBU-89(T-1)/B CBU-89A/B GATOR HIGH ALTITUDE B-1 CBU-89A/B GATOR HIGH ALTITUDE F-117 CBU-89A/B HIGH ALTITUDE F-15E STAMP CBU-89/B CBU 89A/B GATOR HIGH ALTITUDE

Class Weight (lbs.) Length (in.) Diameter (in.) Warhead Dispenser Fuze -

Anti-Personnel/Anti-Materiel (AP/AM) 705.29 91.75 15.60 72 ea BLU-91/B Anti-Tank Mines (4.31 lbs. ea) 22 ea BLU-92/B Anti-Personnel Mines (3.75 lbs. ea) SUU-64/B Integral Part of Dispenser FZU-39/B Proximity Sensor signs

Carriage Options: Aircraft: Launcher/Rack: A-10 14” Lug Spacing B-1B B-2A B-52H F-15E F-16A-D Delivery Envelope: 200-40,000 ft Alt, 200-700 KIAS Contractor / Status / Improvements / Special Equipment: Contractor - Honeywell/Aerojet/Olin/Alliant Status Inventory Management/Engineering/OPR: 507 CBSS/GBLB, Hill AFB, Utah

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Technical Order: 11A9-31-7 Shipping and Storage Containers: Use applicable CNU-411 Container IAW TO 11A9-31-7

SUU-64/B (loaded as CBU-89/B) Fins not deployed Data for BLU-91/B and BLU-92/B: Aeroballistic adapter: 14.7 cm x 12.7 cm x 6.6 cm (5.8 in x 5 in x 2.6 in) Minelet height: 6.6 cm (2.6 in) Minelet diameter: 12.1 cm (4.75 in) Weight: BLU-91/B: 1.95 kg (4.3 lb); BLU-92/B: 1.68 kg (3.7 lb) Explosive: BLU-91/B: 594 g (1.3 lb) RDX; BLU-92/B: 408 g (0.9 lb) Composition B-4

BLU-91/B

BLU-92/B

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Nomenclature: CBU-97

Name: Sensor Fuzed Weapon (SFW)

Capability: Direct Attack Area Attack Munition, Wide area coverage; multiple kills per pass; to defeat fixed, moving and mobile/relocatable land targets; expanded target set - soft and hard mobile targets including heavy armor (adverse weather, at night, or in countermeasure environment (P3I). Description: The Sensor Fuzed Weapon (SFW) CBU-97 consists of a Tactical Munition Dispenser (TMD), SUU-66/B, and ten BLU-108 submunitions. Each submunition contains four projectile warheads. After release over the target area, the TMD opens dispensing the submunitions. The submunitions are parachute retarded into a nose-down orientation and releases the warheads in a horizontal trajectory to obtain maximum area coverage. The warheads targetactivate through a small infrared sensor and fire a self-forging projectile into the target. The warheads self-destruct if not targeted after eight second flight for clean battlefield. SFW Preplanned Product Improvement (P3I), added sensor upgrades (active laser), multi-mission warhead, area footprint extension, and redundant self-destruct features for a cleaner battlefield. CBU-97/B

SFW CBU CONFIGURATION DURING THE PRODUCTION TRANSITION PROGRAM

When the Wind Corrected Munitions Dispenser (WCMD) kit is added it becomes a CBU-105X/X, see page 6-14 for configurations and CRD weapons codes. CBU-97A/B

PEP -1* CONFIGURATION

* Producibility Enhancement Program (PEP), PEP 1: Electronic and mechanical enhancements to the warhead projectile. Characteristics: CRD Weapons Code SZCCA CBU-97 SFW C971A CBU-97/B (SFW) C976A CBU-97/B (SFW) B-1 C978A CBU-97/B (SFW) B-2 C975A CBU-97/B (SFW) F-15E CBU-97A/B (SFW) Weight (lbs.) Length (in.) Diameter (in.) Dispenser Submunition Submunition Weight Length Diameter Fuze -

950 92.00 15.60 SUU-66/B 10 ea BLU-108/B w/ four Warheads Each 10 BLU-108/B, A/B w/ four Warheads Each BLU-108: 63 lbs., Projectile: 8 lbs. BLU-108: 31 in., Projectile: 3.75 in. BLU-108: 5.25 in., Projectile: 5.25 in. Integral Part of Dispenser (12 timer settings) FZU-39/B Proximity Sensor (10 height of function settings)

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Carriage Options: Aircraft: A-10 B-1B F-15E F-16A-D

Launcher/Rack: 14 in. Lug Spacing

Contractor / Status / Improvements / Special Equipment: Contractor - Textron Defense Systems, Wilmington, MA Status Production Management/Engineering: 308 ARSG, Eglin AFB, FL Transitions to 507 CBSS/GBLB, Hill AFB, UT FY10 Technical Order: 11A9-31-7 Shipping and Storage Containers: Use applicable CNU-411 Container IAW TO 11A9-31-7

CBU-97/B sensor-fuzed weapon with a side panel removed

BLU-108/B

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BLU-108/B bomblet with one of the four Skeet warheads flipped out

Model of a Skeet submunition warhead illustrating the formation of the self-forging penetrating pellet.

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Nomenclature: MK 20, CBU-99/100/B, A/B, B/B

Name: Rockeye

Capability: Direct Attack Area Attack Munition that can target troops, trucks, tanks, artillery, SAMs, Radars, POL Tanks, Aircraft on the ground and moving columns. Description: The Navy MK 20 series and CBU-99/100 series is a free-fall folding fin airburst weapon. The bomb consist of a MK 7/SUU-76 bomb dispenser loaded with MK 118 anti-tank bomblets and a MK339 mechanical time fuze or the FMU-140 series Dispenser Proximity Fuze. All variants except CBU-99B/B have been removed from USN/USMC inventory. Characteristics: CRD Weapons Code Guidance None Class Cluster Bomb Unit (CBU) Weight (lbs.) 490-505 Length (in.) 92 Diameter (in.) 13.2 Dispenser MK 7 / SUU 76 Payload 247 MK 118 Anti-Tank bomblets Fuze MK 339 (MK 20 and CBU-99/100/B), FMU-140/B (CBU-99/100/A/B), FMU-140A/B (CBU-99/100/B/B). Propulsion None Carriage Options: Aircraft: AV-8B F/A-18 A-F P-3C

Launcher/Rack: BRU-36/BRU-42 BRU-32/BRU33 BRU-15

Contractor / Status / Improvements / Special Equipment: Contractor - Honeywell Status In Inventory Management/Engineering: PMA-201, Patuxent River, MD Technical Order: NA 11-140-9

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MK 20 MODS EXEPT MODS CBU-99/B, CBU-100/B, AND S MK 20 MODS 9 & 10, CBU-99A/B, CBU99B/B, CBU-100A/B, AND CBU-100B/B

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Nomenclature: CBU-103/104/105

Name: Wind Corrected Munitions Dispenser (WCMD)

Capability: Direct Attack Area Attack Munition that can target troops, trucks, tanks, artillery, SAMs, Radars, POL Tanks, Aircraft on the ground and moving columns. Description: The Wind Corrected Munitions Dispenser’s (WCMD) high speed laydown deliveries are consistent with tactics used against heavily defended target sets. The tail kit inertially steers the munition from a known release point to precise target coordinates while compensating for launch transients, winds aloft, surface winds and adverse weather. Characteristics: CRD Weapons Code C031A C036A C038A C035A C031B C041A C046A C048A C047A C045A C041B C051A C056A C058A C055A C051D C071B P103A SZCDA SZCFA

CBU-103 WCMD CBU-103 WCMD B-1 CBU-103 WCMD B-52H CBU-103 WCMD F-15E CBU-103 WCMD F-16 CBU-104 WCMD CBU-104 WCMD B-1 CBU-104 WCMD B-52H CBU-104 WCMD CBU-104 WCMD F-15E CBU-104 WCMD F-16 CBU-105 WCMD CBU-105 WCMD B-1 CBU-105 WCMD B-52H CBU-105 WCMD F-15E CBU-105 WCMD F-16 CBU-107 WCMD F16 PREPO ISO CBU-103 STAMP CBU-103 CEM WCMD STAMP CBU-105 SFW WCMD

DISPENSER SUU-65/B SUU-65/B SUU-64/B SUU-66/B SUU-66/B SUU-66/B SUU-66/B SUU-66/B Guidance Class Weight (lbs.) Length (in.) -

LOCKHEED MARTIN CBU-103A/B CBU-103B/B CBU-104A/B CBU-105/B CBU-105A/B CBU-105B/B CBU-105C/B CBU-105D/B INS Tactical Munitions Dispenser (TMD) Guidance Kit modification for CBU-87/89/97 980.00 92.00

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Diameter (in.) - 15.60 Dispenser SUU-64/B, SUU-65/B, SUU-66/B TMDs Payload 71 BLU-91/B, 22 BLU-92/B (CBU-104), 202 BLU-97/B or A/B (CBU-103), 10 BLU-108/B, or A/B, or B/B, or C/B, or D/B (CBU-105) Fuze Integral Part of Dispenser / FZU-39/B Proximity Sensor Propulsion None Carriage Options: Aircraft: A-10 B-1B B-52H F-15E F-16C-D

Launcher/Rack: 14 in. Lug Spacing

Contractor / Status / Improvements / Special Equipment: Contractor - Lockheed Martin Status Inventory Special Equipment - AN/GYQ-79 Common Munition Bit Reprogrammable Equipment (CMBRE) Management/Engineering: 308 ARSG, Eglin AFB, FL (CBU-105) until FY10 507 CBSS/GBLB, Hill AFB, UT Technical Order: 11A9-31-7 Shipping and Storage Containers: Use applicable CNU-411 Container IAW TO 11A9-31-7

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Nomenclature: CBU-107/B

Name: Passive Attack Weapon (PAW)

Capability: Attack and defeat a wide range of soft fixed surface targets and chemical/biological targets with low collateral damage. Description: The CBU-107 is an area attack weapon that uses kinetic energy penetrators to address soft ground targets. The weapon is employed the same as a CBU-103. Two hundred and thirty weapons were produced in support of a quick reaction capability program for the US Central Command. The weapon is designed for use in an environment where warfighters need to disable a target without destroying its surroundings. Some examples include storage facilities, fuel storage depots, power substations or antenna fixtures. Characteristics: CRD Weapons Code - None Control Spin (Set at 500 rpm) Autopilot None Class Anti-Material Weight (lbs.) 1000 Length (in.) 92.00 Diameter (in.) 15.50 Warhead 362 large (590 grams), 1004 medium (86 grams), and 2406 small (5.5 & 3.9 grams) rods Fuze Integral Part of Dispenser FZU-39/B Proximity Sensor (Height of Burst Selection - 1500 feet, 110 ft diameter pattern) Carriage Options: Aircraft: B-52H F-15E F-16 (Blk 40/50)

Launcher/Rack: 14 in. Lug Spacing

Contractor / Status / Improvements / Special Equipment: Contractor - General Dynamics Status Inventory Special Equipment - AN/GYQ-79 Common Munition Bit Reprogrammable Equipment (CMBRE) Management/Engineering: 507 CBSS/GBLB, Hill AFB, UT Technical Order: 11A9-31-7 Shipping and Storage Containers: Use applicable CNU-411 Container IAW TO 11A9-31-7

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SMALL ROD PACK LARGE ROD PACK

MEDIUM ROD PACK

CBU-107/B PAW PAYLOAD

Penetrators

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Nomenclature: CBU-116/118

Name: Power Distribution Denial Munition (PDDM)

Capability: Renders an electrical power grid component, such as a substation or transformer yard, inoperable for an indefinite period of time until its effects came be removed. The PDDM will affect an average substation and remain persistent until the fibers can be removed. Description: This non-lethal cluster munition carries 202 Long Conductive Fiber (LCF) submunitions, each containing 114 fiber string balls. The stringballs are similar to aluminized chaff that has been in use militarily for over 40 years. The CBU-116 is an early variant of the PDDM with LCF Version 1 submunitions. The CBU-118 has LCF Version 2 submunitions and a WCMD tail installed. CBU-116/B CBU-118/B

Unguided SUU-65/B TMD w/LCF (Ver 1) submunitions SUU-65/B TMD INS (WCMD) w/BLU-114 A/B (Ver 2) submunitions

Characteristics: CRD Weapons Code Guidance Control Autopilot Class Weight (lbs.) Length (in.) Diameter (in.) Warhead Fuze -

Carriage Options: Variant: CBU-116 CBU-118

None CBU-116 Unguided CBU-118 INS (WCMD) Spin (Set at 500 rpm) None Anti-Material 680 lbs. (CBU-116) / 685 lbs. (CBU-118) 92.00 16.36 202 LCF non-lethal submunitions Integral Part of Dispenser FZU-39/B Proximity Sensor (Height of Burst Selection - 1500 feet)

Aircraft:

Launcher/Rack: 14 in. Lug Spacing

F-15E F-16 (Blk 40/50)

Contractor / Status / Improvements / Special Equipment: Contractor - GD-OTS, Florida Status Inventory Special Equipment - AN/GYQ-79 Common Munition Bit Reprogrammable Equipment (CMBRE) Management/Engineering: 507 CBSS/GBLB, Hill AFB, Utah Technical Order: 11A9-31-7 Shipping and Storage Containers Use applicable CNU-411 Container IAW TO 11A9-31-7

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Non-Lethal Fiber Weapons System - Disrupts Electrical Power - Avoids unacceptable Collateral Damage --Achieves theater commander objectives - Provides new options for commanders

Long Fiber Stringball - Aluminum chaff - 128 microns in diameter - 180 ft Long

PDDM CONOPS 6-19

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Nomenclature: PDU-5/B SUU-76C/B

Name: MK 20 Rockeye II Leaflet Canister

Capability: Dispenses large quantities of psychological leaflets. Description: The PDU-5/B uses the MK 20 Rockeye II canister to dispense large quantities of psychological leaflets. The MK 20 nomenclature is the SUU-76C/B with the MK 399 Fuse. When this empty canister is filled with leaflets it is referred to as the PDU-5/B. Due to the MK 20 canister strength, relative to the M129 fiberglass canister, this steel canister is better suited for use with high performance aircraft. Also, the M129’s use of a primer cord to separate the canister’s two halves tended to burn up many of the leaflets before they ever reached the ground. The PDU-5/B was employed extensively both in Afghanistan and Iraq as part of Operations Enduring Freedom and Iraqi Freedom. Characteristics: CRD Weapons Code Guidance Weight (lbs.) Length (in.) Diameter (in.) Payload Fuze Carriage Options: Aircraft: F-16C-D F/A-18A-F AV-8B P-3C

L051A (SUU-76C/B empty canister) Ballistic 143 empty, 295 +/- 15 lbs. with payload 94.50 13.2 Approximately 60,000 psychological leaflets MK 339 Launcher/Rack: 14 in. Lug Spacing BRU-32/BRU-33 BRU-36/BRU-42 BRU-15

Contractor / Schedule / Improvements / Special Equipment: Contractor - TBD Status Inventory Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A3-2-7, NA 11-140-9

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CHAPTER SEVEN 1 June 2009

NUCLEAR WEAPONS

FOR OFFICIAL USE ONLY

INTENTIONALLY LEFT BLANK

Nomenclature: B61

Name: Nuclear Bomb

Characteristics: B-61 Mod Weight-Full (lbs.) Length (in.) Diameter (in.) -

3, - 4, - 10 755 +/- 10 141.6 13.3

B-61 Mod - 7 Weight (lbs.) - 765.0 +/- 10 Length (in.) - 141.6 Diameter (in.) - 13.3

B-61 Mod -11 Weight (lbs.) - 1,245.0 Length (in.) 145.0 Diameter (in.) - 13.3

Aircraft: B-2A B-52H F-15E F-16A-D PA-200 (NOTE: not all aircraft are certified to carry all mods) Management/Engineering: AFMC/AF NWC, Kirtland AFB, NM Technical Order: 11N-B61-1, 11N-B61A-1, 11N-B61C-1 Status: Inventory

B61 MOD 3/4/10 IN H-1125 BOLSTER

B61 MOD 11 IN THE H-1671

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Nomenclature: B83-1 Characteristics: Weight (lbs.) Length (in.) Diameter (in.) -

Name: Nuclear Bomb

2,478 144.21 (3.66 m) 18 (460mm)

Aircraft: B-2A B-52H Management/Engineering: AFMC/AF NWC, Kirtland AFB, NM Technical Order: 11N-B83-1 Status: Inventory

B83 IN H-1473 BOLSTER

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Nomenclature: W62-0

Name: Nuclear Warhead

Characteristics: Classified Reentry System: MK12, Minuteman III Management/Engineering: AFMC/NWC, Kirtland AFB, NM Technical Order: 11N-W62-1 Status: Inventory

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Nomenclature: W78-0

Name: Nuclear Warhead

Characteristics: Classified Reentry System: MK12A, Minuteman III Management/Engineering: AFMC/NWC, Kirtland AFB, NM Technical Order: 11N-W78-1 Status: Inventory

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Nomenclature: W80-1 Characteristics: Weight (lbs.) Length (in.) Diameter (in.) -

Name: Nuclear Warhead

293.2 31.4 11.8

Carriage Options: AGM-86B (ALCM) Aircraft: B-52H Management/Engineering: AFMC/AF NWC, Kirtland AFB, NM Technical Order: 11N-W80-1 Status: Inventory

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Nomenclature: W87-0

Name: Nuclear Warhead

Characteristics: Classified Reentry System: MK21, Minuteman III Management/Engineering: AFMC/AF NWC, Kirtland AFB, NM Technical Order: 11N-W87-1 Status: Inventory

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CHAPTER EIGHT 1 June 2009

AIRCRAFT GUN SYSTEMS

FOR OFFICIAL USE ONLY

INTENTIONALLY LEFT BLANK

Name: “Minigun” Machine Gun (7.62mm)

Nomenclature: GAU-2B/A GAU-17A (Navy), M-134 (Army)

Capability: Suppress/incapacitate personnel targets and damage or destroy moving and stationary light materiel targets. The gun provides a light-weight, high rate of fire capability for helicopters and light fixed-wing aircraft. Description: The GAU-2B/A is a six barrel automatic gun chambered in 7.62x51mm. The gun can be flexible or fixed mounted and used on various rotary wing aircraft and ground systems or fixed mounted on fixed wing aircraft. The gun rate of fire is selectable for either a Low 2,000 shots per minute (SPM) or High 4,000 SPM setting. Characteristics: Gun Type Externally (electric) powered rotary (Gatling), air cooled, belt fed. Weight (lbs.) 23 Length (in.) 31.5 Cyclic Rate of Fire - 2,000 - 4,000 SPM Ammo Type Ball, Tracer, Dim Tracer, Saboted Light Armor Penetrator (SLAP) (see ammunition section for details). Aircraft: CH-53D/E (ramp mounted) HH-60J, MH-60G, MH-60K MH-60L, MH-60 DAP, SH-60, UH-1N/Y AH-6 Little Bird Note: US Army nomenclature is M134, US Navy nomenclature is GAU-17/A. Contractor / Status / Improvements / Special Equipment: Contractor - General Dynamics Armament & Technical Products Status Inventory Management/Engineering: WR-ALC/GBLE (Gun) Robins AFB, GA; 506 CBSS/GBLB (Ammo), Hill AFB, UT Technical Order: 11W1-13-5-2 (Gun); 11813-10-7 (Ammo)

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Nomenclature: GAU-8/A

Name: “Avenger” Cannon (30mm)

Capability: Suppress/incapacitate personnel targets, damage or destroy moving and stationary light materiel targets, and moving or stationary armored targets. This weapon may also be used in an air-to-air role. Description: Seven barreled automatic cannon chambered in 30x173mm. The weapon is fixed mounted on the A-10. Characteristics: Gun Type - Externally (hydraulic) powered rotary (Gatling), air cooled, double ended linkless/helical feed. Weight (lbs.) 661 Length (in.) 112.83 Diameter (in.) 12 Barrel Length (in.) 93.1 System Weight (lbs.) with TP Ammunition 3,867; Empty - 1,861 Total System Ammunition Capacity (Approx.) - 1,350 Rounds (Old Version Storage Drum) - 1,174 Rounds (New Version Storage Drum) Cyclic Rate of Fire, shots per minute (SPM) - 3,850 (+100, -300) - Nominal Ammo Type - HEI/API/TP (see ammunition section for details). Dispersion (80% dia) 5-mils Aircraft: A-10 Other Use: Goalkeeper Ship Defense system (Netherlands) (with modifications). Contractor / Status / Improvements / Special Equipment: Contractor - General Dynamics Armament & Technical Products Status Inventory Management/Engineering: WR-ALC/GBLE (Gun), Robins AFB, GA; 506 CBSS/GBLB (Ammo), Hill AFB, UT Technical Order: 11W1-12-10-2 (Gun); 11A13-14-7 (Ammo)

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Nomenclature: GAU-12/U

Name: “Equalizer” Cannon (25mm)

Capability: Suppress/ incapacitate personnel targets and damage or destroy moving and stationary light materiel targets. Description: Five barreled automatic cannon chambered in 25x137mm. The weapon is flexible mounted on a trainable gun mount on the AC-130U. Characteristics: Gun Type Externally powered rotary (Gatling), air cooled, linear linkless feed system. Weight (lbs.) 330 Length (in.) 86 Diameter (in.) 11 Cyclic Rate of Fire - 1800 shots per minute (SPM) Ammo Type Cartridge, HEI, TP (see ammunition section for details) Dispersion (80% dia) - 7 mils Aircraft: AC-130U AV-8B Harrier Other use: Modified versions used on Light Armored Vehicle-Air Defense (LAV-AD) Contractor / Status / Improvements / Special Equipment: Contractor - General Dynamics Armament & Technical Programs Status Inventory Management/Engineering: WR-ALC/GBLE (Gun), Robins AFB, GA; 506 CBSS/GBLB (Ammo), Hill AFB, UT Technical Order: 11W1-12-12-2 (Gun); 11A13-16-7 (Ammo)

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Nomenclature: GAU-18/A

Name: Machine Gun (.50 Caliber)

Capability: Suppress/incapacitate personnel targets and damage or destroy moving and stationary light materiel targets including light armor. Description: The GAU-18/A is a lightweight version of the single barrel M2/3, Browning .50 Caliber Machine Gun. It is chambered in caliber .50 (12.7x99mm) and is flexible and fixed mount capable for use on various rotary wing aircraft. It does not utilize the heavy barrel, and is typically set up as a left-hand feed, right-hand charging weapon. In this configuration the gun is fitted with a chute adapter attached to its left hand feed pawl bracket. Thus, the weapon can receive ammunition through a feed chute system connected to internally-mounted or externally-mounted ammo cans. Characteristics: Gun Type Recoil operated, air-cooled, belt fed Weight (lbs.) 65 Length (in.) 61.75 Cyclic Rate of Fire - 750 - 850 shots per minute (SPM) Ammo Type Cartridge, .50 caliber (Ball/AP/API/APIT/Saboted Light Armor Penetrator (SLAP)) (see ammunition section for details) Aircraft: HH-60J, MH-60G, SH-60, UH-60 CH-47D CH-46E CH-53D/E MH-60G MV-22B, CV-22 (Note: Similar models include XM218 (Navy and Marines use), GAU-15/A, and GAU-16/A) Other use: Worldwide use on multiple platforms (w/modifications and nomenclature change) Contractor / Status / Improvements / Special Equipment: Contractor - CAAA Status Inventory Management/Engineering: WR-ALC/GBLE (Gun), Robins AFB, GA; 506 CBSS/GBLB (Ammo), Hill AFB, UT Technical Order: 11W1-13-3-132 (Gun), 11813-10-7 (Ammo)

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Nomenclature: GAU-19/A

Name: Gatling Gun (.50 Caliber)

Capability: Suppress/incapacitate personnel targets and damage or destroy moving and stationary light materiel targets including light armor. Description: Three barrel Gatling Gun, chambered in caliber .50 Browning Machine Gun (12.7x99mm). Flexible and fixed mount capable for use on various rotary wing aircraft. This gun is used on Army helicopters, small Navy patrol boats, and on larger US warships as a defense against small suicide craft. Characteristics: Gun Type three-barrel, 12.7mm, externally powered Gatling Gun, air-cooled, belt fed Drive system electric Weight (lbs.) 560 Length (in.) 46.5 Barrel Length (in.) - 36 Cyclic Rate of Fire, shots per minute (SPM) - Maximum: 2,000 cyclic - Normal maximum: 1,000 to 2,000 cyclic Muzzle Velocity - 2,910 feet per second for M33 Ammunition Ammo Type Cartridge, .50 Caliber (Ball/AP/API/APIT/Saboted Light Armor Penetrator (SLAP)) (see ammunition section for details) Aircraft: AH-6 Little Bird Contractor / Status / Improvements / Special Equipment: Contractor - General Dynamics Status Inventory (U.S. Army) Management/Engineering: Technical Order:

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Nomenclature: GAU-21

Name: Machine Gun (.50 Caliber)

Capability: Suppress/incapacitate personnel targets and damage or destroy moving and stationary light materiel targets including light armor. Description: The GAU-21 M3M 50 .cal Machine Gun is a weapon system rather than just a machine gun. The system has three parts: The Machine Gun, the Medium Pintle Head (MPH) or “Soft Mount”, and the Cradle, which is used to integrate the weapon into a particular aircraft or vehicle. Three important differences between the MEM and the M@ BMG: 1) it uses an open bolt; 2) has an internal recoil spring, and; 3) significantly longer barrel life (est. 10,000 rounds.) Cook-offs are far less likely to occur and the M3M has only a third as much non-compensated recoil as compared to the M2 BMG. The feed system for the 600 round magazines has been modified to reduce the air stream problem and the barrel has an added flash suppressor. Characteristics: Gun Type Recoil operated, air-cooled, belt fed Weight (lbs.) 79.9 Length (in.) 59.8 Barrel Length (in.) - 36 Cyclic Rate of Fire, shots per minute (SPM) - 950 to 1,100 cyclic (- 200 SPM practical) Muzzle Velocity - 2,887 fps Ammo Type Cartridge, .50 caliber (Ball/AP/API/APIT/Saboted Light Armor Penetrator (SLAP)) (see ammunition section for details) Aircraft: CH-46 CH-53D/E HH-60 UH-1N/Y Contractor / Status / Improvements / Special Equipment: Contractor - Fabrique Nationale Herstal, S.A. Status Inventory (U.S. Marines and Navy) Management/Engineering: Technical Order:

GAU-21 mounted on ramp of CH-53E

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Nomenclature: GAU-22/A

Name: Cannon (25mm)

Capability: Neutralize Fixed Wing Aircraft and Helicopter airborne targets and destroy ground moving and stationary armored personnel carriers and light and medium materiel targets, and neutralize identified traditional and nontraditional combatants. Description: The GAU-22/A is a new gun being developed for the Conventional Takeoff and Landing (CTOL) Joint Strike Fighter (F-35/A). It is an externally powered four barrel, Gatling gun which fires at a nominal rate of 3,000 shots per minute (SPM). A modification of this gun system is being developed in a “missionized” gun pod for the Short Takeoff Vertical Landing (STOVL) aircraft version (F-35/B) and the Carrier Variant (CV) aircraft version (F-35/C). The CTOL will carry 181 rounds of 25mm and the CV/STVOL will carry 220 rounds of 25 mm. Characteristics: Gun Type Four-barrel Gatling Weight (lbs.) 250 Length (in.) 84 Diameter (in.) 6 Cyclic Rate of Fire - 3,000 Nominal SPM Ammo Types TP, TBD Combat ammunition to be defined/developed Dispersion (80% dia) 5 mils Aircraft: F-35 Contractor / Status / Improvements / Special Equipment: Contractor - Lockheed Martin Vendor General Dynamics Armament & Technical Products Status In development Notes Missionized Gun Feed System Unique Management/Engineering: Lockheed Martin (Gun); 506 CBSS/GBLB (Ammo), Hill AFB, UT Technical Order: F-35 Automated Joint Technical Data (JTD) System (Gun); 11A13-16-7 (Ammo)

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Nomenclature: M137A1

Name: Cannon (105mm)

Capability: Suppress/incapacitate personnel targets and damage/destroy moving and stationary materiel targets. Damage/breach reinforced concrete structures. Description: Single barreled manually operated cannon chambered in 105mm (M137). The weapon is flexible mounted on a trainable gun mount on the AC-130H/U. Characteristics: Gun Type Single Barrel, manually operated, manually fed System Weight (lbs.) 5,000 Length (ft.) 17.5 Practical Cyclic Rate of Fire, shots per minute (SPM) - 6-10 Ammo Type HE, HE/High Fragmentation, White Phosphorus (WP), and TP (see ammunition section for details) Dispersion (hardstand) - 0.2 mils Aircraft: AC-130H/U Other use: Worldwide use (M102 Howitzer configuration). Contractor / Status / Improvements / Special Equipment: Contractor - N/A Status Inventory Management/Engineering: WR-ALC/GBLE (Gun); Robins AFB, GA; 506 CBSS/GBLB (Ammo), Hill AFB, Technical Order: 11W1-33-7-2 (Gun); 11A13-13-7 (Ammo)

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Nomenclature: M197

Name: 20mm Gatling Gun

Capability: Suppress/incapacitate personnel targets, damage or destroy moving and stationary light materiel targets, and moving or stationary armored targets. Description: The M-197 electric cannon is a three-barreled electric Gatling Gun developed primarily for use by U.S. Army and Marine Corps gunships. It is essentially a lightened version of the General Electric M61 Vulcan, with three barrels instead of six. Its maximum rate of fire is one quarter that of the Vulcan, largely to limit its recoil for light aircraft and helicopter use. The M-197 in

the AH-1 is mated to an ammunition storage and handling system that has a capacity of 700 rounds of linked M-50 or PGU series 20mm electrically primed ammunition. The M-197 utilizes the M-89 or M-89E1 declutching feeder to delink and feed ammunition into the gun. The M-197 is attached to the A/A49E-7 (V4) turret assembly that provides the sighting, positioning (+/- 110 degrees azimuth and +30/-50 degrees elevation/depression), and firing the gun. Characteristics: Gun Type System Weight (lbs.) Length (in.) Ammo Type Rate of fire Dispersion Muzzle velocity Average recoil forceDrive system Feed System -

three Barrel, 20mm, externally powered Gatling gun 132 71-9 M50 and PGU series 20 mm ammunition 650 shots per minute (SPM) 8.0 milliradians diameter, 80 percent circle (M50) 3,380 feet per second 1,300 pounds hydraulic, electric, and pneumatic Linked or linkless

Aircraft: AH-1W Super Cobra AH-1Z Super Cobra Contractor / Status / Improvements / Special Equipment: Contractor - General Dynamics Armament and Technical Products Status Inventory Management/Engineering: US Army Tank-Automotive and Armaments Command Armament and Chemical and Logistics Activity (TACOM-ACALA) Technical Order:

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Nomenclature: M2A1

Name: “Bofors” Cannon (40mm)

Capability: Suppress/incapacitate personnel targets and damage/destroy moving and stationary materiel targets. Description: Single barreled automatic cannon chambered in 40mm (L60). The weapon is flexible mounted on a trainable gun mount on the AC-130H/U. Characteristics: Gun Type Weight (lbs.) Length (ft.) Cyclic Rate of Fire Ammo Type Dispersion (Hardstand) -

Single Barrel, automatic loader, manually fed 1,700 12 100 shots per minute (SPM) Armor Piercing Tracer (APT), HEIP (see ammunition section for details) 0.6 mils

Aircraft: AC-130H/U Other use: Worldwide use as AAA gun system (antiquated). Contractor / Status / Improvements / Special Equipment: Contractor - None Status Inventory Management/Engineering: WR-ALC/GBLE (Gun), Robins AFB, GA; 506 CBSS/GBLB (Ammo), Hill AFB, UT Technical Order: 11W1-33-8-2 (Gun); 11A13-11-7 (Ammo)

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Nomenclature: M230

Name: 30mm Chain Gun

Capability: Suppress/incapacitate personnel targets, damage or destroy moving and stationary light materiel targets, and moving or stationary armored targets. Description: The M230 is a single barrel, externally powered (3 HP electric motor), electrically fired, chain driven weapon. It is mounted in the lower section of the gun turret on the underside of the Apache Helicopter. It fires 30mm Linkless ammunition at a rate of 625 + 25 shots per minute (SPM). The M230 Gun has a positive cook-off safety (open bolt clearing) and double jam prevention. Characteristics: Gun Type externally powered (6.5 HP) Chain Gun Ammo handling system - linear linkless Ammo storage capacity - 1200 rounds M789 Rate-of-fire 625+ 25 SPM Weight (lbs.) 127 Length (in.) 66 Barrel life to 10,000 round Maximum range 4,000 m Effective range 1,500 m Ammunition used: - M788 (TP) Target Practice - M789 (HEDP) High Explosive Dual Purpose - M799 (HEI) High Explosive Incendiary - M848 DUMMY Aircraft: AH-64 Apache MH-60 DAP Contractor / Status / Improvements / Special Equipment: Contractor - McDonnell Douglas Helicopter Systems (MDHS) Status Inventory Management/Engineering: US Army Tank-Automotive and Armaments Command Armament and Chemical and Logistics Activity (TACOM-ACALA) Technical Order:

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Nomenclature: M240D

Name: Machine Gun (7.62mm)

Capability: Suppress/incapacitate personnel targets and damage or destroy moving and stationary light materiel targets. The gun provides a light-weight, self defense fire capability for rotary wing aircraft. Description: The M240D is a single barrel automatic machine gun, chambered in caliber 7.62x51 mm. Flexible and fixed mount capable for use on various rotary wing aircraft. Characteristics: Gun Type Single Barrel, Air-Cooled, Belt Fed Weight (lbs.) 65 Length (in.) 39 Cyclic Rate of Fire - 650 - 950 shots per minute (SPM) Ammo Type Cartridge, 7.62 mm (Ball/Tracer/Dim Tracer) (see ammunition section for details). Aircraft: HH-60G UH-1N/Y Other Use: Worldwide use in various configurations on vehicles and as dismounted crew served weapon. Contractor / Status / Improvements / Special Equipment: Contractor - FN Herstal Status Inventory Management/Engineering: WR-ALC/GBLE (Gun), Robins AFB, GA; 506 CBSS/GBLB (Ammo), Hill AFB, UT Technical Order: 11W2-6-5-2 (Gun); 11813-10-7 (Ammo)

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Nomenclature: M61A1

Name: “Vulcan” Cannon (20mm)

Capability: Damage/destroy aerial targets, suppress/incapacitate personnel targets, damage or destroy moving and stationary light materiel targets. Description: Six barreled automatic cannon chambered in 20x102mm. This weapon is fixed mounted on fighter aircraft. Characteristics: Gun Type -

Externally (hydraulic) powered rotary (Gatling), air cooled, double ended linkless helical or linear linkless feed. Weight (lbs.) 255 Length (in.) 72 System Weight (lbs.) - 935 Cyclic Rate of Fire - SPM 2,500 - 6,000 shots per minute (SPM); (capable up to 7200 SPM) Ammo Type API, HEI, SAPHEI, HEIT, TP, TPT (see ammunition section for details) Dispersion (80% dia) - 8 mils Aircraft: F-15A-E F-16A-D F/A-18A-F Other use: Phalanx Ship Defense System Contractor / Status / Improvements / Special Equipment: Contractor - General Dynamics Armament & Technical Products Status Inventory Management/Engineering: WR-ALC/GBLE (Gun), Robins AFB, GA; 506 CBSS/GBLB (Ammo), Hill AFB, UT Technical Order: 11W1-12-4-32 (Gun); 11A13-4-7 (Ammo)

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Nomenclature: M61A2

Name: Lightweight Cannon (20mm)

Capability: Damage/destroy aerial targets, suppress/incapacitate personnel targets, damage or destroy moving and stationary light materiel targets. Description: Light weight six barreled automatic cannon chambered in 20x102mm. This weapon is fixed mounted on fighter aircraft. Characteristics: Gun Type -

Externally (hydraulic) powered rotary (Gatling), air cooled, double ended Linkless helical or linear linkless feed. Weight (lbs.) 200 Length (in.) 71.93 System Weight (lbs.) - 860 Cyclic Rate of Fire, shots per minute (SPM) - 4,000 or 6,000 selectable. Muzzle Velocity - 1,030 m/s Ammo Type API, HEI, SAPHEI, HEIT, TP, TPT (see ammunition section for details) Dispersion (80% dia) - 8 mils Aircraft: F/A-18A-F F-22A Contractor / Status / Improvements / Special Equipment: Contractor - General Dynamics Armament & Technical Products Status Inventory Management/Engineering: WR-ALC/GBLE (Gun), Robins AFB, GA; 506 CBSS/GBLB (Ammo), Hill AFB, UT Technical Order: 11W1-12-4-32 (Gun); 11A13-4-7 (Ammo)

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Nomenclature: Mk44

Name: “Bushmaster” Cannon (30mm)

Capability: Suppress/incapacitate personnel targets and damage/destroy moving and stationary materiel targets. Description: Light weight single barreled automatic cannon chambered in 30x173mm. Characteristics: Gun Type -

Externally (electrical) powered, single barreled, (Chain Gun), air cooled, linear linkless or clip (manual) feed. Weight (lbs.) 341 Length (ft.) 12 Cyclic Rate of Fire - 200 shots per minute (SPM) Ammo Type HEI/TP Dispersion (80% dia) - 0.5 mils USAF Aircraft: None Other Use: Use in various configurations on Armored Vehicles and Maritime craft. Also being tested for USN Rapid Mine Clearing System (RAMICS). Contractor / Status / Improvements / Special Equipment: Contractor - ATK/Boeing Status Inventory Management/Engineering: WR-ALC/GBLE (Gun), Robins AFB, GA; 506 CBSS/GBLB (Ammo), Hill AFB, UT Technical Order: 11W1-12-16-2 (Gun);

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INTENTIONALLY LEFT BLANK

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CHAPTER NINE 1 June 2009

IMPULSE CARTS, BOMB RACKS, LAUNCHERS and PYLONS

FOR OFFICIAL USE ONLY

INTENTIONALLY LEFT BLANK

Nomenclature: ARD 446-1B

Name: Impulse Cartridge

Description: The general function of this cartridge is to jettison bombs and external stores (i.e., weapons, pylons, racks, etc.) from the aircraft. This cartridge is mainly used by the USAF. It is electrically fired from aircraft power and has a defined shelf and service life. It is interchangeable with the Navy CCU-43/B (which is going obsolete) and CCU-106/B. Dimensions: Length (in.) - 1.812 Diameter (in.) - 1.075 Weight (lbs.) - 0.075 Operation: Cartridge has a one amp, one watt hero capacity Aircraft: Various Management/Engineering: 506 CBSS/GBLA, Hill AFB, UT Technical Order: 11A18-7-7

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Nomenclature: ARD 863-1A1W

Name: Impulse Cartridge

Description: The general function of this cartridge is to jettison bombs and external stores (i.e., weapons, pylons, racks, etc.) from the aircraft. This cartridge is mainly used by the USAF. It is electrically fired from aircraft power and has a defined shelf and service life. It is interchangeable with the Navy CU-44/B (which is going obsolete) and CCU-107/B. Dimensions: Length (in.) - 1.030 Diameter (in.) - 1.075 Weight (lbs.) - 0.053 Operation: Cartridge has a one amp, one watt hero capacity Aircraft: Various Management/Engineering: 506 CBSS/GBLA, Hill AFB, UT Technical Order: 11A18-7-7

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Nomenclature: BBU-35/B

Name: Impulse Cartridge

Description: This is a cylindrical aluminum case containing a firing electrode, bridge-wire, and propellant to generate gas pressure and eject chaff payload out of a plastic chaff cartridge into the aircraft slipstream to disperse several thousand various frequency reflective dipole elements. It is electrically fired from aircraft power and has a defined shelf and service life. Dimensions: Length (in.) - 0.50 Diameter (in.) - 0.625 (flange) 0.49 (body) Weight (lbs.) - 0.0103 Aircraft: Various Dispenser: All ALE-40 Series Countermeasure: RR-170 and RR-180 Chaff; and M206, M211, M212, MJU-46, MJU-48/B, MJU-50 and MJU-51 flares Operation: Cartridge has one amp, one watt no fire, and 4.25 watt all fire Management/Engineering: 506 CBSS/GBLA, Hill AFB, UT Technical Order: 11A16-39-7 and 11A16-40-7

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Nomenclature: BBU-36/B

Name: Impulse Cartridge

Description: This is a cylindrical aluminum case containing a firing electrode, bridge-wire, and propellant to generate gas pressure, heat/flame to ignite and eject flare payload out of an aluminum cartridge into the aircraft slipstream as a countermeasure to IR missiles. It is electrically fired from aircraft power and has a defined shelf and service life. Dimensions: Length (in.) - 0.55 Diameter (in.) - 0.805 (flange) 0.740 (body) Weight (lbs.) - 0.0209 Operation: Cartridge has one amp, one watt no fire, and 4.25 watt all fire Aircraft: Various Dispenser: ALE-40 Series Countermeasure: MJU-7, MJU-10/B, MJU-40/B, and MJU-47/B IR Flares Management/Engineering: 506 CBSS/GBLA, Hill AFB, UT Technical Order: 11A16-40-7 and 11A16-43-7

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Nomenclature: BBU-46/B & A/B

Name: Impulse Cartridge

Description: The general function of cartridge BBU-46/B is to use gas pressure to push the flare’s piston and the flare pellet out of the ejector tube into the aircraft’s slipstream for ignition of the flare pellet. The BBU-46A/B impulse cartridge functions in a similar manner. The main difference is it provides hot gas for ignition of the flare pellet after ejection from the ejector tube. It is electrically fired from aircraft power and has a defined shelf and service life. Dimensions: Length (in.) - 0.55 Diameter (in.) - 1.805 Weight (lbs.) - 0.75 Operation: Cartridge has one amp, one watt no fire, and 4.25 watt all fire Aircraft: B-1B Dispenser: ALE-49 Countermeasure: MJU-23 Management/Engineering: 506 CBSS/GBLA, Hill AFB, UT Technical Order: 11A16-46-7

9-5

FOUO

Nomenclature: BBU-48/B

Name: Impulse Cartridge

Description: This is a cylindrical aluminum case containing a circuit board with two firing electrodes, bridgewires, and two cylinders with propellant charges. When fired separately, each cylinder contains propellant to generate gas pressure and eject two payloads off into the aircraft slipstream to disperse several thousand various frequency reflective dipole elements. The general function of this cartridge is to use gas pressure to push the chaff cartridge piston and payload out of the chaff cartridge. This will disperse chaff dipole elements into the aircraft slipstream. It is electrically fired from aircraft power and has a defined shelf and service life. Dimensions: Length (in.) - 0.65 Diameter (in.) - 0.975 Weight (lbs.) - 0.0159 Aircraft: Various Operation: Cartridge has one amp, one watt no fire, and 4.25 watt all fire Dispenser: All ALE-40 Series Countermeasure: RR-180 Management/Engineering: 506 CBSS/GBLA, Hill AFB, UT Technical Order: 11A16-45-7

9-6

FOUO

Nomenclature: BBU-59/B

Name: Impulse Cartridge

Description: This cartridge is used to eject flares from the F-22A. It consists of a bridge-wire ignition mix, booster, and main propellant charge in a sealed housing. It is a case grounded electrically fired cartridge with 1A1W no-fire. Shelf and service life are applicable to this cartridge. Dimensions: Length (in.) Diameter (in.) Weight (lbs.) Net Explosive Weight (lbs.) -

0.65 1.120 (flange), .956 (body) Unknown ~0.0043

Aircraft: F-22A Management/Engineering: 506 CBSS/GBLA, Hill AFB, UT Technical Order: 11A16-43-7

9-7

FOUO

Nomenclature: BBU-63/B

Name: Impulse Cartridge

Description: This cartridge is used to eject stores from BRU-44 Bomb Rack and is used exclusively by the USAF. It consists of a bridge-wire initiated igniter, two booster charges and a main propellant charge in a sealed aluminum case. It is a non-case grounded electrically fired cartridge with 1A1W no-fire. The latest version is anodized for better corrosion protection. Shelf and service life are applicable to this cartridge. Dimensions: Length (in.) Diameter (in.) Weight (lbs.) Net Explosive Weight (lbs.) -

2.650 1.238 (flange), 1.110 (body) 0.147 0.0556

Aircraft: Aircraft: B-2A

Launcher/Rack: BRU-44 bomb rack

Management/Engineering: 506 CBSS/GBLA, Hill AFB, UT Technical Order: 11A18-7-7

9-8

FOUO

Nomenclature: M796

Name: Impulse Cartridge

Description: This is a cylindrical aluminum case containing a firing electrode, bridge-wire, and propellant to generate gas pressure, heat/flame to ignite and push the flare ejections and payload out of an aluminum cartridge into the aircraft slipstream as a countermeasure to IR missiles. It is electrically fired from aircraft power and has a defined shelf and service life. Dimensions: Length (in.) - 0.50 Diameter (in.) - 0.625 (flange) 0.49 (body) Weight (lbs.) - 0.0110 Operation: Cartridge has one amp, one watt no fire, and 4.25 watt all fire Aircraft: RU-2, H-58, AH-1, RV-1, OV-1D, UH-1, RC-12, C-12, UC-35, UH-60, HH-60, EH-60, CH-47, AH-64 Dispenser: ALE-40 Series, M130, AN/ALQ-212(V) Countermeasure: M206 Aircraft Countermeasure Flare, M212 Aircraft Countermeasure Flare, M211 Infrared Countermeasure Decoy Management/Engineering: US Army RDECOM ARDEC AMSRD-AAR-AEE-W, Bldg. 21 Picatinny, NJ 07806-5000 Technical Order: 11A16-41-7

9-9

FOUO

Nomenclature: MK 107

Name: Impulse Cartridge

Description: The Impulse Cartridge MK 107 Mod 1 is electrically initiated. The cartridge consists of a screwin type steel case with an O-ring, steel-trap plate containing approximately one gram of propellant and a closure disc. The main charge of the cartridge is approximately 24 grams of double base propellant. Cartridge threads are coated with a dry film lubricant. Dimensions: Length (in.) - 4.35 Diameter (in.) - 1.737 (body), charged end diameter 1.253 Weight (lbs.) - 0.0110 Operation: When the cartridge is fired, the resulting gas pressure operates the store release/ejector mechanism. The recommended firing current is 10+/- 0.5 amps. It is used in the Navy MXU611 Fuel Tank Release Mechanism and LAU-93A (Phoenix Missile) Launcher and in the Air Force B-1B Rotary Launcher. Aircraft: B-1B Dispenser: Power source in launchers and jettison release mechanisms. Management/Engineering: 506 CBSS/GBLA, Hill AFB, UT Technical Order: 11P-1-27DB-1

9-10

FOUO

Nomenclature: 14-Inch Bomb Rack

Name: Bomb Rack

Description: The 14-inch ejector rack assembly provides the means for the carriage and release of airborne stores with 14-inch lug spacing. It is installed in the conventional bomb module. The 14-inch ejector rack assembly consists of a linkage mechanism supported between two side plates held together by two cast steel end blocks. These end blocks support the hooks and attach to the conventional bomb module structure. The rack is a compact device lying completely within a 3-inch wide envelope bounded by the two side plates. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

27.00 3.00 7.00 36.5

Aircraft: B-1B Management/Engineering: 575 CBSS/GBLE, Robins AFB, GA Technical Order: 11B29-3-56-11 FORWARD

9-11

FOUO

Nomenclature: A-6 Bomb Release

Name: Bomb Release (Left and Right Hand)

Description: The Type A-6 release is an electrically actuated, spring loaded, mechanical trigger, which actuates the levers on the bomb shackle attached to the cluster bomb rack. Each bomb and shackle combination, when mounted in a bomb rack, requires either a right or a left hand release in order to actuate the shackle and release the bomb. Both right and left hand releases are required in any bomb rack. The functioning parts of the release, except the arms, which engage the bomb shackle, are contained in the protective coated die-case AMS4291 aluminum arm and release housing assembly, which has a sealed cover and connector on the backside. However, internal hardware, release and salvo solenoids and springs are identical in both units. Both configurations of the Type A-6 release perform the same function. Dimensions: Length (in.) - 5.75 Width (in.) - 4.0 Height (in.) - 1.5 Weight (lbs.) - 3.0 Aircraft: B-52H Management/Engineering: 575 CBSS/GBLE, Robins AFB, GA Technical Order: 11B38-2-5-1

9-12

FOUO

Nomenclature: AERO 7A-5

Name: Bomb Rack Ejector Assembly

Description: The Navy and Marine Corps use the AERO 7A-5 Bomb Ejector Rack Assembly. Stores include the MK 80, Mines, Pods (countermeasure/jamming system), 14 and 30 inch suspension. It uses cantered ejector cartridges. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) - 50 Aircraft: EA-6B Management/Engineering: NAVAIRSYSCOM PMA-201, NAS Patuxent River, MD Technical Order: NAVAIR 11-5D20

AERO 7A-5 Bomb Ejector Rack Assembly

9-13

FOUO

Nomenclature: AERO 7B-4

Name: Bomb Rack Ejector Assembly

Description: The Navy and Marine Corps use the AERO 7B-4 Bomb Ejector Rack Assembly. Stores include the MK 80, Mines, Pods (countermeasure/jamming system), 14 and 30 inch suspension. It uses cantered ejector cartridges. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) - 50 Aircraft: F/A-18A-F Management/Engineering: NAVAIRSYSCOM PMA-201, NAS Patuxent River, MD Technical Order: NAVAIR 11-5D-20

AERO 7B-4 Bomb Ejector Rack Assembly

9-14

FOUO

Nomenclature: B-11 Bomb Shackle

Name: Bomb Shackle

Description: The B-11 shackle uses a mechanical interface system with the cluster bomb rack assembly to operate the release mechanism of the shackle. Upon actuation, the shackle releases stores between 100 and 1,600 lbs. The B-11 shackle incorporates two hooks in tandem with a 14 inch suspension capability. Dimensions: Length (in.) - 16.00 Width (in.) - 0.625 Height (in.) - 4.125 Weight (lbs.) - 5.00 Aircraft: B-52H Management/Engineering: 575 CBSS/GBLE, Robins AFB, GA 540 ACSS/GFLCB, Tinker AFB, OK Technical Order: 11B40-2-4-3

9-15

FOUO

Nomenclature: BRU-15/A

Name: Bomb Rack

Description: The Navy uses the BRU-15A on the wing stations of the P-3C. Stores include the AGM-84D Harpoon and the PDU-5/B MK 20 Rockeye II Leaflet Canister. This bomb release unit provides suspension and release of conventional and nuclear weapon/stores of up to 2,000 pounds with 14-inch suspension (Aero 1A adapter assemblies may be attached to increase the bomb rack to 30-inch suspension capability). It uses ejector cartridges. It connects to the aircraft special weapons release and control system to provide cable-actuated manual release, auxiliary unlock, and mechanical arming of a weapon/store. Linear Electromechanical Actuator consists of a spring-loaded plunger that is mechanically locked and electrically released, providing the force to initiate hook release. Mechanical arming of a weapon/store is accomplished through two electrically actuated arming solenoids, which are mounted in the frame assembly. The BRU-15 is capable of suspension and release of a weapon/store in either an armed or safe condition. A safety mechanism is provided to positively lock the release mechanism when a safety pin is installed. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) - 17 lbs TYPE Bomb Rack (Gravity) Aircraft: MQ-9 P-3C Management/Engineering: NAVAIRSYSCOM PMA-201, NAS Patuxent River, MD Technical Order: NAVAIR 11-5E-18

9-16

FOUO

Nomenclature: BRU-32A/A

Name: Ejector Unit Rack Assembly

Description: The Navy and Marine Corps use the BRU-32A/A Ejector Unit Rack Assembly. Stores include the MK 80/GBU Series, Mines (Aircraft laid), JDAM, , PODS (Reconnaissance/Jamming Systems), Launchers, 14 inch Suspension. It uses ejector cartridges. Dimensions: Length (in.) - 37 Width (in.) - 7.3 Height (in.) - 7.5 Weight (lbs.) - 76.25 TYPE Ejector Unit Rack Assembly (Ejector Cartridges) Aircraft: F/A-18A-D Management/Engineering: NAVAIRSYSCOM PMA-201, NAS Patuxent River, MD Technical Order: AW-382AC-750-000

9-17

FOUO

Nomenclature: BRU-32B/A

Name: Ejector Unit Rack Assembly

Description: The Navy and Marine Corps use the BRU-32B/A Ejector Unit Rack Assembly. Stores include the MK 80/GBU Series, Mines (Aircraft laid), JDAM, PODS (Reconnaissance/Jamming Systems), Launchers, 14 inch Suspension. It uses ejector cartridges. Dimensions: Length (in.) - 37 Width (in.) - 7.3 Height (in.) - 7.5 Weight (lbs.) - 76.25 TYPE Ejector Unit Rack Assembly (Ejector Cartridges) Aircraft: F/A-18AE-F Management/Engineering: NAVAIRSYSCOM PMA-201, NAS Patuxent River, MD Technical Order: AW-382AC-750-000

BRU-32B/A Ejector Unit Rack Assembly

9-18

FOUO

Nomenclature: BRU-33A/A

Name: Canted Vertical Ejector Rack (CVER)

Description: The BRU-33A/A CVER incorporates a 5.5-degre cant to each ejector unit to improve weapon separation characteristics. It has 14-in. hooks and is capable of carrying two stores ranging from 10 to 16 in. in diameter and weighing up to 1,000 lb. each. It is attached to the BRU-32 Bomb rack. Store ejection is accomplished by two cartridge-generated gas pressure ejectors. The rack provides for automatic sway-bracing through the use of spring-loaded, self-adjusting wedges. The Navy and Marine Corps use the BRU-33A/A Rack Assembly. Dimensions: Length (in.) - 69.8 Width (in.) - 29.3 Height (in.) - 10.1 Weight (lbs.) - 200 TYPE Vertical Ejector Rack Assembly (Cantered) (Ejector Cartridges) Aircraft: F/A-18A-F Management/Engineering: NAVAIRSYSCOM PMA-201, NAS Patuxent River, MD Technical Order: AW-382AC-750-010

BRU-33A/A Ejector Rack Assembly

9-19

FOUO

Nomenclature: BRU-36A/A

Name: Bomb Ejector Rack

Description: The Marine Corps uses the BRU-36A/A Bomb Ejector Rack. Stores include the MK 80 Series, MK 20 Series, PODS (Countermeasure/Jamming Systems), 14 inch Suspension. It uses ejector cartridges. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) - 29.00 TYPE Aircraft Bomb Ejector Rack (Ejector Cartridges) Aircraft: AV-8B Management/Engineering: NAVAIRSYSCOM PMA-201, NAS Patuxent River, MD Technical Order: AW-380VB-MIB-000

9-20

FOUO

Nomenclature: BRU-36B/A

Name: Bomb Ejector Rack

Description: The Marine Corps uses the BRU-36A/A Bomb Ejector Rack. Stores include the MK 80 Series, MK 20 Series, PODS (Countermeasure/Jamming Systems), 14 inch Suspension. It uses ejector cartridges. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) - 29.00 TYPE Aircraft Bomb Ejector Rack (Ejector Cartridges) Aircraft: AV-8B Management/Engineering: NAVAIRSYSCOM PMA-201, NAS Patuxent River, MD Technical Order: AW-380VB-MIB-000

9-21

FOUO

Nomenclature: BRU-41/A

Name: Improved Multiple Ejector Rack (IMER)

Description: The BRU-41/A IMER is capable of carrying up to six stores, each store weighting up to 1,000 lb. A cartridge-activated mechanism is used to provide for store ejection. The rack weights 282 lbs. and provides the necessary interface for store sensing, arming, and ejector breech firing. Firing sequence is back to front of center, left, then right stations. The Navy uses the BRU-41/A IMER. Stores include practice bombs (MK-76 and BDU-48, LGTR, LUU-2, ITALD, 14 inch Suspension. It uses ejector cartridges. Dimensions: Length (in.) - 156 Width (in.) - 16 Height (in.) - 18 Weight (lbs.) - 282 TYPE Improved Multiple Ejector Rack (Ejector Cartridges) Aircraft: F/A-18A-F Management/Engineering: NAVAIRSYSCOM PMA-201, NAS Patuxent River, MD Technical Order: NAVAIR 11-75A-603

9-22

FOUO

Nomenclature: BRU-42/A

Name: Improved Triple Ejector Rack (ITER)

Description: The BRU-41/A ITER is capable of carrying up to three stores, each store weighing up to 1,000 lb. A cartridge-activated mechanism is used to provide for store ejection. The rack provides the necessary interface for store sensing, arming, and ejector breech firing. Firing sequence is centerline, left shoulder, right shoulder. The Navy and Marine Corps use the BRU42/A. Stores include the Practice Bombs MK-76 and BDU-48, MK-58, LGTR, LUU-2, ITALD, MK 80 series. Dimensions: Length (in.) - 67 Width (in.) - 16 Height (in.) - 18 Weight (lbs.) - 112 TYPE Improved Triple Ejector Rack (Ejector Cartridges) Aircraft: AV-8B F/A18A-F Management/Engineering: NAVAIRSYSCOM PMA-201, NAS Patuxent River, MD Technical Order: NAVAIR 11-75A-603

9-23

FOUO

Nomenclature: BRU-44B/A

Name: Bomb Rack

Description: The ejector has electrically fired impulse cartridges that drive a gas-operated mechanism. The ejector is equipped with two sets of shackles, one set spaced 14 inches apart and one set spaced 30 inches apart, connected by a linkage system to a center bell crank from which the hooks can be manually opened or closed. The ejector is designed to carry conventional or nuclear weapons or external fuel tanks, and is designed to resist the elements of a nuclear blast exposure. The ejector is composed of two side plate assemblies, a top panel, a shackle and linkage assembly, two piston assemblies, two orifice blocks, a gas tube assembly, a gas generator assembly, three arming solenoids, an in-flight safety lock assembly, and a wire harness assembly. Dimensions: Length (in.) - 32.00 Width (in.) - 3.0 Height (in.) - 11.25 (including sway brace pads), 8.0 (excluding sway brace pads) Weight (lbs.) - 95.00 Aircraft: B-2A Management/Engineering: 575 CBSS/GBLE, Robins AFB, GA Technical Order: 11B29-3-70-1

9-24

FOUO

Nomenclature: BRU-46/A

Name: Bomb Rack

Description: The BRU-46/A rack uses electrically fired dual impulse cartridges to generate gas pressure to operate the rack’s release and eject mechanism. Upon actuation, the rack release/eject mechanism forcibly ejects, or free fall releases, conventional stores (not nuclear capable) up to and including 500 lb weight class. The BRU-46/A rack incorporates two hooks in tandem providing 14 inch suspension capability (not 30 inch suspension capable). Each sway brace arm pivots and locks independently of the others to engage the store. Dimensions: Length (in.) - 26.90 Width (in.) - 2.00 Height (in.) - 6.00 Weight (lbs.) - 41.90 Aircraft: BRU-57/A Smart Rack F-15E F-22A Management/Engineering: 575 CBSS/GBLE, Robins AFB, GA Technical Order: 11B29-3-60-2

9-25

FOUO

Nomenclature: BRU-47/A

Name: Bomb Rack

Description: The BRU-47/A rack uses electrically fired dual impulse cartridges to generate gas pressure to operate the rack’s release and eject mechanism. Upon actuation, the rack release/eject mechanism forcibly ejects, or free fall releases, conventional and special stores up to and including 5000 lb weight class. The BRU-47/A rack incorporates four hooks in tandem providing 14 and 30 inch suspension capability. Each sway brace arm pivots and locks independently of the others to engage the store. Dimensions: Length (in.) - 35.70 Width (in.) - 3.00 Height (in.) - 6.70 Weight (lbs.) - 87.50 Aircraft: F-15E F-22A Management/Engineering: 575 CBSS/GBLE, Robins AFB, GA Technical Order: 11B29-3-61-2

9-26

FOUO

Nomenclature: BRU-52

Name: Bomb Rack

Description: This release device is used as the interface between the Bomb Rack Assembly (BRA) and the bomb. It contains the electrical and mechanical components that allow the bomb to be released from the BRA. The release device is used for carrying and releasing up to and including 1,000 lb. class stores with 14 inch lug spacings. A cocked release device may be released by an electrical signal or with a manually applied load. It can be locked in the cocked position by inserting a cable-controlled safing pin in the mechanism. The release device includes two arming solenoids a release solenoid, and a transfer switch. All solenoids incorporate diodes to prevent back Electromotive Force (EMF), and connecting circuits have Electromagnetic Interference (EMI) protection. Dimensions: Length (in.) - 7.125 Width (in.) - 11.50 Height (in.) - 6.00 Weight (lbs.) - 9.50 Aircraft: B-2A Management/Engineering: 575 CBSS/GBLE, Robins AFB, GA Technical Order: 11B29-3-68-3

9-27

FOUO

Nomenclature: BRU-55/A

Name: Bomb Ejector Rack

Description: The Navy uses the BRU-55/A Bomb Ejector Rack. Stores include JDAM. It uses ejector cartridges. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) - 236 TYPE Aircraft Bomb Ejector Rack (Ejector Cartridges) Aircraft: F/A-18C-F Management/Engineering: NAVAIRSYSCOM PMA-201, NAS Patuxent River, MD Technical Order: NAVAIR 11-75A-56

9-28

FOUO

Nomenclature: BRU-56/A

Name: Aircraft Ejector Bomb Rack (A.K.A. 30 Inch Ejector Rack)

Description: The BRU-56/A rack uses electrically fired dual impulse cartridges (MK107) to generate gas pressure to operate the racks release and eject mechanism. Upon actuation, the rack release/eject mechanism forcibly ejects conventional stores up to 4000 lbs. The BRU-56/A rack incorporates two hooks in tandem providing 30 inch suspension capability. Each sway brace arm must be manually adjusted to engage the store. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

38.00 7.952 (w/o sway braces) 5.75 (rack only); 13.25 (rack with pistons); 14.50 (rack with pistons and sway braces) 90.00

Aircraft: B-1B Management/Engineering: 575 CBSS/GBLE, Robins AFB, GA 327 BMSG/GFCC, Tinker AFB, OK Technical Order: 11N-H5086-2

9-29

FOUO

Nomenclature: BRU-57/A

Name: Smart Bomb Rack

Description: The BRU-57/A allows carriage of two smart weapons (up to 1,000 lb class) on a single aircraft station. The rack uses MIL-STD-1760 for aircraft-to-rack and rack-to-weapon interface. The rack is currently used with the Joint Stand-Off Weapon (JSOW) and Wind Corrected Munitions Dispenser (WCMD) configured munitions. Future expansion is planned for other MIL-STD-1760 compatible aircraft and weapon systems. The BRU-57/A strongback attaches to aircraft with 30 inch suspension and both BRU-46/A racks have two hooks in tandem providing 14 inch suspension capability. Each sway brace arm pivots and locks independently of the others to engage the store. Configuration Specifics: BRU-57/A (Air Force) BRU-33 vertical ejector rack strongback, 2 BRU-46 ejector units Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

69.80 29.00 7.10 250.00

Aircraft: F-16 (two Precision Guided Munition (PGM) carriage) Management/Engineering: 575 CBSS/GBLE, Robins AFB, GA Technical Order: 11B29-3-71-1 BRU-57 for the F-16 with two BRU-46/A Bomb Release Units

9-30

FOUO

Nomenclature: BRU-59/A

Name: Bomb Ejector Rack

Description: The Navy and Marine Corps use the BRU-59A Bomb Ejector Rack. Stores include the LAU-61, LAU-68 Rocket Pod, M299 Hellfire Launcher Aircraft Bomb Ejector Rack (ejector carftridge). Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) - 12.6 Aircraft: AH-1Z UH-1N UH-1Y Management/Engineering: Technical Order: NAVAIR 11-75A-55

BRU-59/A Aircraft Bomb Ejector Rack

9-31

FOUO

Nomenclature: BRU-61/A

Name: Common Carriage Assembly

Description: The BRU-61/A is suspended from the aircraft parent bomb rack and uses the aircraft MIL-STD1760 electrical interface at each aircraft station. The BRU-61/A carriage system provides carriage of four GBU-39/B weapons. BRU-61/A carriage systems will generally be delivered loaded with munitions to each operating location munitions storage area. The interface electronics in the carriage system provide a method to distribute the weapons status, control release sequence, and initiate the INS/GPS signals to all weapons on the dispenser. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

126.40 14.00 10.20 320.00

Aircraft: F-15E Objective: B-2A Management/Engineering: 575 CBSS/GBLE, Robins AFB, GA Technical Order: 11B29-3-73-1

BRU-61/A with 4 GBU-39/B

9-32

FOUO

Nomenclature: BRU-67/A

Name: Bomb Rack

Description: The BRU-67/A has 14 inch hooks and uses a high pressure pneumatic system to safely eject and separate weapons/stores. The rack contains a Pneumatic Power Module (PPM) with two pressure vessel’s containing 5000 PSI. The rack incorporates a semi-automatic swaybrace that is integral with the ejector piston to restrain the movement of the weapon/store during captive and employment mode. The rack has three installed Zero Retention Force (ZRF) electromechanical arming units, one forward, center and aft. Additionally, the rack has four Positive Arming Units (PAU) on the operating side of the rack. The rack has a selectable pitch setting control along with a dump valve to vent the pneumatic energy contained in the pressure vessels. The rack has a safe/arm lever which provides a visual status of the condition of the rack and has four positions, safe, safe and unlocked, armed and download. A Reversible InFlight Locking (RIFL) mechanism is incorporated to provide electromechanical safing/arming and is spring biased to fail-safe to the safe mode. The RIFL incorporates a firing circuit interrupt that prevents the rack from firing until the system is armed. The rack also provides for automatic safing when both hooks are properly latched. The rack is currently only used in the weapons bay of the F-35/B (Short Take Off and Vertical Landing STOVL) variant of the F-35. Dimensions: Length (in.) - 33.67 Width (in.) - 4.0 Height (in.) - 12.84 Weight (lbs.) - 65.00 Aircraft: F-35B Management/Engineering: Lockheed Martin Aerospace, Fort Worth, Tx Technical Order: F-35 Automated Joint Technical Data (JTD) system

9-33

FOUO

Nomenclature: BRU-68/A

Name: Bomb Rack

Description: The BRU-68/A has 14 inch and 30 inch hooks and uses a high pressure pneumatic system to safely eject and separate weapons/stores. The rack contains a Pneumatic Power Module (PPM) with two pressure vessel’s containing 5000 PSI. The rack incorporates a semi-automatic swaybrace that is integral with the ejector piston to restrain the movement of the weapon/store during captive and employment mode. The rack has three installed Zero Retention Force (ZRF) electromechanical arming unit’s, one forward, center and aft. Additionally, the rack has four Positive Arming Units (PAU) on the operating side of the rack. The rack has a selectable pitch setting control along with a dump valve to vent the pneumatic energy contained in the pressure vessels. The rack has a safe/arm lever which provides a visual status of the condition of the rack and has four positions, safe, safe and unlocked, armed and download. A Reversible InFlight Locking (RIFL) mechanism is incorporated to provide electromechanical safing/arming and is spring biased to fail-safe to the safe mode. The RIFL incorporates a firing circuit interrupt that prevents the rack from firing until the system is armed. The rack also provides for automatic safing when both hooks are properly latched. The rack is currently used in the weapons bay of the F-35A/C (Common Take Off and Landing (CTOL) and Carrier Variant (CV) variant of the F-35 internal and externally on all F-35 variants. Dimensions: Length (in.) - 36.78 Width (in.) - 85.5 Height (in.) - 4.0 Weight (lbs.) - 85.5 Aircraft: F-35/A/B/C Management/Engineering: Lockheed Martin Aerospace, Fort Worth, Tx Technical Order: F-35 Automated Joint Technical Data (JTD) system

9-34

FOUO

Nomenclature: CBR

Name: Cluster Bomb Rack

Description: There are three Cluster Bomb Rack Assemblies installed in the bomb bay area of the B-52H aircraft. Each Cluster Bomb Rack Assembly consists of two outboard grids and one inboard grid, supported by a forward support beam and aft support beam. Each rack has three pairs of hooks to support the Type B-11 bomb shackle. Type A-6 bomb releases (one for each pair of hooks) are mounted on the racks to actuate the shackles. The forward and aft support beams, which support the two outboard and one in-board grid, are secured to the fuel tank deck with rack support fittings. Dimensions: Length (in.) - 80.0 Width (in.) 22.0 Weight (lbs.) - 306.0 Aircraft: B-52H Management/Engineering: 575 CBSS/GBLE, Robins AFB, GA 540 ACSS/GFLCB, Tinker AFB, OK Technical Order: 11B29-3-21-2WP 002 00

9-35

FOUO

Nomenclature: MA-4

Name: Family of 14” Bomb Racks

Description: Types MA-4A and MA-4B bomb racks are manufactured by Handley Industries Inc. This equipment is a two-hook bomb rack for internal or external installation in trainer fighters, support and cargo aircraft. It will carry a bomb up to and including 1600 pounds, carry and release chemical bombs and, when combined with a pylon, will accommodate jettisonable fuel tanks. Dimensions: Length (in.) 17.09375 Width (in.) 1.40625 Weight (lbs.) 7 Hook Spacing (in.) - 14 Maximum load ability: 10,000 pounds Ambient temperature range: 54°C to 73.6°C (-65°F to 1600°F) Voltage: 18 to 28 V dc Aircraft: C-130, AT-38B, and Special Application Aircraft Management/Engineering: 575 CBSS/GBLE, Robins AFB, GA Technical Order: 11B29-3-8-3

9-36

FOUO

Nomenclature: MAU-12

Name: Bomb Rack

Description: The MAU-12 rack uses electrically fired dual impulse cartridges to generate gas pressure to operate the racks release and eject mechanism. Upon actuation, the rack release/eject mechanism forcibly ejects, or free fall releases, conventional or nuclear stores up to and including 5000 lb weight class or external fuel tanks. The MAU-12 rack incorporates 4 hooks in tandem providing 14 and 30 inch suspension capability. Each sway brace arm must be manually adjusted to engage the store. Dimensions: Length (in.) - 32.00 Width (in.) - 3.00 Height (in.) - 6.26 Weight (lbs.) - 70.00 Aircraft: AC-130H and U B-52H F-15 F-16 MC-130H Talon II Management/Engineering: 575 CBSS/GBLE, Robins AFB, GA Technical Order: 11B29-3-25-2

9-37

FOUO

Nomenclature: MAU-40/A

Name: Bomb Rack

Description: The MAU-40/A rack uses electrically fired dual impulse cartridges to generate gas pressure to operate the racks release and eject mechanism. Upon actuation, the rack release/eject mechanism forcibly ejects, or free fall releases, conventional stores (not nuclear capable) up to and including 5000 lb weight class or external fuel tanks. The MAU-40/A rack incorporates four hooks in tandem providing 14 and 30 inch suspension capability. The MAU-40A is essentially a MAU-12 except it does not contain the safety wiring and in-flight safety lock for nuclear munitions. Each sway brace arm must be manually adjusted to engage the store. Dimensions: Length (in.) - 32.00 Width (in.) - 3.00 Height (in.) - 6.246 Weight (lbs.) - 69.00 Aircraft: A-10 AC-130H and U MC-130H Talon II Management/Engineering: 575 CBSS/GBLE, Robins AFB, GA Technical Order: 11B29-3-39-2

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Nomenclature: MAU-50/A

Name: Bomb Rack

Description: The MAU-50/A rack uses electrically fired dual impulse cartridges to generate gas pressure to operate the racks release and eject mechanism. Upon actuation, the rack release/eject mechanism forcibly ejects, or free fall releases, conventional stores (not nuclear capable) and/or external fuel tanks up to 2000 lbs with a diameter between nine and 30 inches. The MAU-50/A rack incorporates two hooks in tandem providing 14 inch suspension capability (not 30 inch suspension capable). Each sway brace arm must be manually adjusted to engage the store. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

27.75 3.00 6.125 45.00

Aircraft: A-10 Management/Engineering: 575 CBSS/GBLE, Robins AFB, GA Technical Order: 11B29-3-40-2

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Nomenclature: SBRA

Name: Smart Bomb Rack Assembly

Description: The Smart Bomb Rack Assembly (SBRA) is a modified Bomb Rack Assembly with the additional of a left and right wired junction box assembly, a Smart Bomb Release Controller (SBRC) and umbilical cables that allow the SBRA to support a partial or full load of 20 MIL-STD-1760 weapons, in addition to the load configurations of the BRA. The SBRA consists of a BRA with the addition of two wired junction box assemblies mounted on the aft end of the two stanchion assemblies, two modified aft clip-in latch/lock drives, and a new Smart Bomb Release Controller (SBRC). The SBRC is the only Mission Management Subsystem (MMS) Line Replaceable Unit (LRU) installed on the SBRA. The electrical system is modified by the addition of a primary power cable and 20 umbilical cables. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

72.80 65.30 71.40 1,347.00 to 1,677.00 (Depending on Configuration)

Aircraft: B-2A Management/Engineering: 575 CBSS/GBLE, Robins AFB, GA Technical Order: 11-B29-3-66-1

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Nomenclature: SUU-20

Name: Bomb Dispenser

Description: The SUU-20/A dispenser attaches to aircraft with 14 and 30 inch lug suspension and is capable of launching four 2.75 inch diameter Folding Fin Aircraft Rocket (FFAR) and six practice bombs. Stores fired from this launcher are ignited and rocket thrust propels store to slide forward, disengaging from launcher, and flying to target. Practice bombs are ejected by a gas-driven piston ram and free-fall to the target. Both rockets and bombs can be fired in a single mode or a ripple mode. The SUU-20/A dispenser provides mechanical and electrical interface between rocket/bomb and aircraft. Dimensions: Length (in.) 122.00 Height/Width (in.) - 19.30 X 12.25 (Elliptical Shape) Weight (lbs.) 241.00 to 330.00 (Depending on Configuration) Aircraft: F-15 F-16 Management/Engineering: 575 CBSS/GBLE, Robins AFB, GA Technical Order: 11B29-3-28-1

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Nomenclature: TER-9/A

Name: Bomb Rack

Description: The TER-9/A uses electrically fired impulse cartridges (three total, one per rack) to generate gas pressure to operate the racks release and eject mechanism. Upon actuation, the rack release/eject mechanism forcibly ejects, or free fall releases, conventional stores (not nuclear capable) up to 1000 lbs each. Each rack can carry stores with a diameter between 9 and 16 inches (max diameter of 18.6 when loaded single). Stores can be fired independently or simultaneously with ripple delay, and a firing order of center, left, and right. The TER-9/A bomb rack strongback attaches to aircraft with 30 inch suspension and each of the three stores racks have two hooks in tandem providing 14 inch suspension capability only. Each sway brace arm must be manually adjusted to engage the store. Dimensions: Length (in.) - 67.00 Width (in.) - 15.00 Height (in.) - 16.00 Weight (lbs.) - 93.00 Aircraft: A-10 F-16 Management/Engineering: 575 CBSS/GBLE, Robins AFB, GA Technical Order: 11B29-3-35-2

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Nomenclature: TER-9/A MOD

Name: Bomb Rack (High Speed)

Description: The Modified TER-9/A uses electrically fired impulse cartridges (three total, one per rack) to generate gas pressure to operate the rack’s release and eject mechanism. Upon actuation, the rack release/eject mechanism forcibly ejects, or free fall releases, conventional stores (not nuclear capable) up to 1000 lbs each. Each rack can carry stores with a diameter between nine and 16 inches (max diameter of 18.6 when loaded single). Stores can be fired independently or simultaneously with ripple delay, and a firing order of center, left, and right. The MODIFIED TER-9/A bomb rack strongback attaches to aircraft with 30 inch suspension and each of the three stores racks have two hooks in tandem providing 14 inch suspension capability only. Each sway brace arm must be manually adjusted to engage the store. The skin of the MODIFIED TER-9/A is aerodynamically shaped to enhance drag coefficient and covered with spray-on radar absorbent material. Dimensions: Length (in.) - 67.00 Width (in.) - 15.00 Height (in.) - 16.00 Weight (lbs.) - 105.00 Aircraft: F-16 Management/Engineering: 575 CBSS/GBLE, Robins AFB, GA Technical Order: 11B29-3-35-2

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Nomenclature: TER-9/A MOD

Name: Bomb Rack (Electronic)

Description: The Modified TER-9/A uses electrically fired impulse cartridges (three total, one per rack) to generate gas pressure to operate the racks release and eject mechanism. Upon actuation, the rack release/eject mechanism forcibly ejects, or free fall releases, conventional stores (not nuclear capable) up to 1000 lbs each. Each rack can carry stores with a diameter between nine and 16 inches (max diameter of 18.6 when loaded single). Stores can be fired independently, or simultaneously with ripple delay, and a firing order of center, left, and right. The Modified TER-9/A bomb rack strongback attaches to aircraft with 30 inch suspension and each of the three stores racks have two hooks in tandem providing 14 inch suspension capability only. Each sway brace arm must be manually adjusted to engage the store. The Electronic TER-9/A was modified from an analog to a digital configuration in order to enhance the station transfer response time. The end result is to make the TER-9/A more compatible with the F-16 signal and eliminate hung stores. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs) -

67.00 15.00 16.00 105.00

Aircraft: F-16 Management/Engineering: 575 CBSS/GBLE, Robins AFB, GA Technical Order: 11B29-3-35-2

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Nomenclature: 16S210

Name: Guided Missile Launcher

Description: The 16S210 launcher is hard bolted to the aircraft and is capable of launching a single AIM-9 (Sidewinder) missile. The 16S210 launcher provides mechanical and electrical interface between missile and aircraft. Stores fired from this launcher are ignited and missile thrust propels store to slide forward, disengaging from launcher, and flying to target. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

105.00 3.00 5.00 Approximately 70.00

Aircraft: F-16 Management/Engineering: 575 CBSS/GBLD, Robins AFB, GA Technical Order: 11L1-2-16-2

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Nomenclature: AGMBRL

Name: Aircraft Guided Missile and Bomb Rotary Launcher

Description: The B-52H can carry one Aircraft Guided Missile and Bomb Rotary Launcher (AGMBRL). The launcher will suspend and forcibly release eight conventional or nuclear stores. The launcher’s eight stand-alone MAU-12 bomb racks incorporate four hooks in tandem providing 14 and 30 inch suspension capability. This configuration provides a total payload in excess of 20,000 lbs. Dimensions: Length (in.) Diameter (in.) Weight (lbs.) -

267.00 15.00 (Launcher shaft) 40.00 (Cable reel) 2,616.00 (Basic launcher)

Aircraft: B-52H Management/Engineering: 540 ACSS/GFLCB, Tinker AFB, OK Technical Order: 11N-L5001-2

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Nomenclature: CBM

Name: Conventional Bomb Module

Description: The Conventional Bomb Module (CBM) will suspend and forcibly eject up to 28 ea MK-82 Air Inflatable Retarder (AIR) bombs, 28 ea MK36 Destructors. When the module is installed in any of the three aircraft weapons bays, the rotary launcher drive subsystem is mechanically locked and electronically disabled by the aircraft avionics control unit (ACU) software. The CBM incorporates two hooks in tandem with a 14 inch suspension capability. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

178.00 69.96 57.66 2,816.00 to 3,513.00

Aircraft: B-1B Management/Engineering: 575 CBSS/GBLE, Robins AFB, GA Technical Order: 11B29-3-55-1

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Nomenclature: DRA

Name: Dual Rail Adapter

Description: The Dual Rail Adapter (DRA) structure assembly is compromised of an extruded aluminum upper body which is stiffened with forward, mid, and aft bulkheads. The forward and mid bulkheads provide the attachment points for mounting two LAU-105 launchers. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

57.00 14.30 7.00 57.00

Aircraft: A-10 Management/Engineering: 416 SCMS/GUMBC, Hill AFB, UT Technical Order: 31S5-4-3032-1

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Nomenclature: LAU-7/A-6, B/A, Name: Guided Missile Launcher /A-7, B/A-1, C/A, D/A, E/A, and F/A Description: The LAU-7 series of guided missile launcher is a rail-type launcher for carrying and launching the AIM-9 missile family and instrumentation (LATR/TACTS/etc.) pods. The LAU-7 missile launcher carries an internal cooling source for missile seeker cooling and power supply. The launcher weighs 90 lb. (includes 4 lb. of nitrogen) and provides for complete system interface. The LAU-7/A-6, /A-7, B/A, B/A-1, C/A, D/A, and E/A versions can carry and launch the AIM-9M missile and instrumentation pod variants. The LAU-7D/A and E/A versions have digital power supplies and are also authorized to carry and launch the AIM-9X missile variant. The LAU-7C/A and E/A are the only launcher variants that include the High Pressure Pure Air Generator (HiPPAG) cooling system for seeker head cooling; all other variants contain an internal nitrogen bottle for AIM-9M missile seeker cooling. The LAU-7/A-6 is used by the Navy and Marine Corps. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

110 4.2 5.4 90 to 93 (including nitrogen bottle)

Aircraft: Launcher Variant used F/A-18C-F LAU-7/A-6, LAU-7B/A, LAU-7B/A-1, LAU-7D/A, LAU-7E/A, LAU-7F/A F/A-18A-B LAU-7/A-7 AV-8B LAU-7C/A AH-1W LAU-7C/A AH-1Z LAU-7C/A Management/Engineering: NAVAIRSYSCOM PMA-201, NAS Patuxent River, MD Technical Order: NAVAIR 11-75A-54

LAU-7E/A Aircraft Guided Missile launcher

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Nomenclature: LAU-10C/B, D/B

Name: Guided Missile Launcher

Description: The LAU-10C/B or LAU-10D/B launchers are used to fire the Navy MK 71 Zuni 5 inch rockets. The LAU-10 Launcher can fire in single or ripple mode. These launchers have an external thermal coating that greatly prolongs cook-off protection time. The 5.0 Inch Rocket launchers are a cylindrical construction of four aluminum launch tubes. These launch tubes are held together with metal ribs and are covered by an aluminum skin. Launchers can be fitted with forward and aft frangible fairings depending on overall rocket length and fuzing for airborne configuration. The launchers are mated mechanically to the aircraft by way of suspension lugs. The 5.0 Inch Rocket launchers use either a 14 inch or 30 inch suspension. Electrical connection between the aircraft and the launcher is made through an electrical receptacle located on top of the launcher center section to the aircraft’s 28 volt armament circuit. The launchers may be shipped and stored pre-loaded with rocket motors. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

90 to 93 (including nitrogen bottle)

Aircraft: F/A-18A-F AV-8B

LAU-10 Series Launcher

Management/Engineering: NAVAIRSYSCOM PMA-201, NAS Patuxent River, MD Technical Order: NAVAIR 11-75A-92

LAU-10 Series Launcher

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Nomenclature: LAU-61C/A

Name: 2.75-inch Rocket Launcher

Description: The LAU-61C/A Navy/Marine Corps launcher can be used on high and low speed aircraft and helicopters. It attaches to aircraft with 14 inch lug suspension and is capable of launching nineteen 2.75 inch diameter, Mk 66 Series Wrap Around Folding Fin Aircraft Rockets (WAFFAR). The LAU-61C/A (19 rounds) rocket launcher is thermally coated. The launcher can be fired in single (one at a time) or ripple (one after the other in multiple shots) mode. In ripple mode, the LAU-61C/A can fire 19 rounds in about one second. There are no service life requirements on the launcher. The launchers are mated mechanically to the aircraft by way of suspension lugs. Electrical connection between the aircraft and the launcher is made through an electrical receptacle located on top of the launcher center section to the aircraft’s 28 volt armament circuit. The launchers may be shipped and stored pre-loaded with rocket motors (clusters). The launchers are a cylindrical construction of 19 aluminum launch tubes. These launch tubes are held together with glue and metal bands and are covered by an aluminum skin. Launchers can be fitted with forward and aft frangible fairings (as required) depending on overall rocket length for airborne configuration. Dimensions: Length (in.) Diameter (in.) Weight (lbs.) -

83.2 Airborne configuration w/fairings 16.0 594 Loaded w/19 Mk 66 motors w/M151 HE Warheads

Carriage Options: Aircraft: AH-1W and AH-1Z UH-1N and UH-1Y AV-8B F/A-18

Launcher/Rack: LAU-61C/A LAU-61C/A LAU-61C/A LAU-61C/A

Capacity: 19 ea 2.75-inch rockets Contractor / Status / Improvements / Special Equipment: Contractor - Arnold Defense and Electronics Status - Inventory Improvements - Insensitive Munitions (Launcher Thermal Coating) Special Equipment - N/A Management/Engineering: Navy NSWC IHDIV, Indian Head, MD Technical Manual: NAVAIR 11-75A-92

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Navy/Marine Corps LAU-61C/A Rocket Launcher (19 Tubes)

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Nomenclature: LAU-68A/A, B/A, D/A and LAU-131/A

Name: 2.75-inch Rocket Launcher

Description: The LAU-68A/A, LAU-68B/A, and the LAU-131/A launchers can be used on high and low speed aircraft and helicopters. They attach to aircraft with 14 inch lug suspension and are capable of launching seven 2.75 inch diameter MK-4 or MK-40 Folding Fin Aircraft Rocket (FFAR). The LAU-131/A has additional capability to fire seven MK-66 Wrap-Around Folding Fin Aircraft Rockets (WAFFAR). The LAU-68D/A Navy/Marine Corps launchers fire only the MK-66 Rockets (seven). The Navy/Marine Corps launchers are different in they have thermal coating which during exposure to fire will increase the time to potential detonation of rockets. Stores fired from this launcher are ignited and rocket thrust propels store to slide forward, disengaging from launcher and flying to target. The forward frangible fairing disintegrates on rocket impact and the rear fairing acts as a funnel to direct debris away from the launch aircraft. Rockets can be fired in single or ripple mode. The LAU-68/LAU-131 launcher provides mechanical and electrical interface between rocket and aircraft. Dimensions: Length (in.) Diameter (in.) Weight (lbs.) -

61.29 (83.2 Airborne configuration with fairings) 9.80 86 (LAU-68) (247 when loaded with 7 MK66 motors with 151 HE Warheads) 97 (LAU-131)

Carriage Options: Aircraft: A-10 F-16A-D AH-1W and AH-1Z UH-1N and UH-1Y AV-8B F/A-18

Launcher/Rack: LAU-68A/A, LAU-68B/A, LAU-131/A LAU-68A/A, LAU-68B/A, LAU-131/A LAU-68D/A LAU-68D/A LAU-68D/A LAU-68D/A

Capacity: 7 ea 2.75-inch rockets Contractor / Status / Improvements / Special Equipment: Contractor - Arnold Defense and Electronics Status - Inventory Improvements - Insensitive Munitions Special Equipment - N/A Management/Engineering: 506 CBSS/GBLA, Hill AFB, UT Navy NSWC IHCIV, Indian Head, MD Technical Order: 11L1-3-27-1 Navy Technical Manual: NAVAIR 11-75A-92

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Navy/Marine Corps LAU-68D/A Rocket Launcher (Seven Tubes)

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Nomenclature: LAU-88

Name: Guided Missile Launcher

Description: The LAU-88A/A launcher attaches to aircraft with 30 inch lug suspension and is capable of launching up to three AGM-65A, B, or D model Maverick missiles. The LAU-88A/A launcher provides mechanical and electrical interface between missile and aircraft. Stores are fired independently with a firing order of outboard, bottom and inboard. Stores fired from this launcher are ignited and missile thrust propels store to slide forward, disengaging from launcher, and flying to target. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

93.43 27.80 17.54 469.00

Aircraft: A-10 F-15E (requires ADU-578 Missile Launcher Adapter) F-16 Management/Engineering: 507 CBSS/GBLA, Hill AFB, UT Technical Order: 11L1-2-22-1

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Nomenclature: LAU-105/A

Name: Guided Missile Launcher

Description: The LAU-105/A launcher attaches directly to aircraft pylon/adapter and is capable of launching a single AIM-9 Sidewinder missile. The LAU-105/A launcher provides mechanical and electrical interface between missile and aircraft. Stores fired from this launcher are ignited and missile thrust propels store to slide forward, disengaging from launcher, and flying to target. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

90.90 2.80 5.20 53.00

Aircraft: A-10 B-52H (captive carry only) Management/Engineering: 575 CBSS/GBLD, Robins AFB, GA Technical Order: 11L1-2-29-2

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Nomenclature: LAU-106A/A

Name: Guided Missile Launcher

Description: The LAU-106A/A launcher attaches directly to the aircraft fuselage and is capable of suspending and launching/ejecting a single AIM-7 or AIM-120 missile. The LAU-106A/A launcher uses electrically fired dual impulse cartridges to generate gas pressure to operate the release and eject mechanisms. The LAU-106A/A launcher also provides mechanical and electrical interface between missile and aircraft. Stores fired from this launcher are first jettisoned away from the aircraft, then ignite and fly to their target. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

54.30 4.00 8.00 52.00

Aircraft: F-15A - E Management/Engineering: 575 CBSS/GBLD, Robins AFB, GA Technical Order: 11L1-3-29-2

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Nomenclature: LAU-115C/A

Name: Guided Missile Launcher

Description: The LAU-115C/A (133 lb maximum) is a rail-type guided missile launcher that carries and launches the AIM-7 series missiles. The LAU-115C/A has provisions for mounting two LAU-127 launchers for AIM-9 or AIM-120 missiles. A jettison adapter is attached to some LAU-115 launchers for improved jettison characteristics. The adapter weighs 35 lb. The LAU-115C/A is used by the Navy and Marine Corps. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

82 7 12 133 (Maximum)

Aircraft: F/A-18A-D Management/Engineering: NAVAIRSYSCOM PMA-201, NAS Patuxent River, MD Technical Order: NAVAIR 11-75A-115 (AW-394AC-750-000)

LAU-115C/A Aircraft Guided Missile launcher

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Nomenclature: LAU-115D/A

Name: Guided Missile Launcher

Description: The LAU-115C/A is used by the Navy and Marine Corps. Stores include AIM-7 Sparrow, AIM-9, and AIM-120. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

82 7 10 120

Aircraft: F/A-18E-F Management/Engineering: NAVAIRSYSCOM PMA-201, NAS Patuxent River, MD Technical Order: NAVAIR 11-75A-115 (AW-394AC-750-000)

LAU-115D/A Aircraft Guided Missile launcher

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Nomenclature: LAU-116/A

Name: (LH/RH) Guided Missile Launcher

Description: The LAU-116/A guided missile launcher is an ejector-type launcher for carrying and launching an AIM-7 missile on the two fuselage stations (4 and 6). The LAU-116/A is used by the Navy and Marine Corps. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

44 9.5 16 65

Aircraft: F/A-18A-B Management/Engineering: NAVAIRSYSCOM PMA-201, NAS Patuxent River, MD Technical Order: NAVAIR 11-75A-116 (AW-394AC-750-010)

LAU-116/A (LH/RH) Aircraft Guided Missile launcher

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Nomenclature: LAU-116A/A

Name: (LH/RH) Guided Missile Launcher

Description: The LAU-116A/A guided missile launcher is an ejector-type launcher for carrying and launching the AIM-7 or AIM-120 missile on the two fuselage stations (4 and 6). The LAU-116A/A is used by the Navy and Marine Corps. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

44 9.5 16 65

Aircraft: F/A-18C-D Management/Engineering: NAVAIRSYSCOM PMA-201, NAS Patuxent River, MD Technical Order: NAVAIR 11-75A-116 (AW-394AC-750-010)

LAU-116A/A (LH/RH) Aircraft Guided Missile launcher

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Nomenclature: LAU-116B/A

Name: (LH/RH) Guided Missile Launcher

Description: The LAU-116B/A is used by the Navy and Marine Corps. Stores include AIM-7 Sparrow and AIM-120 AMRAAM. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

44 9.5 16 65

Aircraft: F/A-18E-F Management/Engineering: NAVAIRSYSCOM PMA-201, NAS Patuxent River, MD Technical Order: NAVAIR 11-75A-116 (AW-394AC-750-010)

LAU-116B/A (LH/RH) Aircraft Guided Missile launcher

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Nomenclature: LAU-117(V)2/A

Name: Guided Missile Launcher

Description: The LAU-117(V)2/A launcher attaches to aircraft with 14 inch or 30 inch lug suspension and is capable of launching a single AGM-65 Maverick missile (all models). The LAU-117(V)2/A launcher provides mechanical and electrical interface between missile and aircraft. Stores fired from this launcher are ignited and missile thrust propels store to slide forward, disengaging from launcher, and flying to target. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

94.00 11.00 11.00 125.00 to 145.00

Aircraft: AV-8B F/A-18A-F P-3C Management/Engineering: NAVAIRSYSCOM PMA-201, NAS Patuxent River, MD Technical Order: NAVAIR 11-75A-79

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Nomenclature: LAU-117A(V)3/A

Name: Guided Missile Launcher

Description: The LAU-117A(V)3/A launcher attaches to aircraft with 14 inch or 30 inch lug suspension and is capable of launching a single AGM-65 Maverick missile (all models). The LAU-117A(V)3/A launcher provides mechanical and electrical interface between missile and aircraft. Stores fired from this launcher are ignited and missile thrust propels store to slide forward, disengaging from launcher, and flying to target. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

94.00 11.00 11.00 125.00 to 145.00

Aircraft: A-10 F-15E F-16 AV-8B F/A-18A-F P-3C Management/Engineering: 507 CBSS/GBLA, Hill AFB, UT Technical Order: 11L1-2-15-1

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Nomenclature: LAU-118(V)1/A

Name: Guided Missile Launcher

Description: The LAU-118(V)1/A launcher attaches to aircraft with 30 inch lug suspension and is capable of launching a single AGM-88 High-Speed Anti-Radiation Missile (HARM). The LAU-118(V)1/A launcher provides mechanical and electrical interface between missile and aircraft. Electrical interface is provided through the Aircraft Launcher Interface Computer (ALIC). Stores fired from this launcher are ignited and missile thrust propels store to slide forward, disengaging from launcher, and flying to target. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

79.00 11.65 (across top of housing assembly) 8.00 (excluding attach lugs) 120.00

Aircraft: F-16 F/A-18A-F EA-6B Management/Engineering: NAVAIRSYSCOM PMA-201, NAS Patuxent River, MD Technical Order: NAVAIR 11-75A-78

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Nomenclature: LAU-118A(V)4/A

Name: Guided Missile Launcher

Description: The LAU-118A(V)4/A launcher attaches to aircraft with 30 inch lug suspension and is capable of launching a single AGM-88 High-Speed Anti-Radiation Missile (HARM). The LAU-118A(V)4/A launcher provides mechanical and electrical interface between missile and aircraft. Electrical interface is provided through the Aircraft Launcher Interface Computer (ALIC) (enables launcher to be used on F-16’s). Stores fired from this launcher are ignited and missile thrust propels store to slide forward, disengaging from launcher, and flying to target. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

79.00 11.65 (across top of housing assembly) 8.00 (excluding attach lugs) 120.00

Aircraft: F-16 F/A-18A-F EA-6B Management/Engineering: 575 CBSS/GBLD, Robins AFB, GA Technical Order: 11L1-2-20-1

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Nomenclature: LAU-127A/A, B/A D/A, and E/A

Name: Guided Missile Launcher

Description: The LAU-127A/A, LAU-127B/A, LAU-127D/A, and LAU-127E/A guided missile launchers are a rail-type launcher are capable of carrying and launching a single AIM-9 (Sidewinder) family of missiles or AIM-120 Advanced Medium Range Air-to-Air Missile (AMRAAM). They contain a power supply and a supply of nitrogen coolant. The LAU-127A/A, LAU-127B/A LAU-127D/A, and LAU-127E/A launchers attach to the aircraft with two external attachment bolts. These launchers provide mechanical and electrical interface between the missile and the aircraft. Stores fired from these launchers are ignited and missile thrust propels the store to slide forward, disengaging from the launcher, and flying to the target. These launchers are US Navy launchers and they utilize nitrogen stored in a bottle inserted in the aft end of the launcher to cool the seeker of the AIM-9 missile. These launchers are used mainly for under-wing carriage on the aircraft. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) Aircraft: F/A-18A-F

107.75 3.37, 6.43 (at fin retainer) 6.09 LAU-127A/A: 95.9 max (with full nitrogen receiver) LAU-127B/A: 98.5 max (with full nitrogen receiver) LAU-127D/A: 95.9 max (with full nitrogen receiver) LAU-127E/A: 98.5 max (with full nitrogen receiver)

Management/Engineering: 575 CBSS/GBLA, Robins AFB, GA Technical Order: NAVAIR 11-75A-514

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Nomenclature: LAU-127C/A, F/A

Name: Guided Missile Launcher

Description: The LAU-127C/A and LAU-127F/A are capable of launching a single AIM-9 (Sidewinder) family of missiles or AIM-120 Advanced Medium Range Air-to-Air Missile (AMRAAM). The LAU-127C/A and LAU-127F/A launchers attach to the aircraft with two external attachment bolts. This launcher provide mechanical and electrical interface between the missile and the aircraft. Stores fired from this launcher are ignited and missile thrust propels the store to slide forward, disengaging from the launcher, and flying to the target. This launcher is a US Navy launcher and utilizes compressed air from a HiPPAG unit inserted in the aft end of the launcher to cool the seeker of the AIM-9 missile. These launchers are used mainly for wing-tip carriage on the aircraft. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

118.75 3.37, 6.43 (at fin retainer) 6.09 LAU-127 C/A: 117 max (with HiPPAG) LAU-127 F/A: 117 max (with HiPPAG)

Aircraft: F/A-18E-F Management/Engineering: 575 CBSS/GBLA, Robins AFB, GA Technical Order: NAVAIR 11-75A-514

9-68

FOUO

Nomenclature: LAU-128A/A, D/A

Name: Guided Missile Launcher

Description: The LAU-128A/A, D/A (BIT capabilities removed and replaced with dummy parts) launcher requires the use of an ADU-552, Missile Launcher Adapter, to provide ample missile stabilizer wing clearance for launch. This adapter is hard-mounted to the pylon and the launcher is hardmounted to the adapter with two external attachment bolts. The LAU-128A/A, D/A is capable of launching a single AIM-9 (Sidewinder) or AIM-120 Advanced Medium Range Air-to-Air Missile (AMRAAM). The LAU-128A/A, D/A launcher provides mechanical and electrical interface between missile and aircraft. Stores fired from this launcher are ignited and missile thrust propels store to slide forward, disengaging from launcher, and flying to target. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

103.14 3.71 6.09 87.00

Aircraft: F-15A - E Management/Engineering: 575 CBSS/GBLA, Robins AFB, GA Technical Order: 11L1-2-24-2

9-69

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Nomenclature: LAU-128B/A

Name: Guided Missile Launcher (BOL)

Description: The LAU-128B/A launcher requires the use of an ADU-552, Missile Launcher Adapter, to provide ample missile stabilizer wing clearance for launch. This adapter is hard-mounted to the pylon and the launcher is hard-mounted to the adapter with two external attachment bolts. The LAU-128B/A is capable of launching a single AIM-9 (Sidewinder) or AIM-120 (AMRAAM). The LAU-128B/A launcher provides mechanical and electrical interface between missile and aircraft. Stores fired from this launcher are ignited and missile thrust propels store to slide forward, disengaging from launcher, and flying to target. This launcher includes the AN/ALE-58 BOL Countermeasures Dispenser which allows the aircrew to dispense chaff or infrared expendables in order to prevent tracking of the aircraft. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

136.38 8.82 6.09 131.0

Aircraft: F-15A-B Management/Engineering: 575 CBSS/GBLA, Robins AFB, GA Technical Order: 11L1-2-24-2

9-70

FOUO

Nomenclature: LAU-129A/A

Name: Guided Missile Launcher

Description: The LAU-129A/A launcher attaches to aircraft with three external attachment bolts. The LAU-129A/A is capable of launching a single AIM-9 (Sidewinder) family of missile or AIM-120 Advanced Medium Range Air-to-Air Missile (AMRAAM). The LAU-129A/A launcher provides mechanical and electrical interface between missile and aircraft. Stores fired from this launcher are ignited and missile thrust propels store to slide forward, disengaging from launcher, and flying to target. There are also five other versions of the LAU-129 produced strictly for foreign military sales. These are the LAU-129B/A, the LAU-129C/A, the LAU-129D/A, the LAU-129E/A and the LAU-129F/A. The only difference between these launchers is the material they are coated with or the color of the coating. All parts are the same as the LAU-129A/A. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

102.98 3.62 6.00 90.00

Aircraft: F-16 Management/Engineering: 575 CBSS/GBLA, Robins AFB, GA Technical Order: 11L1-2-30-1

9-71

FOUO

Nomenclature: LAU-139

Name: Guided Missile Launcher

Description: The LAU-139 is capable of launching a single AIM-9 (Sidewinder) family of missiles or AIM-120 Advanced Medium Range Air-to-Air Missile (AMRAAM). The LAU-139 launcher attaches to the aircraft with two external attachment bolts. This launcher provides mechanical and electrical interface between the missile and the aircraft. Stores fired from this launcher are ignited and missile thrust propels the store to slide forward, disengaging from the launcher, and flying to the target. This launcher is a US Navy Foreign Military Sales (FMS) launcher and utilizes nitrogen stored in a bottle inserted in the aft end of the launcher to cool the seeker of the AIM-9 missile. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

107.75 3.37, 6.43 (at fin retainers) 6.09 95.9 max (with full nitrogen receiver)

Aircraft: Saab JAS-39A Grippen Management/Engineering: 575 CBSS/GBLA, Robins AFB, GA Technical Order: (FMS) 11-75A-139

9-72

FOUO

Nomenclature: LAU-141/A

Name: Configurable Rail Launcher (CRL)

Description: The LAU-141/A Configurable Rail Launcher (CRL) is a trapeze, rail-type launcher used to suspend and launch AIM-9M and AIM-9X (Sidewinder) missiles. The CRL consists of the rail assembly, forward and aft trapeze arms, hydraulic actuator, and AIM-9 power supply. One CRL is installed in the left and right side weapons bays on the F-22A aircraft. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

104.0 9.0 20.0 retracted, 37.0 extended 128

Aircraft: F-22A Management/Engineering: Lockheed-Martin Corporation, Ft. Worth, TX Technical Order: Interactive Electronic Technical Manual

9-73

FOUO

Nomenclature: LAU-142/A

Name: AMRAAM Vertical Eject Launcher (AVEL)

Description: The LAU-142/A AMRAAM Vertical Ejection Launcher (AVEL) is designed to carry, launch, and jettison AIM-120C (AMRAAM) missiles on F-22A aircraft. The mechanism is driven by a hybrid hydraulic/pneumatic actuator. The launchers are internally mounted in the left and right main weapons bays (three per bay). Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

41.0 8.5 14.0 retracted, 23.0 extended 117

Aircraft: F-22A Management/Engineering: Lockheed-Martin Corporation, Ft. Worth, TX Technical Order: Interactive Electronic Technical Manual

9-74

FOUO

Nomenclature: LAU-144/A

Name: Munitions Launcher Assembly (A.K.A. Multi-purpose Rotary Launcher (MPRL) or 180 Inch Rotary Launcher)

Description: The B-1B can carry up to three Munitions Launcher Assemblies in three weapons bays. Each launcher will suspend and release eight GBU-31, AGM-154, AGM-158 or MK-84 conventional stores. The Munitions Launcher Assembly provides the electrical, mechanical, and pneumatic interface between aircraft and stores. It incorporates eight BRU-56/A racks with two hooks in tandem with a 30 inch suspension capability. Dimensions: Length (in.) - 178.00 Diameter (in.) (w/o stores) - Approximately 41.00 Weight (lbs.) w/ejectors (w/o stores) - 1,300.00 to 2,055.00 (Depending on Configuration) Aircraft: B-1B Management/Engineering: 707 MSUS, Tinker AFB, OK Technical Order: 11N-L5002-2

9-75

FOUO

Nomenclature: LAU-147/A

Name: Missile Launcher

Description: The LAU-147/A launcher is designed to eject launch the AIM-120 missile from the internal weapons bay of the F-35A/B/C. The launcher uses a high pressure pneumatic system to safely eject and separate AIM-120 series missiles. The launcher contains a Pneumatic Power Module (PPM) with two pressure vessel’s containing 5000 PSI. The launcher incorporates a swaybrace that is integral with the ejector piston to restrain the movement of the weapon/store during captive and employment mode. The launcher has a safe/arm lever which provides a visual status of the condition of the rack and has four positions, safe, safe and unlocked, armed and download. A Reversible In-Flight Locking (RIFL) mechanism is incorporated to provide electromechanical safing/arming and is spring biased to fail-safe to the safe mode. The RIFL incorporates a firing circuit interrupt that prevents the rack from firing until the system is armed. Dimensions: Length (in.) - 43.02 Width (in.) - 4.0 Height (in.) - 6.9 Weight (lbs.) - 62.4 Aircraft: F-35A/B/C Management/Engineering: Lockheed Martin Aerospace, Fort Worth, Tx Technical Order: F-35 Automated Joint Technical Data (JTD) system

9-76

FOUO

Nomenclature: LAU-148/A

Name: External Rail Launcher

Description: The LAU-148/A is used on the F-35 aircraft for external carriage and launching a single AIM-9X or AIM-120 AMRAAM. The launcher provides mechanical and electrical interface between the missile and aircraft. The LAU-148/A is hard-mounted to the aircraft via either an external pylon station or an External Missile Adapter using 2 attachment tension bolts and 1 electrical interface connection to a Missile Remote Interface Unit (MRIU) internal to the launcher. Store fired from this launcher is ignited and resultant thrust propels the store to slide forward, disengaging from the launcher and flying to its target. Included with each launcher is a mass representative Gas Generation System Mass Model (GGSMM) to preserve mass/CG properties for future capability to launch AIM-132 ASRAAM. Dimensions: Length (in.) - 115-inches Width (in.) - 5-inches Height (in.) - 6.39-inches Weight (lbs.) - 100.2-pounds Store Class: Air to Air Aircraft: F-35A/B/C Management/Engineering: Lockheed Martin Aerospace, Fort Worth, Tx Technical Order: F-35 Automated Joint Technical Data (JTD) system

9-77

FOUO

Nomenclature: M299

Name: Missile Launcher

Description: The M299 Longbow Missile Launcher is a state of the art digital design that allows the launcher to interface with a variety of helicopters and to recognize and fire all AGM-114 Hellfire variants in any sequence. Designed for ease of maintenance, the M299 comprises four line replaceable units (LRUs), which can be replaced by an aviation unit with a 30-minute mean-time-to-repair. Built-in test capabilities identify malfunctions without removing the launcher from the aircraft. The launcher is compatible with fielded test sets to simplify maintenance. This launcher is also modified for use on the MQ-9 Reaper and the MQ-1 Predator (see Modified M229). The M229 features: MIL-STD-1760 interface Digital 1553 data bus compatibility Four missile capacity Fires any Hellfire missile, in any order Embedded training missile emulation Two-level maintenance design Dimensions: Dimensions (4 missiles) (in.) - 22X29 Weight (lbs) - 145 (empty); 541 (loaded with 4AGM-114K missiles Aircraft: AH-64D Apache MH-64 Seahawk AH-1W/Z Super Cobra

UH-1N/Y AH-6

Contractor: Lockheed Martin Missiles and Fire Control; Marvin Engineering Company Management/Engineering: Redstone Arsenal, Huntsville, AL Technical Order: TM 1-1520-Longbow/Apache EM 0126 MIL-STD-1760 Umbilical Connector

Standard 14-inch lugs

Interconnect CCA LEA CCAs Power Supply Dual Missile Interface (2) Processor Electrical Bonding Spring Latch

Safe/Arm Switch Knob

Launch Rail

Microswitch

M299 Missile Launcher is made by the US Army for the Longbow Apache

9-78

FOUO

Nomenclature: Modified M299

Name: Missile Launcher Rail

Description: The M299 Longbow Missile Launcher is modified for use on the MQ-9 Reaper and the MQ-1 Predator. The MQ-9 Reaper carries two modified M299 missile launchers. Each modified M299 launcher has two rails, with a MIL-STD-1760A aircraft interface. The MQ-1 Predator houses the modified M299 launcher electronics assembly (LEA) in the aft avionics bay. Cables are routed from the LEA to the launcher rails on the Predator wings to provide launch communication to Hellfire missiles. The launcher electronics can handle all Hellfire missile variants; the Air Force MQ-1 and MQ-9 with “P” software employ Hellfire II missiles (AGM114P/P-2A/P-2B, AGM-114M-6, AGM-114N-6, and AGM-114K/K-2/K-2A). Dimensions: MQ-9 M299 Launcher Length (in.) - 58.0 Width (in.) - 21.0 Height (in.) - 11.0 Weight (lbs) - 93.0

MQ-1 M299 Rail Length (in.) Width (in.) Height (in.) Weight (lbs) -

58.0 3.0 5.0 37.0

Aircraft: MQ-1B Predator Unmanned Aerial Vehicle (UAV) MQ-9 Reaper UAV Contractor: Missiles/Fire Control and Marvin Engineering Company M299; General Atomics (GA) at San Diego, Ca modifies the four rail M299 long bow version to a two rail MQ-9 M299 version. Management/Engineering: Redstone Arsenal, Huntsville, AL; 658 AESG Det 3, San Diego, CA Technical Order: TM 1-1520-Longbow/Apache EM 0126 Modified M299 MQ-9 Launcher Modified M299 MQ-1 Rail

M299 Missile Launcher is made by the US Army for the Longbow Apache

9-79

FOUO

Nomenclature: RLA

Name: Advanced Application Rotary Launcher (A.K.A. Rotary Launcher Assembly)

Description: The B-2A can carry two Advanced Application Rotary Launchers. The launcher will suspend and forcibly eject, or free fall, eight, conventional or nuclear stores up to and including 5000 pound weight class. The launchers eight stand-alone BRU-44B/A bomb racks incorporate four hooks in tandem providing 14 and 30 inch suspension capability. This configuration provides a total payload in excess of 20,000 lbs. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

264.73 35.83 32.14 2,160.00

Aircraft: B-2A Management/Engineering: 707th MSUS, Tinker AFB, OK (BRU-44B/A managed by 575th CBSS/GBLE, WR-ALC, Robins AFB, GA) Technical Order: 11N-L5006-2

9-80

FOUO

Nomenclature: SECBM

Name: MIL-STD-1760 Conventional Bomb Module

Description: The 10-Carry Enhanced Conventional Bomb Module (ECBM) was modified IAW TCTO 11B293-55-513 to the new 1760 Conventional Bomb Module (SECBM). This TCTO modified the existing ECBM hardware to the SECBM configuration and also installed 1760 LRU'S. The 10Carry SECBM consists of the shell structure with attached frames for mounting 10 each, 14Inch Bomb Ejector Racks. The 10 Carry SECBM is designed to carry and release 10 Cluster Bomb Units (CBU), either CBU-87, 89, 97, 103, 104 and 105. Also certified to carry and release the GBU-38 500 pound Joint Direct Attack Munitions (JDAM), with 6 in the FWD, 6 in the intermediate and 3 in the AFT bay. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

178.00 69.96 57.66 2,816.00 empty

Aircraft: B-1B Management/Engineering: 575 CBSS/GBLE, Robins AFB, GA Technical Order: 11B29-3-55-1

9-81

FOUO

Nomenclature: F-35 Pneumatic Power Source (PPS) Description: The F-35 Pneumatic Power Source (PPS) provides ejection energy in the form of compressed air to the BRU-67/A, BRU-68/A and LAU-147/A on the F-35A/B/C aircraft. The PPS is located in the right hand weapons bay and supplies air pressure to stations 4, 5, 7 and 8. Additionally, a PPS is located in the air-to-ground pylons providing air pressure to the BRU68/A in each pylon. The PPS consists of a compressor motor, filter manifold, PAO cooling plate and Electronic Control Unit (ECU) internally and a motor compressor; filter module and ECU in the pylons. The PPS is capable of supplying 5,000 PSI to the various racks/launchers on demand. Carriage Options: F-35A/B/C Management/Engineering: Lockheed Martin Aerospace, Fort Worth, Tx Technical Order: F-35 Automated Joint Technical Data (JTD) system

9-82

FOUO

Nomenclature: Stations 1 and 11

Name: A-10 Pylon

Description: The pylon assembly is a non-jettisonable pylon assembly that is carried on the outboard wing stations number 1 and 11. The pylon contains a MAU-50 bomb ejector rack, and a type B station control unit for the desired release of the munition that is carried. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

46.70 4.40 16.40 96.50

Aircraft: A-10 Management/Engineering: 416SCMS/GUMBA, HILL AFB, UT Technical Order: 16W6-28-2

9-83

FOUO

Nomenclature: Stations 2 and 10

Name: A-10 Pylon

Description: The pylon assembly is a non-jettisonable pylon assembly that is carried on the outboard wing stations number 2 and 10. The pylon contains a MAU-50 bomb ejector rack, and a type B station control unit for the desired release of the munition that is carried. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

69.50 4.50 11.50 96.90

Aircraft: A-10 Management/Engineering: 416SCMS/GUMBA, HILL AFB, UT Technical Order: 16W6-28-12

9-84

FOUO

Nomenclature: Stations 3 and 9

Name: A-10 Pylon

Description: The pylon assembly is a non-jettisonable pylon assembly that is carried on the wing stations number 3 and 9. The pylon contains a MAU-40 bomb ejector rack, and a type B station control unit for the desired release of the munition that is carried. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

73.70 4.50 12.00 129.20

Aircraft: A-10 Management/Engineering: 416SCMS/GUMBA, HILL AFB, UT Technical Order: 16W6-28-22

9-85

FOUO

Nomenclature: Stations 4 and 8

Name: A-10 Pylon

Description: The pylon assembly is a nonjettisonable pylon assembly that is carried at wing stations number 4 and 8. The pylon contains a MAU-40 bomb ejector rack, a type B station control unit, and fuel and air line. The pylon assembly is capable of carrying an external store or a fuel tank as directed by mission requirements. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

81.20 4.50 12.00 133.80

Aircraft: A-10 Management/Engineering: 416SCMS/GUMBA, HILL AFB, UT Technical Order: 16W6-28-32

9-86

FOUO

Nomenclature: Stations 5 and 7

Name: A-10 Pylon

Description: The pylon assembly is a non-jettisonable pylon assembly that is carried on the fuselage stations number 5 and 7. The pylon contains a MAU-40 bomb ejector rack, a type B station control unit. The pylon assembly is capable of carrying an external store as directed by mission requirements. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

90.20 4.50 10.00 131.40

Aircraft: A-10 Management/Engineering: 416SCMS/GUMBA, HILL AFB, UT Technical Order: 16W6-28-42

9-87

FOUO

Nomenclature: Station 6

Name: A-10 Pylon

Description: The pylon assembly is a non-jettisonable pylon assembly that is carried at fuselage center station number 6. The pylon contains a MAU-40 bomb ejector rack, a type B station control unit, and fuel and air line. The pylon assembly is capable of carrying an external store or a fuel tank as directed by mission requirements. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

90.20 4.50 7.80 136.10

Aircraft: A-10 Management/Engineering: 416SCMS/GUMBA, HILL AFB, UT Technical Order: 16W6-28-52

9-88

FOUO

Nomenclature: Pylon

Name: F-22A Pylon

Description: The F-22A pylon provides carriage, deployment, and jettison of external stores in ferry or combat configurations. External stores include a 600 gallon fuel tank and/or launchers carrying two AIM-120 or two AIM-9 missiles per wing station. Growth provisions exist for additional types of stores. A BRU-47 rack installed in the forward section provides the attachment for fuel tanks, missile adapters, and other external stores. An internal pyrotechnic device provides jettison capability for the pylon plus stores throughout the prescribed envelope. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

140.0 23.0 20.0 386

Aircraft: F-22A Management/Engineering: Lockheed Martin Corporation, Fort Worth, TX Technical Order: 16W6-56-2

9-89

FOUO

Nomenclature: Pylon

Name: Integrated Conventional Stores Management System (ICSMS) Pylon

Description: The Integrated Conventional Stores Management System (ICSMS) Pylon consists of the Stub Wing-Pylon with the Heavy Stores Adapter Beam (HSAB). These two halves are bolted together to form the ICSMS pylon. The ICSMS pylon can be installed under each wing of the B-52H and attaches in the same manner as the cruise missile pylons. Electrical cabling routed in the sub-pylon connects to receptacles in the wing-pylon adapter and HSAB. The term ICSMS stores refer to non-nuclear stores designed for MIL-STD-1760 which is a definition of the electrical interface between the aircraft and store. An optional method of weapons release uses a stepper switch for a non-1760 style weapons. This pylon is capable of carrying the full range of 1760 weapons along with a significant number of conventional munitions including general purpose bombs, cluster bomb units, aerial mines, and laser guided munitions. Dimensions: Length (in.) 286 Width (in.) 48 Height (in.) 60 Weight (lbs.) 2400 Operating Temperature Range - same as aircraft Power Requirements - ICSMS 28 (+3) VDC and 115 VAC, 400 Hz, three phase - Conventional 28 (+3) VDC Constructed from aluminum, fittings, fiberglass, and plastic Attached are nine MAU-12 Bomb Racks Internal to the Pylon - four LRUs control by the MIL-S-1553 data bus (before Technical Change to Technical Order (TCTO) 16W6-47-514) AFTER TCTO 16W6-47-514 one LRU (IWIU) by the MIL–S-1553 data bus Aircraft: B-52H Management/Engineering: 540 ACSS/GFLCB, Tinker AFB, OK Technical Order: 16W6-47-2

9-90

FOUO

9-91

FOUO

Nomenclature: ALE-25 PYLON

Name: B-52H Aircraft Pylon

Description: The ALE-25 pylon is utilized during carriage of the Air Combat Maneuvering Instrumentation (ACMI) pod. The pylon can be installed under each wing of the B-52H aircraft. Electrical cabling routed in the ALE-25 pylon connects to receptacles at the aircraft 559 station under each wing. Dimensions: Length (in.) 117 inches Width (in.) 9 inches Height (in.) Approximately 19 inches without adapter Weight (lbs.) 60 pounds (without bomb rack) Launcher fittings - 15 pounds ACMI POD 124 pounds Operating Temperature Range - same as aircraft Power Requirements 28 (+3) VDC and 115 VAC, 400 Hz, three phase Material Aluminum sheet and extrusion Construction - Semimonocoque box beam design having longitudinal stiffener angles plus stiffener angles around inner perimeter of box section at numerous stations.

ALE-25 Pylon

9-92

FOUO

Nomenclature: LASER POD (LITENING) PYLON

Name: B-52H Aircraft Pylon

Description: The Laser Pod pylon is utilized during carriage of the AN/AAQ-28 Airborne Targeting and Designator (LITENING) pod. The pod can be installed under the right wing of the B-52H aircraft. Electrical cabling routed inside this ALE-25 pylon connects to receptacles at the aircraft 559 station under the right wing designated for LITENING. Dimensions: Length (in.) 117 inches Width (in.) 9 inches Height (in.) Approximately 19 without adapter, 25 inches with adapter Weight (lbs.) 62 pounds without adapter Pod adapter fitting - 70 pounds Assembled pylon - 146 pounds Operating Temperature Range - same as aircraft Power Requirements 28 (+3) VDC and 115 VAC, 400 Hz, three phase Material Aluminum sheet and extrusion Construction: Semimonocoque box beam design having longitudinal stiffener angles plus stiffener angles around inner perimeter of box section at numerous stations.

Laser Pod Pylon

9-93

FOUO

Nomenclature: SUU-59B/A

Name: F-15 Inboard Aircraft Pylon

Description: The F-15 Inboard Aircraft Pylon provides the F-15A-D aircraft with carriage and jettison capabilities of external fuel tank and conventional air-to-air armament. The SUU-59B/A contains one MAU-12 bomb rack. The SUU-59B/A and MAU-12 combination provides electrical, mechanical and fuel delivery interface between the attached store/external fuel tank and various aircraft systems. This entire pylon can be jettisoned from the aircraft just as stores are jettisoned from the MAU-12. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

159.00 5.00 18.00 335.00

Aircraft: F-15A-D Management/Engineering: 568 ACSS/GFLC, Robins AFB, GA Technical Order: 16W6-25-12

9-94

FOUO

Nomenclature: SUU-59C/A

Name: F-15 Inboard Aircraft Pylon

Description: The F-15 Inboard Aircraft Pylon provides the F-15E aircraft with carriage and jettison capabilities of external fuel tank, conventional air-to-air missiles, and conventional/nuclear airto-ground armament. The SUU-59C/A contains one BRU-47/A bomb rack. The SUU-59C/A and BRU-47/A combination provides electrical, mechanical and fuel delivery interface between the attached store/external fuel tank and various aircraft systems. This entire pylon can be jettisoned from the aircraft just as stores are jettisoned from the BRU-47/A. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

159.00 5.00 18.00 371.00

Aircraft: F-15E Management/Engineering: 568 ACSS/GFLC, Robins AFB, GA Technical Order: 16W6-25-12

9-95

FOUO

Nomenclature: SUU-60B/A

Name: F-15 Centerline Aircraft Pylon

Description: The F-15 Centerline Aircraft Pylon provides the F-15A-D aircraft with carriage and jettison capabilities of external fuel tank and special equipment. The SUU-60B/A contains one MAU-12 bomb rack. The SUU-60B/A and MAU-12 combination provides electrical, mechanical and fuel delivery interface between the attached store/external fuel tank and various aircraft systems. This entire pylon can be jettisoned from the aircraft just as stores are jettisoned from the MAU-12. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

148.00 5.00 15.00 285.00

Aircraft: F-15A-D Management/Engineering: 568 ACSS/GFLC, Robins AFB, GA Technical Order: 16W6-25-2

9-96

FOUO

Nomenclature: SUU-62/A, B/A

Name: F/A-18 Centerline Aircraft Pylon

Description: The centerline SUU-62 pylon provides mechanical and electrical interface between the aircraft fuselage and the stores carried. The BRU-32 bomb rack is contained internally and provides pylon/weapon interface. Weight with the BRU-32 is 130 lb. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

90 7 8 130

Aircraft: F/A-18A-D Management/Engineering: 568 ACSS/GFLC, Robins AFB, GA Technical Order: 16W6-25-2

9-97

FOUO

Nomenclature: SUU-63

Name: F/A-18 Centerline Aircraft Pylon

Description: The SUU-63 pylon provides mechanical and electrical interface between the aircraft wing structure and the stores carried. t can be installed at any of the wing stations. The BRU-32 bomb rack is contained internally and provides the pylon/weapon interface. Weight with the BRU-32 is 273 lb. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

120 6 28 273 (with BRU-32)

Aircraft: F/A-18A-D Management/Engineering: 568 ACSS/GFLC, Robins AFB, GA Technical Order: 16W6-25-2

9-98

FOUO

Nomenclature: SUU-67/A

Name: Pylon

Description: The SUU-67/A aircraft pylon is an aerodynamic interface between the B-52H and the Air Launched Cruise Missiles (AGM-86B and AGM-86C). The pylon is interchangeable and can be attached under either wing of the B-52H, between the inboard engines and the fuselage. Dimensions: Length (in.) Height (in.) Width (in.) Weight (lbs.) -

492 60 26 4,446 without missiles

Aircraft: B-52H Contractor / Status / Improvements / Special Equipment: Contractor - Boeing Special Equipment - TOs: 35D5-3-8-31, 35M8-2-7-1, 35MA1-1-101 Management/Engineering: 707 MSUS, Tinker AFB, OK Technical Order: 16W6-33-1

9-99

FOUO

Nomenclature: SUU-72A

Name: Pylon

Description: The SUU-72/A aircraft pylon is an aerodynamic interface between the B-52H and the Air Launched Cruise Missile AGM-129. The pylon is interchangeable and can be attached under either wing of the B-52H, between the inboard engines and the fuselage. Dimensions: Length (in.) Height (in.) Width (in.) Weight (lbs.) -

492 60 26 4,446 without missiles

Aircraft: B-52H Contractor / Status / Improvements / Special Equipment: Contractor - Boeing Special Equipment - TOs: 35D5-3-8-31, 35M8-2-7-1, 35MA1-1-101 Management/Engineering: 707 MSUS, Tinker AFB, OK Technical Order: 16W6-33-1

9-100

FOUO

Nomenclature: SUU-73/A

Name: F-15 Centerline Aircraft Pylon

Description: The F-15 Centerline Aircraft Pylon provides the F-15E aircraft with carriage and jettison capabilities of external fuel tank, special equipment and conventional/nuclear air-to-ground armament. The SUU-73/A contains one BRU-47/A bomb rack. The SUU-73/A and BRU-47/A combination provides electrical, mechanical and fuel delivery interface between the attached store/external fuel tank and various aircraft systems. The SUU-73/A pylon has additional electrical interface provision for special weapon carriages. This entire pylon can be jettisoned from the aircraft just as stores are jettisoned from the BRU-47/A. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

148.00 5.00 15.00 316.00

Aircraft: F-15E Management/Engineering: 568 ACSS/GFLC, Robins AFB, GA Technical Order: 16W6-25-2

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Nomenclature: WWP

Name: Wing Weapons Pylon Assembly

Description: The wing weapon pylon assembly is hard-mounted to the F-16 aircraft. The pylon uses a MAU-12 bomb rack to carry conventional and nuclear stores. The pylon provides electrical and mechanical interface between the attached store and various aircraft systems. The exterior surface of the pylon is covered with spray-on radar absorbent material. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

80.00 20.00 17.00 220.00 to 322.00 (Depending on Configuration)

Aircraft: F-16 Management/Engineering: 518 CBSS/GBMAC, Hill AFB, UT Technical Order: 16W6-51-2

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Nomenclature: WWP (PIDS)

Name: Wing Weapons Pylon Integrated Dispenser System

Description: The pylon provides for carriage and release of external stores, other than fuel tanks, and capability for internal pylon integrated dispenser system (PIDS-3). PIDS-3 is a chaff dispenser system. The pylon trailing edge provides mounting for three ALE-40 magazines, matrix, sequencer switches, and an EMI-filter. Dimensions: Length (in.) Width (in.) Height (in.) Weight (lbs.) -

101.00 19.40 17.00 217 (approximately)

Aircraft: F-16A-B Management/Engineering: 518 CBSS/GBMAC, Hill AFB, UT Technical Order: 16W6-54-2

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INTENTIONALLY LEFT BLANK

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CHAPTER TEN 1 June 2009

COUNTERMEASURES

FOR OFFICIAL USE ONLY

INTENTIONALLY LEFT BLANK

Nomenclature: ADM-141A, B

Name: Tactical Air-Launched Decoy (TALD)

Capability: Low cost, Tactical Air-Launched unpowered glide decoy to confuse and saturate enemy air defenses. Description: The TALD is an expendable air launched, preprogrammed, unpowered, glide chaff, RF passive, or RF active vehicle used to deceive and saturate enemy integrated air defenses during strike aircraft operations. It has a square section fuselage, flip-out wings, and three tail surfaces. It has a digital flight control system which can be preprogrammed with various speed and maneuvering profiles. Launched from high-altitude (max. 12,200 m (40,000 ft)), the TALD has a glide range of up to 126 km (68 nm), while the range at lower altitudes of about 600 m (2,000 ft) is still around 26 km (14 nm). The basic TALD exists in several versions with different payloads. The A/B37U-1(V)1 is a chaff-dispensing vehicle carrying up to 36 kg (80 lb) of chaff, the A/B37U-1(V)2 is a passive radar decoy which uses a Luneberg lens the enhance its radar signature, and the ADM-141A uses both passive (Luneberg lens) and active (RF amplifier) radar enhancers. I don't know why the latter version was designated as a guided missile, when the two former ones were classed as aeronautical support equipment. The ADM-141B is also described as a chaff-dispensing TALD. Characteristics: Launch Interface - F/A-18 “Un-powered” Guidance Control Rear Mounted Actuator Control Fins and Variable Translation/Variable Sweep Wing Assembly, Programmable flight path via mission planning software Class Guided Missile, Air Launched Decoy Weight (lbs.) 400 Length (in.) 92 Wing Span (in.) 61 Width/Height (in.) - 10 Propulsion none Range (nm) 68 (126 km) Speed 250 knots (126 km/h) Carriage Options: Aircraft: F/A-18A-F P-3C

Launcher: 14 in lugs BRU-41/A BRU-42/A

Contractor / Status / Improvements / Special Equipment: Contractor - Brunswick Corporation Status Special Equipment Management/Engineer:

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Technical Order:

ADM-141A

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Nomenclature: ADM-141C

Name: Improved Tactical AirLaunched Decoy (ITALD)

Capability: Low Cost, Air-Launched Jet Powered Miniature Decoy - Stimulate, Deceive or Saturate Adversary Air Defenses. Description: The ITALD is an air launched, preprogrammed, powered RF active vehicle used to deceive and saturate enemy integrated air defenses during strike aircraft operations. It is a Preplanned Product Improvement towhead that adds turbojet propulsion and low-level navigation capability to the TALD. A computer within each vehicle is preprogrammed with flight profile data prior to loading. It provides flight management and controls of the vehicle through a series of planned maneuvers after launch. The ITALD has enhanced terrain tracking capability and an extended flight envelope for expanded missions. The Improved Tactical Air-Launch Decoy (ITALD) simulates a fighter/attack size aircraft better than current decoys. Characteristics: Launch Interface - F/A-18 “Powered” Guidance Control -

GPS aided/INS Avionics Suite, SAASM Compliant Rear Mounted Actuator Control Fins and Variable Translation/Variable Sweep Wing Assembly, Programmable flight path via mission planning software Class Guided Missile, Air Launched Decoy Weight (lbs.) 400 Length (in.) 92 Wing Span (in.) - 61 Width/Height (in.) - 10 Propulsion Teledyne CAE J700-CA-400 turbojet; 790 N (177 lb) Range (nm) 160 (300 km) Speed Mach 0.8 Carriage Options: Aircraft: F/A-18A-F P-3C

Launcher: 14 in lugs BRU-41/A BRU-42/A

Contractor / Status / Improvements / Special Equipment: Contractor - IMI Status Special Equipment Management/Engineer: Technical Order:

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ADM-141C

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Nomenclature: ADM-160B

Name: Miniature Air Launched Decoy (MALD)

Capability: Low Cost, Air-Launched Jet Powered Miniature Decoy - Stimulate, Deceive or Saturate Adversary Air Defenses. Description: The Miniature Air Launched Decoy (MALD) is an, air launched, expendable decoy that will provide the United States Air Force the capability to stimulate, deceive, decoy, and saturate enemy threat Integrated Air Defense System (IADS). Characteristics: Launch Interface - F-16 “Un-powered” B-52 MIL-STD-1760D Guidance GPS aided/INS Avionics Suite, SAASM Compliant Control Rear Mounted Actuator Control Fins and Variable Translation/Variable Sweep Wing Assembly, Programmable flight path via mission planning software Class Guided Missile, Air Launched Decoy Weight (lbs.) 282 Length (in.) 113 Wing Span (in.) 67 Diameter (in.) 11 Propulsion TJ-150 Engine Carriage Options: Aircraft: Threshold: F-16C/D B-52H Objective: F-15E B-1B A-10 F-22A F-35

Launcher: 14 in lugs MAU-12, TER-9 (2 per TER) HSAB (8 per HSAB)

Contractor / Status / Improvements / Special Equipment: Contractor - Raytheon Missile Systems Company, Tucson, AZ Status Initial Operational Test Schedule - LRIP decision FY08 – Fielding FY09 – FRP decision FY10 Special Equipment - No peculiar support equipment required. MALD is compatible with Common Munitions Bit Reprogramming Equipment (CMBRE) and CMBRE+ Management/Engineer: 692d Armament Systems Squadron (ARSS), Eglin AFB, FL Supporting ALC: 575 Combat Sustainment Squadron (CBSS), Robins AFB, GA

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Technical Order: 21-AD160B-2 (Preliminary Technical Order)

MALD External View

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Nomenclature: ADM-160C

Name: Miniature Air Launched Decoy-Jammer (MALD-J)

Capability: Low Cost, Air-Launched Jet powered Miniature Decoy/Jammer - Stimulate, Deceive, Saturate, Jam Adversary Air Defenses. Description: The MALD-J is an, air launched, expendable decoy/jammer that will provide the United States Air Force the capability to stimulate, deceive, decoy, saturate, and jam enemy threat Integrated Air Defense System (IADS). Characteristics: Launch Interface - F-16 “Un-powered” B-52 MIL-STD-1760D Guidance GPS aided/INS Avionics Suite, SAASM Compliant Control Rear Mounted Actuator Control Fins and Variable Translation/Variable Sweep Wing Assembly, programmable flight path via mission planning software Class Guided Missile, Air Launched Decoy Weight (lbs.) 282 Length (in.) 113 Wing Span (in.) - 67 Diameter (in.) 11 Propulsion TJ-150 Engine Carriage Options: Aircraft: Threshold: F-16C/D B-52H Objective: F-15E B-1B A-10 F-22A F-35

Launcher: 14 in lugs MAU-12, TER-9 (2 per TER) HSAB (8 per HSAB)

Contractor / Status / Improvements / Special Equipment: Contractor - Raytheon Missile Systems Company, Tucson, AZ Status Risk reduction Phase II Schedule - Engineering Manufacturing Development Phase - FY10 Special Equipment - No peculiar support equipment required. MALD-J is compatible with Common Munitions BIT Reprogramming Equipment (CMBRE) and CMBRE + Management/Engineer: 692d Armament Systems Squadron (ARSS), Eglin AFB, FL Supporting ALC: 575 Combat Sustainment squadron (CBSS), Robins AFB, GA

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Technical Order: 21-AD160B-2 (in development)

Note: MALD-J has identical external view as MALD.

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Nomenclature: ALA-17

Name: Flare Rack

Description: The ALA-17 Flare Rack is a metal rectangular box which is designed to hold eight ALA-17 flare cartridges. The rack contains the electrical circuitry and connectors necessary to fire the flares selectively. The top of the rack is equipped with an electrical connector assembly and a shorting ring. The rack is installed into the ALE-20 Dispenser. Characteristics: Weight (lbs.) Length (in.) Width (in.) Height (in.) -

9.0 (empty) 43.0 (loaded) 12.25 5.75 13.5

Carriage Options: B-52H Dispenser: ALE-20 Impulse Cartridge: N/A Contractor / Status / Improvements / Special Equipment: Contractor - Unknown Status Inventory Improvements - N/A Special Equipment - N/A Management/Engineering: 506 CBSS/GBLA, Hill AFB, UT Technical Order: 11A16-7-23 & 11A16-7-7

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Nomenclature: ALA-17B

Name: IR Flare Cartridge

Description: The ALA-17B flare cartridge is a magnesium based dual stacked IR counter- measure. It consists of two aluminum case assemblies roll crimped in the center, crimped on aluminum bottom cap, upper and lower illuminant assemblies, upper and lower ignition assemblies, and an upper electrical contact assembly. A polyethylene sleeve covers the outside of the flare. The lower pellet is dispensed by means of an internal squib from the first fire command. Next fire command dispenses the upper pellet in a similar manner. Characteristics: Weight (lbs.) 4.25 Length (in.) 12.5 Diameter (in.) 2.75 Carriage Options: B-52H Dispenser: ALE-20 & ALA-17 Flare Rack Impulse Cartridge: Electric squibs built in, All-Up-Round Contractor / Status / Improvements / Special Equipment: Contractor Longhorn Army Ammunition Plant Status Inventory Improvements - ALA-17C in development, est. 2007 for fielding Special Equipment - N/A Management/Engineering: 506 CBSS/GBLA, Hill AFB, UT Technical Order: 11A16-7-7

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Nomenclature: AN/ALE-20

Name: Flare Ejector Set

Description: The AN/ALE-20 flare ejector system provides a means of selecting the number of flares to be fired, timing the interval between bursts, and igniting and firing the flares from the aircraft. The flare ejector system utilizes 12, AN/ALA-17, with ALA-17A flare sets, with 16 flare bursts per set, and a maximum of 192 single flare bursts per aircraft. The flares may be programmed to fire in bursts of one, two, or three flares at intervals of 2 to 20 seconds, between bursts. The flares may also be salvoed at a rate of one flare every 65 milliseconds by pressing the fast train switch. All flares may be ejected from the aircraft in less than 40 seconds. Characteristics: Weight (lbs.) Length (in.) Width (in.) Diameter (in.) Carriage Options: B-52H Capacity: This Dispenser system utilizes 12 AN/ALA-17, 17A flare sets, with 16 flare bursts per set. The system carries a maximum of 192 flares Contractor / Status / Improvements / Special Equipment:

Management/Engineering: 561 CBSS/GBLB - 542 CBSG/GBEBA, Robins AFB, GA Technical Order:

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Nomenclature: AN/ALE-48

Name: Chaff Dispenser

Description: Characteristics: Weight (lbs.) - 45 Length (in.) - 20.0 Width (in.) 13.2 Diameter (in.) - 13.6 Carriage Options: B-1B Capacity: 120ea RR-170 / 188 Chaff Cartridges Contractor / Status / Improvements / Special Equipment: Procurement of additional assets from Naval Sea Systems Command, Crane, IN, includes improved handle design and single-piece housing using modern CNC machining. Management/Engineering: 561 CBSS/GBLB - 542 CBSG/GBEBA, Robins AFB, GA Technical Order: 12P3-4-88-2

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Nomenclature: AN/ALE-49

Name: Flare Dispenser

Description: Characteristics: Weight (lbs.) Length (in.) Width (in.) Diameter (in.) -

65.2 20.0 13.2 13.6

Carriage Options: B-1B Capacity: 12 ea MJU-23A/B Flare Cartridges Contractor / Status / Improvements / Special Equipment: Improved handle design being considered as part of ALE-48 procurement. Management/Engineering: 561 CBSS/GBLB - 542 CBSG/GBEBA, Robins AFB, GA Technical Order: 12P3-4-89-2

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Nomenclature: AN/ALE-50A(V)1

Name: Countermeasures Decoy Dispensing Set (CMDDS)

Description: The AN/ALE-50 Countermeasures Decoy Dispensing Set (CMDDS) consists of an Advanced Airborne Expendable Decoy (AAED) round, a launcher which holds the decoy round and launches it upon command, and a controller which contains the electronic circuitry that interfaces with each host platform. The decoy is a self-contained repeater that presents a more attractive target to an incoming missile and lures it away from the carrier aircraft. The complete decoy round consists of a canister, reel assembly, towline, and the expendable decoy, which is common to all platforms. The AN/ALE-50A(V)1 is designed for the B-1B and is comprised of the Integrated Multi-Platform Launch Controller (IMPLC) and 1x4 Dual Compatible Launcher (DCL) and can deploy both the AAED and a Fiber Optic towed Decoy (FOTD). This version can carry four decoys and two systems are mounted on the B-1B for a total of up to eight available decoys per aircraft. Characteristics: Weight (lbs.) Length (in.) Width (in.) Height (in.) -

IMPLC 33 14 5.7 7.5

Characteristics: Weight (lbs.) Length (in.) Width (in.) Height (in.) -

Dispenser (1X4 Dual Compatible Launcher) 45 27 16 4

Carriage Options: B-1B Capacity: Four ea Decoys Squib/Cart: CCU-41/B Impulse Carts Contractor / Status / Improvements / Special Equipment: Contractor Raytheon Electronic Warfare Systems, Goleta, CA Status Sustainment. Improvements None. Special Equipment - Fault Isolation System Tester (FIST) allows the field to test the system without using “live” decoys, and tests three modes: Stray Voltage, Standard, and Operational. A production decision for this Support Equipment is anticipated in FY06-4.

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Management/Engineering: 561 CBSS/GBLA, Robins AFB, GA Technical Order: 12P3-2ALE50-2

AN/ALE-50A(V)1

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Nomenclature: AN/ALE-50(V)2

Name: Countermeasures Decoy Dispensing Set (CMDDS)

Description: The AN/ALE-50(V)2 consists of an Advanced Airborne Expendable Decoy (AAED) round, a launcher which holds the decoy round and launches it upon command, and a controller which contains the electronic circuitry that interfaces with each host platform. The decoy is a selfcontained repeater that presents a more attractive target to an incoming missile and lures it away from the carrier aircraft. The complete decoy round consists of a canister, reel assembly, towline, and the expendable decoy, which is common to all platforms. It is designed for the Block 25/30 F-16s and Block 40/50 F-16C/D and is comprised of the 1x2 Launcher/Controller that is installed into the 16S351-805 pylon and can only deploy the AAED. This version can carry two decoys and two systems can be mounted on the F-16 for a total of up to four decoys per aircraft. Characteristics: 1X2 Launcher/Controller Weight (lbs.) 35 Length (in.) 23 Width (in.) 9 Height (in.) 6 Carriage Options: F-16 Capacity: Two ea Decoys Squib/Cart: CCU-41/B Impulse Cartridges Contractor / Status / Improvements / Special Equipment: Contractor - Raytheon Electronic Warfare Systems, Goleta, CA Status Sustainment Improvements - On-going modification to retrofit 650 of the Launcher/Controllers with the Transient Suppression Assembly, to protect against lightning. Once this mod is completed, the entire inventory of Launcher Controllers will be the same configuration. Special Equipment - Fault Isolation System Tester (FIST) allows the field to test the system without using “live” decoys. FIST for F-16 is fielded and stable. Management/Engineering: 561 CBSS/GBLA, Robins AFB, GA Technical Order: 12P3-2ALE50-2

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AN/ALE-50(V)2

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Nomenclature: LAU-74

Name: Flare Launcher System

Description: Characteristics: Weight (lbs.) Length (in.) Width (in.) Diameter (in.) -

395 57.0 31.0 43.0

Carriage Options: C-130 Capacity: 24 ea MK 24 Mod 4 Flares or 24 ea LUU-2/B Flares or 24 ea LUU-1/B Target Markers or 24 ea LUU-5/B Target Markers or 24 ea MJU-6/B Chaff Cartridges Contractor / Status / Improvements / Special Equipment: Management/Engineering: WR-ALC/LNXB Technical Order: 11L1-5-4-2

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Nomenclature: LUU-1, -5

Name: Target Marker

Description: Air-deployed LUU-1 and LUU-5 flares are used to illuminate targets, providing a target area ground reference. The flares ignite in the air at a distance set on an ignition timer, then burn on the ground, providing a colored flame that is visible from the air. Characteristics: Weight (lbs.) Length (in.) Diameter (in.) -

26 36.0 5.0

Carriage Options: A-10 C-17 C-130 C-141 F-15 F-16 Dispenser: SUU-25 Dispenser or LAU-74 Launcher or Hand Dispensed or Single Carriage Bomb Rack Contractor / Status / Improvements / Special Equipment: Management / Engineering: 506 CBSS/GBLA, Hill AFB, UT Technical Order: 11A10-33-7

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Nomenclature: LUU-2, -19

Name: Illuminating Flare

Description: The LUU-2 and LUU-19 illumination flares have timers that are set to ignite the flare after a predetermined drop distance. The timer deploys a parachute which activates the igniter. The flare burns for a set amount of time, illuminating an area, then the parachute is collapsed by means of an explosive bolt in order to clear the air space. The LUU-19 emits light in the NIR region for use with night vision goggle, while the LUU-2 emits visible light. Characteristics: Weight (lbs.) Length (in.) Diameter (in.) -

29 (LUU-2), 36 (LUU-19) 36.0 5.0

Carriage Options: A-10 C-17 C-130 C-141 F-15 F-16 AV-8B F/A-18A-F Dispenser: SUU-25 Dispenser or LAU-74 Launcher or Hand Dispensed or Single Carriage Bomb Rack Contractor / Status / Improvements / Special Equipment: Management / Engineering: 506 CBSS/GBLA, Hill AFB, UT Technical Order: 11A10-24-7

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Nomenclature: M206

Name: IR Flare

Description: The M206 Decoy Flare is the current in-service inventory production decoy flare primarily used by Army and Air Force platforms, and Marine Corps KC-130J. The M206 flare is a magnesium based IR countermeasure. The M206 Decoy Flare consists of a square aluminum case approximately 8.1 inches in length and 1 inch square with an unsealed plastic end cap. Internally, it consists of a pressed pyrotechnic flare grain and a piston. The pyrotechnic flare grain consists of a chemical mixture of Magnesium, Teflon , and Viton (MTV). The flare grain is directly initiated through a central hole in the piston by the impulse cartridge. It is dispensed and ignited in flight by a BBU-35/B or M796 impulse cartridge. When functioned, the M206 has an intensity, rise time, and burn time designed and optimized for use from lower signature assault support (rotary wing) and transport aircraft. This decoy flare was procured initially to support KC-130J testing, but is being replaced for future use by the Navy MJU-61/B. This decoy flare may be used in test, operations and training by all KC-130J aircraft Characteristics: Weight (lbs.) Length (in.) Width (in.) Height (in.) -

0.43 8.1 1.0 1.0

Carriage Options: A-10 MC-130 F-16 KC-130 J/T UC-35D Dispenser: ALE-40/47, M130, D-61(V)/ALQ-212(V) Impulse Cartridge: BBU-35/B, M796, CCU-145/A Contractor / Status / Improvements / Special Equipment: Contractor - Kilgore Flares, Esterline Armtec Status Inventory and in production Improvements - N/A Special Equipment - N/A Management/Engineering: 506 CBSS/GBLA, Hill AFB, UT US Army RDECOM ARDEC, RDAR-MEE-T, Bldg. 472, Picatinny, NJ 07806-5000 Navy, PMA-272, Jacksonville, Fl

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Technical Order: 11A16-41-7 (Air Force) NAVAIR 11-140-7 (Navy)

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Nomenclature: M206 (T-2)/B

Name: Flare Simulator

Description: The M206 (T-2)/B flare simulator is a smoke generating countermeasure simulator. It consists of a plastic case, plastic end cap, and fiberboard encased smoke pellets. It is dispensed and ignited in flight by a BBU-35/B or M796 impulse cartridge. A yellowish smoke is generated to simulate a flare for training purposes. Characteristics: Weight (lbs.) Length (in.) Width (in.) Height (in.) -

0.30 8.1 1.0 1.0

Carriage Options: A-10 MC-130 F-16 Others Dispenser: ALE-40/47 Impulse Cartridge: BBU-35/B, M796 Contractor / Status / Improvements / Special Equipment:

Contractor - Universal Propulsion Company (UPCO) Status Inventory Improvements - N/A Special Equipment - N/A Management/Engineering: 506 CBSS/GBLA, Hill AFB, UT Technical Order: 11A16-41-7

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Nomenclature: M211

Name: Decoy

Description: The M211 infrared countermeasure decoy consists of an aluminum cartridge case purged with nitrogen and containing a payload of stacked special material elements which react with air. Each aluminum cartridge case contains a sealed receptacle cup with an O-ring for an impulse cartridge, a plastic/nylon piston, crimped and then sealed, and a metal end plate. When the impulse cartridge is initiated by the firing pulse, the impulse cartridge receptacle cup frangible membrane ruptures. Pressure inside the canister increases pushing on the piston and breaking the end cap seal deploying the special material payload in the air stream. The special material payload reacts with air in generating infrared energy to decoy surface-to-air and air-to-air missiles. Characteristics: Weight (lbs.) Length (in.) Width (in.) Height (in.) -

0.66 8.00 1.00 1.00

Carriage Options: A-10 F-16 MC-130 Helicopters Dispenser: ALE-40, ALE-45 and ALE-47 Squib/Cart: BBU-35/B Contractor / Status / Improvements / Special Equipment: Contractor - Alloy Surfaces Inc Status Inventory and in production Management/Engineering: 506 CBSS/GBLA, Hill AFB, UT US Army RDECOM ARDEC, RDAR-MEE-T, Bldg. 472, Picatinny, NJ 07806-5000 Technical Order: 11A16-47-7

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Nomenclature: M212

Name: IR Flare

Description: The M212 flare is a boron based IR countermeasure. It consists of an aluminum case, brass end cap, safe and initiation device, plastic piston, and the flare pellet. It is dispensed and ignited in flight by a BBU-35/B or M796 impulse cartridge. Characteristics: Weight (lbs.) Length (in.) Width (in.) Height (in.) -

0.50 8.1 1.0 1.0

Carriage Options: MC-130 Helicopters Others Dispenser: ALE-40/47, D-61(V)/ALQ-212(V) Impulse Cartridge: BBU-35/B, M796 Contractor / Status / Improvements / Special Equipment:

Contractor - ATK Thiokol Status Inventory and in production Improvements N/A Special Equipment - N/A Management/Engineering: 506 CBSS/GBLA, Hill AFB, UT US Army RDECOM ARDEC, RDAR-MEE-T, Bldg. 472, Picatinny, NJ 07806-5000 Technical Order: 11A16-41-7

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Nomenclature: MJU-7A/B

Name: IR Flare

Description: The MJU-7A/B flare is a magnesium based IR countermeasure. It consists of an aluminum case, plastic end cap, felt spacer, plastic piston, safe & initiation device, and the flare pellet. It is dispensed and ignited in flight by a BBU-36/B impulse cartridge. Characteristics: Weight (lbs.) Length (in.) Width (in.) Height (in.) -

0.82 8.0 2.0 1.0

Carriage Options: A-10, F-15, F-16, F-22A, MC-130, Others Dispenser: ALE-40/45/47/52 Impulse Cartridge: BBU-36/B Contractor / Status / Improvements / Special Equipment: Contractor - Kilgore Flares, Esterline Armtec Status Inventory and in production Improvements - N/A Special Equipment - N/A Management/Engineering: 506 CBSS/GBLA, Hill AFB, UT Technical Order: 11A16-40-7

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Nomenclature: MJU-7(T-2)/B

Name: Flare Simulator

Description: The MJU-7(T-2)/B flare simulator is a smoke generating countermeasure simulator. It consists of a plastic case, plastic end cap, and fiberboard encased smoke pellets. It is dispensed and ignited in flight by a BBU-35/B or M796 impulse cartridge. A yellowish smoke is generated to simulate a flare for training purposes. Characteristics: Weight (lbs.) Length (in.) Width (in.) Height (in.) -

0.30 8.0 2.0 1.0

Carriage Options: A-10 F-15 F-16 MC-130 Others Dispenser: ALE-40/45/47 Impulse Cartridge: BBU-35/B, M796 Contractor / Status / Improvements / Special Equipment: Contractor - Universal Propulsion Company (UPCO) Status Inventory Improvements - N/A Special Equipment - N/A Management/Engineering: 506 CBSS/GBLA, Hill AFB, UT Technical Order: 11A16-40-7

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Nomenclature: MJU-10/B

Name: IR Flare

Description: The MJU-10/B flare is a magnesium based IR countermeasure. It consists of an aluminum case, crimped on aluminum end cap, felt spacer, plastic and silicone piston, safe and initiation device, and the flare pellet. It is dispensed and ignited in flight by a BBU-36/B impulse cartridge. Characteristics: Weight (lbs.) Length (in.) Width (in.) Height (in.) -

2.50 8.1 2.7 2.0

Carriage Options: C-17, F-15, F-22A Dispenser: ALE-45/47/52 Impulse Cartridge: BBU-36/B Contractor / Status / Improvements / Special Equipment: Contractor - Kilgore Flares, Esterline Armtec Status Inventory and in production Improvements - N/A Special Equipment - N/A Management/Engineering: 506 CBSS/GBLA, Hill AFB, UT Technical Order: 11A16-43-7

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Nomenclature: MJU-11

Name: Chaff/Flare Magazine

Description: (1X1) magazine Characteristics: Weight (lbs.) Length (in.) Width (in.) Height (in.) -

6.6 7.5 5.7 8.1

Carriage Options: A-10, C-17, C-130, C-141, F-15, F-16, MH-53J Capacity: 30 ea RR-170 or RR-188 Chaff Cartridges or 30 ea M206 Flares or 30 ea M206 (T-2) Flare Simulators Contractor / Status / Improvements / Special Equipment: Management/Engineering: 542 CBSSS/GBEAB, Robins AFB, GA Technical Order: 12P3-ALE40-3

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Nomenclature: MJU-12

Name: Flare Magazine

Description: (1X2) magazine Characteristics: Weight (lbs.) Length (in.) Width (in.) Height (in.) -

7.5 7.5 5.7 8.1

Carriage Options: A-10, C-17, C-130, C-141, F-15, F-16, MH-53J Capacity: 15 ea MJU-7/B Flares or 15 ea MJU-7A/B Flares or 15 ea MJU-7(T-2)B Flare Simulators Contractor / Status / Improvements / Special Equipment: Management/Engineering: 542 CBSSS/GBEAB, Robins AFB, GA Technical Order: 12P3-2ALE40-3

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Nomenclature: MJU-17

Name: Flare Magazine

Description: (2X2.5) magazine Characteristics: Weight (lbs.) Length (in.) Width (in.) Height (in.) -

7.5 7.5 7.5 8.11

Carriage Options: F-15E Capacity: Six ea MJU-10 Flare Cartridges Contractor / Status / Improvements / Special Equipment: Management/Engineering: 542 CBSSS/GBEAB, Robins AFB, GA Technical Order: 12P3-2ALE45-2

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Nomenclature: MJU-23A/B

Name: IR Countermeasure Flare

Description: The MJU-23A/B flare is a magnesium based IR countermeasure. It consists of an aluminum case, crimped on plastic end cap, red closure cap, plastic piston with o-ring, safe and initiation device, and the flare pellet. It is dispensed and ignited in flight by a BBU-46A/B impulse cartridge. Characteristics: Weight (lbs.) 4.10 Length (in.) 10.6 Diameter (in.) 2.85 Carriage Options: B-1B Dispenser: ALE-49 Impulse Cartridge: BBU-46A/B Contractor / Status / Improvements / Special Equipment: Contractor - Esterline Armtec Status Inventory Improvements - N/A Special Equipment - N/A Management/Engineering: 506 CBSS/GBLA, Hill AFB, UT Technical Order: 11A16-46-7

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Nomenclature: MJU-27A/B

Name: IR Decoy Device

Description: The MJU-27A/B Decoy Device is no longer in production, but is being replaced by the MJU49/B Decoy Device. The MJU-27A/B Decoy Device consists of a cylindrical aluminum case approximately 5.8 inches in length and 1.42 inches in diameter with an o-ring sealed aluminum end cap. The case and end cap closure design is identical to the MJU-49/B Decoy Device. Internally, it consists of a plastic piston and a pyrophoric metal air reactive payload. The pyrophoric metal payload consists of hundreds of very thin metal foils stacked on top of each other, which have been chemically treated to be air reactive and produce IR energy. This device is visually covert in daylight and is slightly visible at night. When functioned, the MJU27A/B pyrophoric metal payload is designed to disperse in the airstream producing an area source of IR energy. The MJU-27A/B has an intensity, rise time, reaction temperature, and reaction time designed and optimized for use on all military aircraft. This decoy device may be used in training by all Naval aircraft. Characteristics: Weight (lbs.) Length (in.) Width (in.) Height (in.) -

0.833 5.80 1.4 1.4

Carriage Options: F/A-18 A/B/C/D/E/F, AV-8B, EA-6B, E/A-18G, KC-130 F/R, AH-1W, AH-1Y/Z, UH-1N, CH-46, CH-53 D/E, MV-22, C-130 F/R, P-3C (AIP), P-3C, P-8, MH-60 R/S, SH-60B, HH-60H, MH-53E Dispenser: ALE-39/47 Impulse Cartridge: CCU-136A/A Management/Engineering: PMA-272, Jacksonville, Fl Technical Order: NAVAIR 11-140-7

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Nomenclature: MJU-32/B

Name: IR Decoy Flare

Description: The MJU-32/B Decoy Flare is the improved current in-service inventory production decoy flare (third generation) replacement for the Mk 46 Mod 1C Decoy Flares. The MJU-32/B Decoy Flare consists of a cylindrical aluminum case approximately 5.8 inches in length and 1.42 inches in diameter with a plastic end cap. Internally, it consists of an extruded pyrotechnic flare grain and a bore sensing out-of-line igniter ignition system. This improved sympathetic ignition system is safer than the old pull-wire ignition system in the Mk 46 Mod 1C. The pyrotechnic flare grain consists of a chemical mixture of Magnesium, Teflon , and Viton (MTV) and is wrapped in an adhesive backed aluminum foil tape. When functioned, the MJU-32/B has an intensity, rise time, and burn time designed and optimized for use from lower signature assault support (rotary wing) and transport aircraft. This decoy flare is not designed for use operationally from tactical strike (jet) or high signature fixed wing aircraft. This decoy flare may be used in training by all Naval aircraft. Characteristics: Weight (lbs.) Length (in.) Width (in.) Height (in.) -

0.563 5.8 1.4 1.4

Carriage Options: KC-130 F/R, AH-1W, AH-1Z, UH-1N, UH-1Y, CH-46, CH-53 D/E, MV-22, C-130 F/R, P-3 (AIP), P-3, P-8, MH-60 R/S, HH-60H, SH-60B, MH-53E Dispenser: ALE-39/47 Impulse Cartridge: CCU-136A/A Management/Engineering: PMA-272, Jacksonville, Fl Technical Order: NAVAIR 11-140-7

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Nomenclature: MJU-38/B

Name: IR Decoy Flare

Description: The MJU-38/B Decoy Flare is the improved current in-service inventory production decoy flare (third generation) replacement for the MJU-8/B and MJU-8A/B Decoy Flares. The MJU-38/B Decoy Flare consists of a cylindrical aluminum case approximately 5.8 inches in length and 1.42 inches in diameter with a plastic end cap. Internally, it consists of an extruded pyrotechnic flare grain and a bore sensing out-of-line igniter ignition system. This improved sympathetic ignition system is safer than the old pull-wire ignition system in the MJU-8/B and MJU-8A/B. The pyrotechnic flare grain consists of a chemical mixture of Magnesium, Teflon , and Viton (MTV) and is wrapped in an adhesive backed aluminum foil tape. When functioned, the MJU-38/B has an intensity, rise time, and burn time designed and optimized for use from higher signature tactical jet aircraft. This decoy flare is not designed for use operationally from helos and lower signature fixed wing aircraft. This decoy flare may be used in training by all Naval aircraft. Characteristics: Weight (lbs.) Length (in.) Width (in.) Height (in.) -

0.500 5.4 1.4 1.4

Carriage Options: F/A-18 A/B/C/D/E/F, AV-8B, EA-6B, E/A-18G Dispenser: ALE-39/47 Impulse Cartridge: CCU-136A/A Management/Engineering: PMA-272, Jacksonville, Fl Technical Order: NAVAIR 11-140-7

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Nomenclature: MJU-32 A/B & MJU-38 A/B

Name: IR Decoy Flare

Description: The MJU-32A/B and MJU-38A/B are product improvements to, and replacements for the original MJU-32/B and MJU-38/B respectively. The improvements incorporated into both these decoy flares are, (1) a bored out decoy case to reduce setback forces, (2) a plastic squib cup to reduce reactive loads to the dispenser magazine bolts, (3) a new igniter derived from the MJU-57/B. The MJU-32A/B and MJU-38A/B are completely interchangeable with, and will be similarly applied to applicable T/M/S aircraft the same as the basic MJU-32/B and MJU-38/B. Characteristics: Weight (lbs.) Length (in.) Width (in.) Height (in.) -

0.500 5.8 1.4 1.4

Carriage Options: MJU-32 A/B = KC-130 F/R, AH-1W, AH-1Z, UH-1N, UH-1Y, CH-46, CH-53 D/E, MV-22, C-130 F/R, P-3C (AIP), P-3C, P-8, MH-60 R/S, HH-60H, SH-60B, MH-53E MJU-38 A/B = F/A-18 A/B/C/D/E/F, AV-8B, EA-6B, E/A-18G Dispenser: ALE-39/47 Impulse Cartridge: CCU-136A/A Management/Engineering: PMA-272, Jacksonville, Fl Technical Order: NAVAIR 11-140-7

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Nomenclature: MJU-39/B

Name: IR Flare

Description: The MJU-39/B flare is a magnesium based kinematic IR counter-measure. It consists of an aluminum case, crimped on aluminum end cap, plastic piston, sequencer device, flare body with nozzle and shroud. It is dispensed and ignited in flight by a BBU-59/B impulse cartridge. Characteristics: Weight (lbs.) Length (in.) Width (in.) Height (in.) -

3.07 10.5 2.6 2.0

Carriage Options: F-22A Dispenser: ALE-52 Impulse Cartridge: BBU-59/B Contractor / Status / Improvements / Special Equipment: Contractor - Kilgore Flares Status Inventory and in production Improvements - N/A Special Equipment - N/A Management/Engineering: 506 CBSS/GBLA, Hill AFB, UT Technical Order: 11A16-43-7

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Nomenclature: MJU-40/B

Name: IR Flare

Description: The MJU-40/B flare is a magnesium based kinematic IR countermeasure. It consists of an aluminum case, crimped on aluminum end cap, plastic piston, sequencer device, flare body with nozzle and shroud. It is dispensed and ignited in flight by a BBU-36/B impulse cartridge. Characteristics: Weight (lbs.) Length (in.) Width (in.) Height (in.) -

3.04 10.5 2.6 2.0

Carriage Options: F-22A Dispenser: ALE-52 Impulse Cartridge: BBU-36/B Contractor / Status / Improvements / Special Equipment: Contractor - Kilgore Flares Status Inventory and in production Improvements - N/A Special Equipment - N/A Management/Engineering: 506 CBSS/GBLA, Hill AFB, UT Technical Order: 11A16-43-7

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Nomenclature: MJU-46/B

Name: IR Flare

Description: The MJU-46/B infrared countermeasure decoy consists of an aluminum cartridge case purged with nitrogen and containing a payload of stacked special material elements which react with air. Each aluminum cartridge case contains a sealed receptacle cup with O-ring for an impulse cartridge, a plastic/nylon piston, crimped and then sealed, metal end plate. When the impulse cartridge is initiated by the firing pulse, the impulse cartridge receptacle cup frangible membrane ruptures. Pressure inside the canister increases pushing on the piston and breaking the end cap seal deploying the special material payload in the air stream. The special material payload reacts with air in generating infrared energy to decoy surface-to-air and air-to-air missiles. Characteristics: Weight (lbs.) Length (in.) Width (in.) Height (in.) -

0.81 8.00 1.00 1.00

Carriage Options: A-10 C-130 F-16 Dispenser: ALE-40, ALE-45 and ALE-47 Squib/Cart: BBU-35/B Contractor / Status / Improvements / Special Equipment: Contractor - Alloy Surfaces Inc Status Inventory Management/Engineering: 506 CBSS/GBLA, Hill AFB, UT Technical Order: 11A16-47-7

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Nomenclature: MJU-47/B

Name: IR Flare

Description: The MJU-47/B flare is a magnesium based kinematic IR countermeasure. It consists of an aluminum case, crimped on aluminum end cap, plastic piston, sequencer device, and flare body with nozzle. It is dispensed and ignited in flight by a BBU-36/B impulse cartridge. Characteristics: Weight (lbs.) Length (in.) Width (in.) Height (in.) -

2.90 8.1 2.7 2.0

Carriage Options: F-15 F-16 Dispenser: ALE-45/47 Impulse Cartridge: BBU-36/B Contractor / Status / Improvements / Special Equipment: Contractor - Esterline Armtec Status Inventory and in production Improvements - N/A Special Equipment - N/A Management/Engineering: 506 CBSS/GBLA, Hill AFB, UT Technical Order: 11A16-43-7

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Nomenclature: MJU-48/B

Name: IR Flare

Description: The MJU-48/B flare is combination magnesium based IR flare and special material decoy countermeasure. It consists of an aluminum case, crimped and sealed aluminum end cap, felt spacer, special material payload, mid-spacer, flare pellet, safe and initiation device, plastic piston and a sealed cartridge cup. It is dispensed and ignited in flight by a BBU-35/B impulse cartridge. Characteristics: Weight (lbs.) Length (in.) Width (in.) Height (in.) -

1.30 8.0 2.0 1.0

Carriage Options: F-15 F-16 Dispenser: ALE-45/47 Impulse Cartridge: BBU-35/B Contractor / Status / Improvements / Special Equipment: Contractor - Esterline Armtec Status Inventory and in production Improvements - N/A Special Equipment - N/A Management/Engineering: 506 CBSS/GBLA, Hill AFB, UT Technical Order: 11A16-40-7

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Nomenclature: MJU-49/B

Name: IR Decoy Device

Description: The MJU-49/B Decoy Device is a current in-service inventory production decoy. The MJU-49/B Decoy Device consists of a cylindrical aluminum case approximately 5.8 inches in length and 1.42 inches in diameter with an aluminum end cap. The case and end cap closure are solid aluminum hermetically sealed with an o-ring. Internally, it consists of a plastic piston and a pyrophoric metal air reactive payload. The pyrophoric metal payload consists of hundreds of very thin metal foils stacked on top of each other, which have been chemically treated to be air reactive and produce IR energy. This device is visually covert in daytime and slightly visible at night. When functioned, the MJU-49/B pyrophoric metal payload is designed to disperse in the airstream producing an area source of IR energy. The MJU-49/B has an intensity, rise time, reaction temperature, and reaction time designed and optimized for use on all military aircraft. This decoy device may be used in training by all Naval aircraft. Characteristics: Weight (lbs.) Length (in.) Width (in.) Height (in.) -

0.860 5.8 1.4 1.4

Carriage Options: F/A-18 A/B/C/D/E/F, AV-8B, EA-6B, E/A-18G, KC-130 F/R, AH-1W, AH-1Z, UH-1N/Y, CH-46, CH-53 D/E, MV-22, C-130 F/R, P-3C (AIP), P-3C, P-8, MH-60 R/S, HH-60H, SH-60B, MH-53E Dispenser: ALE-39/47 Impulse Cartridge: CCU-136A/A Management/Engineering: PMA-272, Jacksonville, Fl Technical Order: NAVAIR 11-140-7

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Nomenclature: MJU-50

Name: IR Decoy Flare

Description: The MJU-50/B is an Air Force decoy device, developed under the Advanced Strategic & Tactical Expendable (ASTE) countermeasure program, adapted by the Air Force for use on their F-16, A-10 and C-130 transport aircraft. The MJU-50/B form factor was designed to be the same as the M206 Aircraft Countermeasures Flare (1”x 1”x 8”). The MJU-50/B payload onsists of a pyrophoric payload of the same basic type as the Navy MJU-27A/B, but cut in squares to fit into the 1x1 form factor. This payload is housed in an aluminum case with a metal plate for an end cap, sealed in-place with a sealing compound. The decoy device case is composed of a square tube with an integral impulse cartridge retainer. A separate impulse cartridge squib cup is glued in place to seal the end of the unit. This device was initially procured to support the Marine KC-130J, but is being replaced by the MJU-64/B for future procurements. This decoy device was procured initially to support KC-130J testing, but is being replaced for future use by the Navy MJU-64/B. This decoy device may be used in test, operations and training by all KC-130J aircraft. Characteristics: Weight (lbs.) Length (in.) Width (in.) Height (in.) -

0.670 8.0 1.0 1.0

Carriage Options: KC-130 J/T, UC-35D Dispenser: ALE-47 Impulse Cartridge: BBU-35/B, CCU-145/A Management/Engineering: PMA-272, Jacksonville, Fl Technical Order: NAVAIR 11-140-7

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Nomenclature: MJU-50/B

Name: Decoy

Description: The MJU-50/B infrared countermeasure decoy consists of an aluminum cartridge case purged with nitrogen and containing a payload of stacked special material elements which react with air. Each aluminum cartridge case contains a sealed receptacle cup with O-ring for an impulse cartridge, a plastic/nylon piston, crimped and then sealed, metal end plate. When the impulse cartridge is initiated by the firing pulse, the impulse cartridge receptacle cup frangible membrane ruptures. Pressure inside the canister increases pushing on the piston and breaking the end cap seal deploying the special material payload in the air stream. The special material payload reacts with air in generating infrared energy to decoy surface-to-air and air-to-air missiles. Characteristics: Weight (lbs.) Length (in.) Width (in.) Height (in.) -

0.81 8.00 1.00 1.00

Carriage Options: A-10 C-130 F-16 Dispenser: ALE-40, ALE-45 and ALE-47 Squib/Cart: BBU-35/B Contractor / Status / Improvements / Special Equipment: Contractor - Alloy Surfaces Inc Status Inventory Management/Engineering: 506 CBSS/GBLA, Hill AFB, UT

End Cap View of MJU-50/B

Technical Order: 11A16-47-7

Cutaway View of MJU-50/B

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Nomenclature: MJU-51A/B

Name: Decoy

Description: The MJU-51/B infrared countermeasure decoy consists of an aluminum cartridge case purged with nitrogen and containing a payload of stacked special material elements which react with air. Each aluminum cartridge case contains a sealed receptacle cup with O-ring for an impulse cartridge, a plastic/nylon piston, crimped and then sealed, metal end plate. When the impulse cartridge is initiated by the firing pulse, the impulse cartridge receptacle cup frangible membrane ruptures. Pressure inside the canister increases pushing on the piston and breaking the end cap seal deploying the special material payload in the air stream. The special material payload reacts with air in generating infrared energy to decoy surface-to-air and air-to-air missiles. Characteristics: Weight (lbs.) Length (in.) Width (in.) Height (in.) -

0.81 8.00 2.00 1.00

Carriage Options: F-15, F-16, and C-17 Dispenser: ALE-40, ALE-45 and ALE-47 Squib/Cart: BBU-35/B Contractor / Status / Improvements / Special Equipment: Contractor - Alloy Surfaces Inc Status Inventory Management/Engineering: 506 CBSS/GBLA, Hill AFB, UT Technical Order: 11A16-47-7

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Nomenclature: MJU-52/B

Name: Decoy

Description: The MJU-52/B infrared countermeasure decoy is enclosed in a plastic case. The individual payload is heat sealed in a plastic case (tray), with a plastic cover/strap that is purged with nitrogen and contains a payload of stacked special material foil elements, which react with air. The individual tray of MJU-52/B decoy is dispensed in flight mechanically. When the plastic payload tray of special material hits the air stream it breaks apart scattering the special material out into the air stream. The special material payload reacts with air in generating infrared energy to decoy surface-to-air and air-to-air missiles. Characteristics: Weight (lbs.) Length (in.) Width (in.) Height (in.) -

0.106 3.00 2.50 0.375

Carriage Options: F-15 Dispenser: AN/ALE-58 Dispenser installed in the LAU-128B/A Launcher Contractor / Status / Improvements / Special Equipment: Contractor - Alloy Surfaces Inc Status Inventory Management/Engineering: 506 CBSS/GBLA, Hill AFB, UT Technical Order: 11A16-48-7

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Nomenclature: MJU-53/B

Name: IR Flare

Description: The MJU-53/B flare is a magnesium based IR countermeasure. It consists of an aluminum case, crimped and sealed plastic end cap, rubber spacer, plastic piston, safe and initiation device, flare pellet, and a sealed cartridge cup. It is dispensed and ignited in flight by a BBU36/B impulse cartridge. Characteristics: Weight (lbs.) Length (in.) Width (in.) Height (in.) -

0.80 .0 2.0 1.0

Carriage Options: C-17 Dispenser: ALE-47 Impulse Cartridge: BBU-36/B Contractor / Status / Improvements / Special Equipment: Contractor - Esterline Armtec Status Inventory and in production Improvements - N/A Special Equipment - N/A Management/Engineering: 506 CBSS/GBLA, Hill AFB, UT Technical Order: 11A16-40-7

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Nomenclature: MJU-55/B

Name: IR Decoy Flare

Description: The MJU-55/B Decoy Flare-Device consists of a cylindrical aluminum case approximately 5.8 inches in length and 1.42 inches in diameter with an o-ring sealed aluminum end cap. Internally, it consists of two separate infrared energy generating payloads. One payload is an extruded pyrotechnic flare grain with a bore sensing out-of-line igniter ignition system. This payload is similar to the MJU-38/B only it is approximately 1/3 the size. The other portion of the payload is the same pyrophoric metal foils as are in the MJU-49/B, and comprises the remainder of the payload volume (approximately ½ of the quantity as the MJU-49/B). When functioned, the two payloads of the MJU-55/B each produce an infrared energy source with intensity, rise times, and burn times designed and optimized for use on most military aircraft including higher signature tactical jet aircraft. Characteristics: Weight (lbs.) Length (in.) Width (in.) Height (in.) -

0.730 5.8 1.4 1.4

Carriage Options: F/A-18 A/B/C/D/E/F, AV-8B, EA-6B, E/A-18G Dispenser: ALE-39/47 Impulse Cartridge: CCU-136A/A Management/Engineering: PMA-272, Jacksonville, Fl Technical Order: NAVAIR 11-140-7

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Nomenclature: MJU-57/B

Name: IR Decoy Flare

Description: The MJU-57/B Decoy Flare consists of a cylindrical aluminum case approximately 5.8 inches in length and 1.42 inches in diameter with an o-ring sealed steel/tungsten end cap. Internally, it consists of three major components: the pressed pyrotechnic flare grain composed of Magnesium/Teflon /Viton /Anthracene (MTV/Antracene) composition, the nozzle/fin assembly, and the spring loaded bore sensing out-of-line slider interrupter igniter assembly. The payload is designed to be a thrusting body during function. When functioned, the MJU-57/B has an intensity, rise time, burn time, and forward flying characteristics designed and optimized for use on aircraft capable of speeds greater than 200 KIAS. Characteristics: Weight (lbs.) Length (in.) Width (in.) Height (in.) -

0.804 5.8 1.4 1.4

Carriage Options: F/A-18 A/B/C/D/E/F, AV-8B, EA-6B, E/A-18G, KC-130 F/R, C-130 F/R, P-3C (AIP), P-3C, P-8 Dispenser: ALE-39/47 Impulse Cartridge: CCU-136A/A Management/Engineering: PMA-272, Jacksonville, Fl Technical Order: NAVAIR 11-140-7 5.838” (Max) Igniter Assembly

Tungsten Ballast

Nozzle Section

O-Ring

Case

Impulse Cartridge Cavity

Spring-Loaded Fins (4) Ignition Pellets (2)

Grain Ignition Slurry

Nozzles (8)

Pyrotechnic Grain Body Tube /End Cap

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Outer Case Crimp

Nomenclature: MJU-57 A/B

Name: IR Decoy Flare

Description: The MJU-57A/B is a form/fit/function direct replacement for the MJU-57/B, incorporating design features to improve safety, producibility, reliability and unit cost. The MJU-57A/B design improves safety during manufacturing by reducing human exposure/handling through a much more streamlined and efficient fabrication/assembly process, and will reduce the average unit production cost by 50% or more, as compared to the MJU-57/B. The flare payload consists of a EXTRUDED Magnesium-Teflon®-Viton® (MTV) pyrotechnic grain housed in a plastic body. One end of the body contains a Tungsten ballast to help aerodynamic stability while the other end contains a nozzle for the unit’s thrust. Wrapped around the body is a one-piece spring steel fin. Attached to the nozzle end of the body is a Safe and Arm (S&A) type igniter. The MJU57A/B payload is housed in an aluminum case and is crimped in place. The case contains a plastic cartridge retainer that has been shown to reduce ejection forces onto the dispenser when the unit is functioned. When functioned, the MJU-57A/B has an intensity, rise time, burn time, and forward flying characteristics designed and optimized for use on aircraft capable of speeds greater than 200 KIAS. This decoy provides significant improvement to aircraft survivability through improved countermeasure effectiveness against the advanced IR MANPAD threat. Characteristics: Weight (lbs.) Length (in.) Width (in.) Height (in.) -

0.660 5.8 1.4 1.4

Carriage Options: F/A-18 A/B/C/D/E/F, AV-8B, EA-6B, E/A-18G, KC-130 F/R/J/T, C-130 F/R, P-3 (AIP), P-3, P-8 Dispenser: ALE-39/47 Impulse Cartridge: CCU-136A/A Management/Engineering: PMA-272, Jacksonville, Fl Technical Order: NAVAIR 11-140-7

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Nomenclature: MJU-61/B

Name: IR Decoy Flare

Description: The MJU-61/B Decoy Flare a countermeasure to defeat infrared seeking missiles. This flare will support the Navy’s acquisition of KC-130J Aircraft. The MJU-61/B form factor was designed to be the same as the M206 Aircraft Countermeasures Flare (1”x 1”x 8”). The following figures illustrate the configuration of the MJU-61/B Decoy Flare. The flare payload consists of a Magnesium-Teflon®-Viton® (MTV) pyrotechnic grain equipped with a Safe and Arm (S&A) type igniter. This payload is housed in an aluminum case with a plastic end cap that is crimped in place. The end cap contains an o-ring for a hermetic seal. In between the grain and end cap is a silicone foam rubber pad that takes up tolerances to assure there is always a tight fit of the pyrotechnic payload. The pad also adds protection to the unit during aircraft vibration and rough handling. When functioned, the pyrotechnic payload of the MJU-61/B produces an infrared energy source with intensity, rise times, and burn times designed and optimized for use on most military transport aircraft. The MJU-61/B decoy requires the CCU-145/A (HERO Safe), or BBU-35/B Impulse Cartridge to be dispensed from the D-49/ALE-47 dispensers on the KC130J aircraft. Characteristics: Weight (lbs.) Length (in.) Width (in.) Height (in.) -

0.430 8.0 1.0 1.0

Carriage Options: KC-130 J/T, UC-35D Dispenser: ALE-47 Impulse Cartridge: BBU-35/B or CCU-145/A Management/Engineering: PMA-272, Jacksonville, Fl Technical Order: NAVAIR 11-140-7 Aluminum Polyethylen e Piston

Igniter

MTV Grain

One Piece Case

1.050

Silicone Foam Rubber Pad

End Cap With O-ring

.975

8.105

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Nomenclature: MJU-62/B

Name: IR Flare

Description: The MJU-62/B flare is a boron based IR countermeasure. It consists of an aluminum case, plastic end cap, felt spacer, safe and initiation device, plastic piston, and the flare pellet. It is dispensed and ignited in flight by a BBU-36/B impulse cartridge. Characteristics: Weight (lbs.) Length (in.) Width (in.) Height (in.) -

0.92 8.0 2.0 1.0

Carriage Options: C-17 Dispenser: ALE-47 Impulse Cartridge: BBU-36/B Contractor / Status / Improvements / Special Equipment: Contractor - ATK Thiokol Status Inventory and in production Improvements - N/A Special Equipment - N/A Management/Engineering: 506 CBSS/GBLA, Hill AFB, UT Technical Order: 11A16-40-7

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Nomenclature: MJU-64/B

Name: IR Decoy Device

Description: The MJU-64/B decoy device is a Navy version of the Army M211, consists of an 1” x 1” x 8” aluminum outer case loaded with a pyrophoric metal payload. A plastic piston below the pyrophoric metal payload ensures the payload is ejected from the case. The decoy is closed with an o-ring sealed metal end cap. The items are sealed to prevent contamination or activation of the pyrophoric metal payload. Characteristics: Weight (lbs.) Length (in.) Width (in.) Height (in.) -

0.672 8.0 1.0 1.0

Carriage Options: KC-130 J/T, UC-35D Dispenser: ALE-47 Impulse Cartridge: BBU-35/B or CCU-145/A Management/Engineering: PMA-272, Jacksonville, Fl Technical Order: NAVAIR 11-140-7

Pyrophoric Metal O-Ring

Piston

Case, One-Piece

O-Ring End Cap

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Nomenclature: RR-129/AL

Name: Chaff Cartridge

Description: The RR-129 consists of a cylindrical plastic case approximately 5.8 inches in length and 1.42 inches in diameter. The base end of the device case is flanged to fit the counterbore of an AN/ALE-39 and/or AN/ALE-47 Countermeasures Dispensing Set. The RR-129 consists of four major elements: the chaff payload, piston, and case and end cap. The chaff payload consists of aluminized glass dipoles, precut to three lengths. When the chaff payload is ejected, it disperses in the airstream, creating a cloud that reflects incident radar energy resulting in clutter echoes or false targets in the threat radar systems against which it operates. Item being replaced by RR-129A/AL. Characteristics: Weight (lbs.) Length (in.) Width (in.) Height (in.) -

0.362 5.8 1.42 1.42

Carriage Options: F/A-18 A/B/C/D/E/F, AV-8B, EA-6B, E/A-18G, KC-130 F/R, AH-1W, AH-1Z, UH-1N/Y, CH-46, CH-53 D/E, MV-22, C-130 F/R, P-3C (AIP), P-3C, P-8, MH-60 R/S, SH-60B, HH-60H, MH-53E Dispenser: ALE-39/47 Impulse Cartridge: CCU-136A/A Management/Engineering: PMA-272, Jacksonville, Fl Technical Order: NAVAIR 11-140-7

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Nomenclature: RR-129A/AL

Name: Chaff Cartridge

Description: The RR-129A/AL is an RF passive (chaff) countermeasure, providing aircraft survivability and protection against RF guided threats and tracking radars. It is intended as an improvement over the existing RR-129/AL chaff countermeasure, incorporating an improved end cap and a more durable, opaque plastic case. The new chaff countermeasure will have the same dipole cuts as the original RR-129/AL, with frequency coverage between 2-18 GHz. Characteristics: Weight (lbs.) Length (in.) Width (in.) Height (in.) -

0.368 5.8 1.42 1.42

Carriage Options: F/A-18 A/B/C/D/E/F, AV-8B, EA-6B, E/A-18G, KC-130 F/R, AH-1W, AH-1Z, UH-1N, UH-1Y, CH-46, CH-53 D/E, MV-22, C-130 F/R, P-3 (AIP), P-3, P-8, MH-60 R/S, SH-60B, HH-60H, MH53E Dispenser: ALE-39/47 Impulse Cartridge: CCU-136A/A Management/Engineering: PMA-272, Jacksonville, Fl Technical Order: NAVAIR 11-140-7

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Nomenclature: RR-144A/AL

Name: Chaff Cartridge

Description: The RR-129A/AL is an RF passive (chaff) countermeasure, providing aircraft survivability and protection against RF guided threats and tracking radars. It is intended as an improvement over the existing RR-129/AL chaff countermeasure, incorporating an improved end cap and a more durable, opaque plastic case. The new chaff countermeasure will have the same dipole cuts as the original RR-129/AL, with frequency coverage between 2-18 GHz. Characteristics: Weight (lbs.) Length (in.) Width (in.) Height (in.) -

0.368 5.8 1.42 1.42

Carriage Options: F/A-18 A/B/C/D/E/F, AV-8B, EA-6B, E/A-18G, KC-130 F/R, AH-1W, AH-1Z, UH-1N/, CH-46, CH-53 D/E, MV-22, C-130 F/R, P-3 (AIP), P-3, P-8, MH-60 R/S, SH-60B, HH-60H, MH-53E Dispenser: ALE-39/47 Impulse Cartridge: CCU-136A/A Management/Engineering: PMA-272, Jacksonville, Fl Technical Order: NAVAIR 11-140-7

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Nomenclature: RR-170A/AL

Name: Chaff Cartridge

Description: The RR-170A/AL is a chaff countermeasure. It is the standard USAF tactical chaff cartridge. It consists of a plastic case, plastic end cap, aluminum coated glass fiber payload, plastic piston, and a felt spacer. It is dispensed in flight by a BBU-35/B impulse cartridge. Characteristics: Weight (lbs.) Length (in.) Width (in.) Height (in.) -

0.40 8.1 1.0 1.0

Carriage Options: A-10, MC-130, F-15, F-16, C-17, B-1B, Others Dispenser: ALE-40/45/47/48 Impulse Cartridge: BBU-35/B Contractor / Status / Improvements / Special Equipment: Contractor - Esterline Armtec Status Inventory Improvements - N/A Special Equipment - N/A Management/Engineering: 506 CBSS/GBLA, Hill AFB, UT Technical Order: 11A16-39-7

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Nomenclature: RR-170A/AL (Navy)

Name: Chaff Cartridge

Description: The RR-170A/AL is the standard USAF tactical chaff cartridge. The figure below shows the RCS of a single RR-170 chaff cartridge based on frequency. It shows that the largest RCS occurs at about 3 GHz. However, for the spectrum between 2-18 GHz, which includes most SAM TTRs, the RCS of the RR-170 cartridge is over 50 square meters. Since the typical fighter aircraft RCS varies between 1 and 10 square meters, depending upon frequency and aspect, the RR-170 chaff cartridge should provide a sufficient RCS to mask the aircraft RCS. The Navy’s version is RR-170A/AL with a different NALC (DOCIC) 4W59 NSN 5765-01-262-1157. This is due to the NAVY conducts lot acceptance test on our items there, a new NALC % NSN was developed to ensure Navy conducts these tests when received from the contractor. Characteristics: Weight (lbs.) Length (in.) Width (in.) Height (in.) -

0.260 5.8 1.42 1.42

Carriage Options: KC-130 J/T, UC-35D Dispenser: ALE-39/47 Impulse Cartridge: CCU-136A/A Management/Engineering: PMA-272, Jacksonville, Fl Technical Order: NAVAIR 11-140-7

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Nomenclature: RR-180/AL

Name: Chaff Cartridge

Description: The RR-180/AL is a chaff countermeasure. It consists of a dual payload plastic case. Each payload has a rubber end cap, aluminum coated glass fiber payload with plastic “I” beam supports, plastic piston, and a felt spacer. It is dispensed in flight by a BBU-48/B dual impulse cartridge. Characteristics: Weight (lbs.) Length (in.) Width (in.) Height (in.) -

0.50 8.1 1.0 1.0

Carriage Options: A-10 C-17 F-15 F-16 MC-130 Others Dispenser: ALE-45/47 Impulse Cartridge: BBU-48/B Contractor / Status / Improvements / Special Equipment: Contractor - Esterline Armtec Status Inventory and in production Improvements - N/A Special Equipment - N/A Management/Engineering: 506 CBSS/GBLA, Hill AFB, UT Technical Order: 11A16-45-7

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Nomenclature: RR-188/AL

Name: Chaff Cartridge

Description: The RR-188/AL is a training chaff countermeasure. It consists of a plastic case, plastic end cap, aluminum coated glass fiber payload, plastic piston, and a felt spacer. It is dispensed in flight by a BBU-35/B impulse cartridge. The RR-188 is identical to the RR-170 in form and fit but the RR-188 is only used for training missions. Characteristics: Weight (lbs.) Length (in.) Width (in.) Height (in.) -

0.40 8.1 1.0 1.0

Carriage Options: A-10 B-1B C-17 F-15 F-16 MC-130 Others Dispenser: ALE-40/45/47/48 Impulse Cartridge: BBU-35/B Contractor / Status / Improvements / Special Equipment: Contractor - Esterline Armtec Status Inventory and in production Improvements - N/A Special Equipment - N/A Management/Engineering: 506 CBSS/GBLA, Hill AFB, UT Technical Order: 11A16-39-7

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Nomenclature: RR-196/AL

Name: Chaff Cartridge

Description: The RR-196/AL is a bundled chaff countermeasure. It consists of a dual payload plastic case. Each payload has a rubber end cap, aluminum coated glass fiber payload bundled with Kapton wrap in 3 sections, and a plastic piston with glued on felt spacer. It is dispensed in flight by a BBU-48/B dual impulse cartridge. Characteristics: Weight (lbs.) Length (in.) Width (in.) Height (in.) -

0.50 8.1 1.0 1.0

Carriage Options: F-22A Dispenser: ALE-52 Impulse Cartridge: BBU-48/B Contractor / Status / Improvements / Special Equipment: Contractor - Esterline Armtec Status Inventory and in production Improvements - N/A Special Equipment - N/A Management/Engineering: 506 CBSS/GBLA, Hill AFB, UT Technical Order: 11A16-45-7

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Nomenclature: RT-1489/ALE

Name: GEN-X Decoy

Description: The GEN-X is a small, one-shot, expendable terminal Radio Frequency (RF) threat countermeasure that receives an RF signal from a recognized threat and then transmits RF power to counter airborne and land/sea-based radar guided missiles. The device uses a generic monopulse technique that has been made possible through new monolithic Gallium Arsenide (GaAs) microwave integrated circuit technology. The base end of this case is flanged to fit in counter-bore of an AN/ALE-39 or AN/ALE-47 Countermeasures Dispenser Set (CMDS). The base end of the GEN-X case incorporates a conductive elastomer with acts as a seal for the gases from the impulse cartridge used to dispense the device. The end of the case opposite the flanged base incorporates a coined-end integral to the aluminum case. The major assemblies in the GEN-X are the electronic modules assembly, antenna, battery, and a tail assembly. There are four electronic modules, consisting of monolithic microwave integrated circuits, which perform the basic functions of receiving, amplifying, modulating and transmitting RF energy. The antenna receives and transmits RF energy. The battery is a self-contained, lithium based thermal type that is activated at launch sympathetically by a small primer at the base of the battery. Upon a dispense command, a CCU-136A/A impulse cartridge is initiated by the CMDS and the force of this impulse strikes the primer and initiates the thermal battery. The battery supplies all power to the electrical circuits of the GEN-X. The tail assembly is used to stabilize the decoy's descent. This type of tail is known as a folding wing tail. After the pilot launches the GEN-X, the operation is automatic. The illustration below shows GENX after launch. Characteristics: Weight (lbs.) 1.10 Length (in.) 5.8 Width (in.) 1.42 Height (in.) 1.42 Carriage Options: F/A-18 A/B/C/D/E/F, AV-8B, EA-6B, E/A-18G Dispenser: ALE-39/47 Impulse Cartridge: CCU-136A/A Management/Engineering: PMA-272, Jacksonville, Fl Technical Order: NAVAIR 11-140-7

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Nomenclature: SM-875B/ALE

Name: IR Simulator Flare

Description: SM-875B/ALE Simulator, Flare (hereafter referred to as the SM-875B). The SM-875B consists of a cylindrical plastic case approximately 5.8 inches in length and 1.42 inches in diameter. The base end of the flare case is flanged to fit the counter bore of an AN/ALE-39 or AN/ALE-47 Countermeasures Dispensing Set. The end of the flare case opposite the flanged base is closed with an plastic end cap with an O-ring seal. Internally the SM-875B has small pyrotechnic (MTV based) flare grain, with integral safe & arm bore riding slider mechanism. The flare grain is ignited by igniter pellets within the safe & arm device, which are ignited by the Impulse Cartridge that ejects it from the Dispenser. The SM-875B was developed as a replacement for the previous SM-875A/ALE. This new design will have an igniter (a derivative of the current MJU-32/38 sealed igniter) instead of lighting from the impulse cartridge and a flare grain with effectively 4 times the intensity of the previous SM-875A/ALE. Testing has also shown that this new configuration is visually detectable at much greater distances than the previous training devices, and even has sufficient energy to facilitate use with CATM-9 trainers. Characteristics: Weight (lbs.) Length (in.) Width (in.) Height (in.) -

0.250 5.8 1.42 1.42

Carriage Options: F/A-18 A/B/C/D/E/F, AV-8B, EA-6B, E/A-18G, KC-130 F/R, AH-1W, AH-1Z, UH-1N/Y, CH-46, CH-53 D/E, MV-22, C-130 F/R, P-3C (AIP), P-3C, P-8, MH-60 R/S, SH-60B, HH-60H, MH-53E Dispenser: ALE-39/47 Impulse Cartridge: CCU-136A/A Management/Engineering: PMA-272, Jacksonville, Fl Technical Order: NAVAIR 11-140-7

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Nomenclature: SUU-25

Name: Flare Dispenser

Description: The SUU-25 flare dispensers can carry either eight illuminating flares or eight target marking flares. It is composed of a tubular metal body consisting of four internal tubes enclosed by an outer skin, with a bulkhead at each end. Two flares are loaded in each tube. Flares are ejected from the rear of the dispenser. The flare dispenser itself is not normally expended after use. Characteristics: Weight (lbs.) Length (in.) Diameter (in.) -

260 (unloaded) 96.0 14.0

Carriage Options: A-10 Capacity: 8ea LUU-1, LUU-2, LUU-5 or LUU-19 Squib/Cart: ARD-863, CCU-107 Impulse Cartridges Contractor / Status / Improvements / Special Equipment: Required Parts: ADU-381 Adapter Kit, Shear Pins Management/Engineering: 506 CBSS/GBLA, Hill AFB, UT Technical Order: 11A21-7-7

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CHAPTER ELEVEN 1 June 2009

FUZES and SENSORS

FOR OFFICIAL USE ONLY

INTENTIONALLY LEFT BLANK

Nomenclature: DSU-33 DSU-33A/B General Purpose DSU-33B/B, DSU-33C/B & DSU-33D/B

Name: Proximity Sensor

Characteristics: Fuzing FMU-139, FMU-152A/B Interface JDAM, GP Bombs Power/Safety - FZU-48/B, FZU-55A/B Air Turbine (AF), Fuze Function Control Set (N), and Thermal Battery/Fuzing Employment Options: Weapons Used On - M117, MK 80 Series, BLU-110/111/117 General Purpose Bombs and JDAM (DSU-33A/B Limited Usage) Contractor / Status / Improvements / Special Equipment: DSU-33A/B -Contractor Motorola Inc -Manufacturer Motorola Inc, Scottsdale AZ -Status Inventory DSU-33B/B -Contractor -Manufacturer -Status -

ATK, Tactical Systems Company, LLC ATK, Tactical Systems Company, LLC, Rocket City, WV Inventory

DSU-33C/B -Contractor -Manufacturer -Status -

ATK, Tactical Systems Company, LLC ATK, Tactical Systems Company, LLC, Rocket City, WV Inventory

DSU-33D/B -Contractor -Manufacturer -Status -

ATK, Tactical Systems Company, LLC ATK, Tactical Systems Company, LLC, Rocket City, WV Production USAF/FMS

Management/Engineering: DSU-33 A/B, B/B, C/B, D/B: 506 CBSS/GBLB, Hill AFB, UT Note - Joint Program with the Navy, USAF Lead Service

DSU-33A/B

DSU-33B/B, DSU-33C/B & DSU-33D/B

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Nomenclature: DTU-31/B

Name: Bomb Adaptor Timer-Actuator

Description: The DTU-31/B Timer-Actuator provides a pre-selected time delay to activate BSU-49/B retarders on air launched MK 82 and MK 36 general purpose munitions. It is an electromechanical device that is mechanically initiated by a lanyard attached to the munition release system. This initiation energizes an electronic timing circuit that provides a preset time delay of .650 seconds. At the conclusion of the timing cycle, a pressure cartridge is fired which initiates operation of the BSU-49/B retarders. The timer-actuator is installed directly onto the MK 82 and MK 36 general purpose bombs for use in B-1B Bomber. Characteristics: Weight 2.5 lbs. Length 14.125 in. Delay Time - 0.65 +or- 0.05 sec Interface - B-1B Bomber Employment Options: Weapons Used On Delivery Speed -

A1R, MK 82, MK 36 350 to 600 kt. or 0.9 M

Contractor / Status / Improvements / Special Equipment: Manufacturer - Chamberlain Amptec Corporation Status - Inventory Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT

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Nomenclature: FMU-54A/B Characteristics: Fuze type Interface Power/Safety -

Name: Impact Bomb Fuze

Impact for general purpose bombs Standard Bomb Out-of-line explosive train

Employment Options: Weapons Used On - M117, MK 82, MK 83, MK 84 Explosive Components: Primer None Detonator - M9 Stab T75 Elec for Prox mode Lead - Long - Tetryl 350 mg (two) Short - Tetryl 60 mg (two) Booster 162 g Tetryl Contractor / Status / Improvements / Special Equipment: Status - Inventory (currently being demilitarized) Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT

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Nomenclature: FMU-56/B, D/B

Name: Bomb Proximity Fuze

Characteristics: Fuze type Proximity fuze for cluster bombs Interface Cluster Bomb Power/Safety - Thermal battery/out-of-line explosive train Employment Options: Weapons Used On - CBU-24/B, CBU-29/B Explosive Components: Primer In Thermal Battery Detonator - D74B1 Lead None Booster FZU-1/B Other Two explosive bellows drivers operate rotor Contractor / Status / Improvements / Special Equipment: Status - Inventory (currently being demilitarized) Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT

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Nomenclature: FMU-81

Name: Bomb Impact Fuze

Characteristics: Fuze type Impact for laser guided bombs Interface Laser Guided Bomb Power/Safety - Thermal battery/out-of-line explosive train Employment Options: Weapons Used On - GBU-10, GBU-12 Explosive Components: Primer None Detonator - M36A1 Lead none Booster FZU-2/B Other Two Bellows Drivers for Arm Enable and Mechanical Arming Contractor / Status / Improvements / Special Equipment: Status - Inventory Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT

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Nomenclature: FMU-110

Name: Proximity Fuze

Characteristics: Fuze type Proximity for cluster munitions Interface Cluster Munitions Power/Safety - In thermal battery/out-of-line explosive train Employment Options: Weapons Used On - SUU-30 Dispenser Explosive Components: Primer In Thermal Battery Detonator - D74B1 Lead None Booster FZU-1/B Other Arming Bellows, Locked Rod Bellows; Less 1g Explosives Each Contractor / Status / Improvements / Special Equipment: Status - Inventory (currently being demilitarized) Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT

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Nomenclature: FMU-113

Name: Proximity Fuze

Characteristics: Fuze type Proximity Fuze Interface Standard Bomb (Low Drag) Power/Safety - Alternator/out-of-line explosive train Employment Options: Weapons Used On - M117, MK 82, MK 83, MK 84 Explosive Components: Primer None Detonator - MK 44 Lead 466 mg CH-6 Booster FZU-2/B Other Electric and Stab Actuators Contractor / Status / Improvements / Special Equipment: Status - Inventory Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT

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Nomenclature: FMU-124

Name: Guided Bomb Impact Fuze

Characteristics: Fuze type Impact delay for guided bomb Interface Guided Bomb Power/Safety - GBU-15 guided bomb power supply/out-of-line explosive train Employment Options: Weapons Used On - GBU-15, AGM-130 Explosive Components: Primer None Detonator - MK 100-0 Lead 160 mg Tetryl Booster 123 g Tetryl Other MK 20-0 Bellows Drivers (Two) Contractor / Status / Improvements / Special Equipment: Status - Inventory Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT

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Nomenclature: FMU-139A/B, C/B

Name: Electronic Bomb Fuze

Characteristics: Fuze Type - Impact, Impact Delay, and Proximity (w/ external proximity sensors) Interface Standard Bomb Power/Safety - FZU-48/B Air Turbine (AF), Fuze Function Control Set (N) Employment Options: Weapons Used On - GBU-10, GBU-12, GBU-16, GBU-22, GBU-24, GBU-31/32/38/54, GBU51/52, M117, MK 82, MK 83, MK 84 Contractor / Status / Improvements / Special Equipment: Manufacturer(s) - ATK, Tactical Systems Company, LLC Rocket City, WV - L-3 Fuzing and Ordnance Systems, Cincinnati, OH Status - Inventory (FMU-139A/B) - Production (FMU-139C/B) Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT

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Nomenclature: FMU-140 Series

Name: Dispenser Proximity Fuze

Characteristics: Fuze Type - Proximity fuze with an optional Arm and Fire (timer) mode. It is a repackaged version of the AF FMU-110/B Dispenser Proximity Fuze (DPF). Arming times and functioning altitudes are variable and are selected during preflight on the fuze faceplate. Interface - Navy/Marine Corps ROCKEYE II and GATOR weapons. Power/Safety - is a self-powered doppler radar device acting as a radar altimeter, it has 5 safety interlocks. Employment Options: Weapons Used On - Navy/Marine Corps ROCKEYE II and GATOR weapons. Note: For specific FMU-140 fuze/weapon configurations refer to NAVAIR 11-140-9 Contractor / Status / Improvements / Special Equipment: Contractor Motorola Inc Manufacturer - Motorola Inc, Scottsdale AZ Status Inventory Management/Engineering: NAVAIRSYSCOM PMA-201, NAS Patuxent River, MD and Naval Air Warfare Center Weapons Division, China Lake, CA Notes: 1. Refer to NAVAIR 11-1F-2 for specific FMU-140 fuze functional information including arm times.

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Nomenclature: FMU-143B/B-Q/B

Name: Electronic Bomb Fuze

Characteristics: Fuze Type - Impact delay for penetrating warheads ( 0.030, 0.060, and 0.120 Second Delays) Interface - BLU-109, BLU-113, BLU-116, BLU-121, and BLU-122 Power/Safety - FZU-32B/B Bomb Fuze Initiator, GBU-15/AGM-130 Battery Employment Options: Weapons Used On - GBU-10, GBU-24, GBU-27, GBU-28, GBU-31, AGM-130, AGM-142 (With BLU-109, BLU-113, BLU-116, BLU-121, or BLU-122) Note: For specific FMU-143 fuze/weapon configurations refer to T.O. 11A-1-63, NAVAIR 11-140-10 Contractor / Status / Improvements / Special Equipment: Contractor Kaman Precision Products, Orlando, FL L-3 Fuzing and Ordnance Systems, Cincinnati, OH Manufacturer - L-3 Fuzing and Ordnance Systems Status Inventory (FMU-143B/B and FMU143N/B) - Kaman Precision Products Production (FMU-143B/B) - L-3 Fuzing and Ordnance Systems Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT Notes: 1. Joint Program with Navy, Air Force Lead Service. 2. Navy FMU-143 versions: FMU-143 E/B , FMU-143 K/B, FMU-143 L/B, and FMU-143 M/B with impact delays of 0.060, 0.030, 0.060, and 0.120 seconds respectively. AF FMU-143 versions: FMU-143 B/B, FMU-143 D/B, FMU-143F/B, FMU-143 G/B, FMU-143 H/B, FMU-143 J/B, FMU-143 N/B, FMU-143P/B, and FMU-143Q/B with impact delays of 0.060, 0.060, 0.030, 0.060, 0.120, 0.120, 0.060, 0.060, 0.120 seconds respectively. 3. Refer to T.O. 11A7-32-7 or NAVAIR 11-1F-2 for specific FMU-143 fuze functional information including arm times.

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Nomenclature: FMU-152A/B

Name: Electronic Bomb Fuze

Characteristics: Fuze Type - Multi-Delay, Multi-Arm and Proximity Sensor Compatible with General Purpose BlastFrag and Hardened-Target Penetrator Warheads. Cockpit selectable in-flight (prior to release) when used with JDAM weapons. Interface - MK 82, MK 83, MK 84, BLU-109, BLU-110, BLU-111, BLU-113, BLU-122 Power/Safety - FZU-55A/B Bomb Fuze Initiator, GBU-15/AGM-130 Battery, Navy FFCS Employment Options: Weapons Used On - GBU-10, GBU-12, GBU-15, GBU-16, GBU-24, GBU-27, GBU-28, GBU-31, GBU-32, GBU-38, and AGM-130 Contractor / Status / Improvements / Special Equipment: Contractor Kaman Precision Products, Orlando, FL Manufacturer Kaman Precision Products, Orlando, FL Status Production Management/Engineering: 679 ARSS, Eglin AFB, FL

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Nomenclature: FZU-39/B

Name: Proximity Fuze Sensor

Characteristics: Type Proximity sensor used with dispenser fuze for cluster bombs Interface Cluster Bombs Power/Safety - Powered by thermal battery Employment Options: Weapons Used On - SUU-64/B, SUU-65/B Explosive Components: Primer - N/A Detonator - N/A Lead - N/A Booster - N/A Contractor / Status / Improvements / Special Equipment: Status - Inventory Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT

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Nomenclature: M904E4

Name: Mechanical Bomb Fuze, Nose

Characteristics: Fuze type Impact delay for general purpose bombs (0.00, 0.01, 0.25, 0.05, or 0.1 second delays) Interface Standard Bomb Power/Safety - Mechanical arming upon release (arming vane), spring-driven out-of-line explosive train Employment Options: Weapons Used On - M117, MK 82, MK 83, MK 84, BLU-110, BLU-111, BLU-117 Explosive Components: Primer None Detonator - M35 Lead 100 mg Tetryl Booster 72.3 g Tetryl Requires use of M-9 Delay and M146 (AF), M148 (N) Nose Adapter Booster (Separate Components) Contractor / Status / Improvements / Special Equipment: Status - Inventory Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT

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Nomenclature: M905

Name: Mechanical Bomb Fuze, Tail

Characteristics: Fuze type Impact delay for general purpose bombs (0.00, 0.01, 0.25, 0.05, or 0.1 second delays) Interface Standard Bomb Power/Safety - Mechanical arming upon release (arming vane), spring-driven out-of-line explosive train Employment Options: Weapons Used On - GBU-10, GBU-12, M117, MK 82, MK 83, MK 84 Explosive Components: Primer M42 Detonator - M35 Lead None Requires use of M-9 Delay and M147 Tail Adapter Booster and ATU-35/B Vane Drive Assembly (Separate Components) Contractor / Status / Improvements / Special Equipment: Status - Inventory Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT

ROTOR

DETONATOR

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Nomenclature: M907

Name: Mechanical Fuze, Airburst

Characteristics: Fuze type Mechanical airburst for cluster bombs Interface Cluster Bombs Power/Safety - Mechanical arming upon release (arming vane) Employment Options: Weapons Used On - CBU-24, CBU-49, CBU-62, M120 Photoflash Bomb Explosive Components: Primer M72 Detonator - None Lead None Booster 6.18 g Black Powder Contractor / Status / Improvements / Special Equipment: Status - Inventory (current inventory not employed by USAF, currently being demilitarized) Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT

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Nomenclature: MK 339 Mods 0 & 1

Name: Mechanical Time (MT) Fuze

Description: The MK 339 Mods 0 & 1 is a mechanical time fuze used with dispenser weapons. The primary and option functioning delays are preset during assembly at the factory. The fuze is preset at 1.2 seconds for primary delay, and the option delay is preset at 4.0 seconds. These time delays can be reset during weapon preparation to meet various tactical requirements. The functional delays for both the primary and option modes of the fuze can be adjusted from 1.2 to 50 seconds (Mod 0) or 1.2 to 100 seconds (Mod 1) in 0.1 second increments. The fuze safe/arm indicator is viewed through the indicator observation window in the upper nose fairing. There is a layer of green foil at the base of the indicator bubble. The fuze is in a safe condition when the green foil is intact, and it is armed when the green foil is pierced by the indicator pin. Characteristics: Fuze type Proximity Fuze for Cluster Munition Interface Cluster Munition Power/Safety - Out-of-Line Explosive Train Employment Options: Weapons Used On - CBU-59/B, CBU-72, MK 20, PDU-5/B (loaded with Leaflets), SUU-76C/B (empty) Explosive Components: Primer None Detonator - MK 43 Mod 2 Lead None Booster None Contractor / Status / Improvements / Special Equipment: Status - Inventory Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT

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CHAPTER TWELVE 1 June 2009

MUNITIONS MATERIEL HANDLING EQUIPMENT (MMHE)

FOR OFFICIAL USE ONLY

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INTENTIONALLY LEFT BLANK

Name: 2.75 Inch Rocket Transport Module Description: This module transports or stores up to 60 fully assembled 2.75 inch rockets configured in lengths of approximately 54 to 72 inches (rocket lengths vary on rocket motor and warhead combinations). Characteristics: Height (in.) - 33.0 Width (in.) - 80.0 Length (in.) - 53.0 Contractor / Status / Improvements / Special Equipment: Status - Procurement/Inventory Management / Engineering: 578 CBSS/GBLB, Robins AFB, GA Technical Order: 35DA3-6-38-1

2.75 Inch Rocket Transport Module With Rocket Access Closed

2.75 Inch Rocket Transport Module With Rocket Access Doors Open

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Name: 20mm Ammunition Loading System (ALS) Replenisher Assembly Description: The 20mm Ammunition Loading System (ALS) Replenisher assembly is used to transfer 20mm ammunition from storage into the ALS, the Universal Ammunition Loading System (UALS), or the Linkless Ammunition Loading System (LALS) for transportation to the flight line. While performing this function, it simultaneously and independently receives spent cases and/or unfired ammunition from the loader assembly. The replenisher will function when supplied with either built (loose) or linked ammunition. Characteristics: Weight (lbs.) Height (in.) Width (in.) Length (in.) -

330.0 39.3 30.7 79.4

Contractor / Status / Improvements / Special Equipment: Status - Inventory Management / Engineering: 578 CBSS/GBLB, Robins AFB, GA Technical Order: 35D30-4-11-1

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Name: 20mm Replenisher Table Description: The 20mm ammunition loading system replenisher assembly is used to transfer 20mm ammunition from storage into the ALS, UALS, or LALS for transportation to the flight line. While performing this function, it simultaneously and independently receives spent cases and/or unfired ammunition from the loader assembly. The replenisher will function with loose ammunition only. Characteristics: Weight (lbs.) Height (in.) Width (in.) Length (in.) -

185.0 40.75 36.25 41.25

Contractor / Status / Improvements / Special Equipment: Status - Procurement Management / Engineering: 578 CBSS/GBLB, Robins AFB, GA Technical Order: 35D30-4-21-1

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Nomenclature: ADU-537 A/E

Name: Missile Munitions Loading Adapter (MMLA)

Description: The Missile Munitions Loading Adapter (MMLA) is to be used in conjunction with the MJ-1 Bomb Lift Truck or Munition Handling Unit (MHU-194/E) Manually Operated Lift Truck (MOLT) to facilitate loading air-to-air missiles on tactical aircraft. The main components of the unit are a rotating missile cradle and a removable lifting boom. The manually operated boom is used to lift munitions out of All-Up-Round-Containers (AURCs) and set them on the cradle without the need for additional handling equipment. Characteristics: Weight (lbs.) Height (in.) Width (in.) Length (in.) -

161 18.5 (minimum) 23.0 39.0 (minimum)

Capacity: Boom (lbs.) Cradle (lbs.) Table (lbs.) -

525 (A) / 1050 (B) 525 1050

Contractor / Status / Improvements / Special Equipment: Status - Inventory Management / Engineering: 578 CBSS/GBLB, Robins AFB, GA Technical Order: 35DA3-6-37-1

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Nomenclature: A/E32K-3

Name: Munitions Assembly Conveyor (MAC)

Description: The MAC is designed for the rapid build up of many different types of conventional munitions. The main components include four roller conveyors, two gantries with pneumatic hoists, two triple bomb bars, four rail conveyors with 30 munitions dollies, interface control board, arming wire dispenser, on and off load lighting, adjustment bar, and restraint strap Characteristics: Rail Conveyor (assembled) Weight (lbs.) - 165 each table Height (in.) - 33.13 Width (in.) - 27.5 Length (ft.) - 40 ft total length - 10 ft each table

Gantry (assembled) Weight (lbs.) - 1695.2 Height (ft.) - 14.4 Width (in.) - 149.5 Length (in.) - 181.6

Capacity: Capacity (net lbs.) - 4,000 (Load on gantries, hoists, or triple bomb bar) Contractor / Status / Improvements / Special Equipment: Status - Inventory Management / Engineering: 578 CBSS/GBLB, Robins AFB, GA Technical Order: 35D2-17-1

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Nomenclature: A/E32K-9

Name: Munitions Assembly Conveyor II (MAC II)

Description: The MAC II replaces the aging MAC system enhancing the capability to assemble bomb bodies into fully operational munitions with fuze, guidance section and tail kit. The system provides an increased lifting capacity, decreased system and munitions assembly/disassembly time, and improved lighting. In addition, MAC II will extend capability service life to 30 years. Characteristics: System weight (lbs.) System length (ft.) System height (ft.) System width (ft.) -

11,001 72 16.5 21.5

Capacity: 6000 lb load on gantries, hoists, and triple bomb bar Contractor / Status / Improvements / Special Equipment: Status - Procurement/Inventory Management / Engineering: 578 CBSS/GBLB, Robins AFB, GA Technical Order: 35D2-17-11

MAC II

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Nomenclature: ALE-40 Series

Name: Chaff/Flare Transport Module

Description: This module transports ALE-40 chaff and flare magazines from the munitions storage area to the flightline. The maximum capacity per module is 40 magazines. It secures to either the MHU-141, MHU-226 or MHU-110 trailer. It replaces all existing local manufactured transport modules. Characteristics: Height (in.) - 47.0 Width (in.) - 18.0 Length (in.) - 73.0 Contractor / Status / Improvements / Special Equipment: Status - Procurement/Inventory Management / Engineering: 578 CBSS/GBLB, Robins AFB, GA Technical Order: 35DA3-6-38-1

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Nomenclature: ALE-50 Series

Name: Decoy Transport Module

Description: This module transports ALE-50 decoy magazines from the munitions storage area to the flightline. The maximum capacity per module is 30 magazines. It secures to either the MHU141, MHU-226 or MHU-110 trailer. It replaces all existing local manufactured transport modules. Characteristics: Height (in.) - 35.0 Width (in.) - 34.0 Length (in.) - 56.0 Contractor / Status / Improvements / Special Equipment: Status - Procurement/Inventory Management / Engineering: 578 CBSS/GBLB, Robins AFB, GA Technical Order: 35DA3-6-38-1

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Nomenclature: ALS

Name: 20mm Ammunition Loading System (ALS) Loader Assembly

Description: The 20mm ammunition loading system loader assembly is used to transfer 20mm series ammunition into an aircraft gun system on the flight line. While performing this loading function, the loader assembly simultaneously downloads cleared rounds and/or spent cases from the gun system of the F-16. Characteristics: Weight (lbs.) Height (in.) Width (in.) Length (in.) -

2558 (full) 37.50 68.00 181.38

Contractor / Status / Improvements / Special Equipment: Status - Inventory Management / Engineering: 578 CBSS/GBLB, Robins AFB, GA Technical Order: 35D30-4-10-1

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Nomenclature: ARS

Name: Aluminum Rail Set (ARS)

Description: The ARS Kit allows for six different rail configurations using the same basic parts and assemblies on the trailer deck and can be mounted on 40-foot and munition handling trailers (MHU). The Rail set can be assembled with wood dunnage for rolling hard munitions or rollerized rails for sliding soft skin munitions. The rails can be configured in lateral or longitudinal directions. Characteristics: Configuration MHU Existing Rail Longitudinal (-10) MHU Wood Longitudinal (-30) MHU Existing Rail Lateral (-50) 40/38 Foot Center Trolley Longitudinal (-70) 40/38 Foot Wood Longitudinal (-110) 40/38 Foot Center Trolley Lateral (-130)

Maximum Load 10 X CBU/MK82 18 X MK82 4 X MK84 30 X CBU/MK82 42 X MK82 12 X MK84

Contractor / Status / Improvements / Special Equipment: Status - Inventory Management / Engineering: 578 CBSS/GBLB, Robins AFB, GA Technical Order: 35DA5-2-1

MHU Existing Rail Lateral (-50)

40/38 Foot Wood Longitudinal (-110)

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Nomenclature: BDU-33/MK 106

Name: Practice Bomb Transport Module (40 Round Version)

Description: The BDU-33/MK 106 Practice Bomb Transport Module protects training munitions from the elements during delivery to and from the flight line or loading area. Each module has the capacity to carry 40 practice bombs. Characteristics: Height (in.) - 35.0 Width (in.) - 27.0 Length (in.) - 57.0 Contractor / Status / Improvements / Special Equipment: Status - Procurement/Inventory Management / Engineering: 578 CBSS/GBLB, Robins AFB, GA Technical Order: 35DA-3-6-38-1

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Nomenclature: BDU-33/MK 106

Name: Practice Bomb Transport Module (80 Round Version)

Description: The BDU-33/MK 106 Practice Bomb Transport Module protects training munitions from the elements during delivery to and from the flight line or loading area. Each module has the capacity to carry 80 practice bombs. Characteristics: Height (in.) - 35.0 Width (in.) - 27.0 Length (in.) - 114.0 Contractor / Status / Improvements / Special Equipment: Status - Procurement/Inventory Management / Engineering: 578 CBSS/GBLB, Robins AFB, GA Technical Order: 35DA-3-6-38-1

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Nomenclature: GFU-7/E

Name: 30mm Ammunition Loader

Description: The purpose of the loader is to load 30mm ammunition from shipping and storage containers into the A-10 aircraft within a specific time and to simultaneously unload and deposit spent and / or live rounds of ammunition from the aircraft gun system into Ammunition and Storage containers. Characteristics: Weight (lbs.) Height (in.) Width (in.) Length (in) -

2,800 (loaded with tubes) 92.0 69.0 194.0

Contractor / Status / Improvements / Special Equipment: Status - Inventory Management / Engineering: 578 CBSS/GBLB, Robins AFB, GA Technical Order: 35D30-4-12-2

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Nomenclature: LALS

Name: 20mm USAF Linkless Ammunition Loading System (LALS)

Description: The LALS loader assembly is used to transfer 20mm series ammunition into F-15 and F-16 gun systems on the flightline. While performing this loading function, the loader assembly simultaneously downloads cleared rounds and/or spent cases from the gun system. Characteristics: Weight (lbs.) Height (in.) Width (in.) Length (in.) -

3,275 (full, loaded with 1800 rounds) 37.5 68.0 189.0

Contractor / Status / Improvements / Special Equipment: Status - Inventory Management / Engineering: 578 CBSS/GBLB, Robins AFB, GA Technical Order: 35D2-19-1

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Nomenclature: MHU-40

Name: Truck, Lift, Aerial Stores

Description: The Munitions Handling Unit (MHU-40) is a 10,000 pound capacity, self-propelled hydraulically operated lifting and positioning device used to lift and attach aerial stores. It consists of a main structural frame on which is mounted a cantilevered lift boom, extendable outriggers and auxiliary frames for sheet metal. Characteristics: Weight (lbs.) Width (in.) Length (in.) -

7,230 73.5 (front), 52.0 (rear) 185.0

Capacity: Total (net lbs.) 10,000 Load on Forks (net lbs.) - 6,000 Load on Head (net lbs.) - 7,230 Contractor / Status / Improvements / Special Equipment: Status - Inventory Management / Engineering: 578 CBSS/GBLB, Robins AFB, GA Technical Order: 35D3-9-21-1

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Nomenclature: MHU-83

Name: Truck, Lift, Aerial Stores

Description: The Munitions Handling Unit (MHU-83) is a self-propelled, hydraulic operated lift truck. The rear wheels are driven by a 27.5 HP gasoline/diesel engine and connected to a conventional limitedslip differential by a hydrostatic drive system. Characteristics: Weight (lbs.) Width (in.) -

6,380 69.500 (front), 53.625 (rear)

Capacity: Load on Forks (net lbs.) - 6,000 Load on cradle (net lbs.) - 7,000 Contractor / Status / Improvements / Special Equipment: Status - Inventory Management / Engineering: 578 CBSS/GBLB, Robins AFB, GA Technical Order: 35D5-3-8-31

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Nomenclature: MHU-110/M

Name: Munitions Handling Trailer

Description: The MHU-110/M munitions handling trailer is designed for temporary storage and transportation of conventional munitions only. It is a ten-wheel flatbed carrier capable of transporting any munitions within the load, dimensional and stability limitations. It is air-transportable, and capable of transporting loads of conventional ammunition up to 15,000 lbs. The accessories furnished with the trailer are general-purpose items. The MHU-110 is equipped to be attached to a tow vehicle having a pintle hook with safety pin and electrical connections for running lights. Special adapters/accessories required during loading/transportation of a munition will be listed in the applicable munition or aircraft manual. The trailer is typically used to transport GP bombs, GBU’s, CBU’s, all up round containerized missiles (AURC), and the MAC/MACII Systems. Characteristics: Weight (lbs.) Height (in.) Width (in.) Deck Length (in.) Wheel Base (in.) Ground Clearance (in.) Tongue Length (in.) Brakes - Service Turning Angle -

4,200 30.0 87.0 180.0 110.0 10.0 74.0 6 Wheel Hydraulic, Parking - 4 Wheel Mechanical Hand Lever 45 Degrees

Capacity: Capacity (net lbs.) - 15,000 Restraint Capacity: Main Deck Rings (lbs.) - 10,000, Side Deck Rings (lbs.) - 25,000 Contractor / Status / Improvements / Special Equipment: Status - Inventory Management / Engineering: 578 CBSS/GBLB, Robins AFB, GA Technical Order: 35D3-2-26-1

HMU-110M with B1B Chaff and Flare Transport Module

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Nomenclature: MHU-141/M

Name: Munitions Handling Trailer

Description: The MHU-141/M munitions handling trailer designed for temporary storage and transportation of conventional, nuclear munitions and other stores. It is a four-wheeled automotive steering vehicle capable of transporting loads of up to 5500 pounds. The MHU-141 is equipped to be attached to a tow vehicle having a pintle hook with safety pin and electrical connections for running lights. The center section of the deck is hinged and is lifted open for most all up round (AUR) munitions configurations. One large toolbox at the rear of the trailer is provided for storage of accessories; side toolboxes are no longer required. The trailer is generally used to transport GP bombs, GBU’s, CBU’s and missiles in and out of containers. Characteristics: Weight (lbs.) Height (in.) Width (in.) Deck Length (in.) Wheel Base (in.) Ground Clearance (in.) Tongue Length (in.) Brakes - Service Turning Angle -

2900 32.0 84.0 126.0 89.0 8.0 88.0 4 Wheel Hydraulic, Parking - 2 Wheel Mechanical Hand Lever 40 Degrees

Capacity: Capacity (net lbs.) - 5,500 Restraint Capacity: Main Deck Rings (lbs.) - 10,000, Side Deck Rings (lbs.) - 25,000 Main Deck Link/Pin Assembly (lbs.) - 1,350 Contractor / Status / Improvements / Special Equipment: Status - Inventory Management / Engineering: 578 CBSS/GBLB, Robins AFB, GA Technical Order: 35D3-2-27-1

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Nomenclature: MHU-194/E

Name: Manually Operated Lift Truck (MOLT)

Description: The MOLT is a towable, manual approach to munitions handling capable of loading/unloading external stores on tactical aircraft. Characteristics: Weight (lbs.) - 1,900 Height (in.) 62.0 (tow bar in up position) Width (in.) 59.0 Length (in.) 136.0 Capacity: Lifting Capacity (net lbs.): Using Top Hole in Outer Arm Assembly Using Lower Hole in Outer Arm Assembly With Extension Lift Arms Adapter With Fork Adapter -

2,450 (lbs.) 1,200 (lbs.) 1,000 (lbs.) 1,000 (lbs.)

Contractor / Status / Improvements / Special Equipment: Status - Inventory Management / Engineering: 578 CBSS/GBLB, Robins AFB, GA Technical Order: 35D3-9-23-1

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Nomenclature: MHU-196/M

Name: Munitions Handling Trailer

Description: The MUH-196/M is a heavy-duty, U-type frame vehicle used for transporting munitions and in loading/unloading operations on strategic aircraft. The MUH-196/M is equipped to be attached to a tow vehicle having a pintle hook and safety pin, air connections for brakes, and electrical connections for running lights and hydraulic fluid circulation. Characteristics: Weight (lbs.) Height Width Length (ft.) -

39,100 4 feet 2 inches 9 feet 8 inches to 13 feet 1 inch, adjustable 30

Capacity: Capacity (net lbs) - 40,000 Contractor / Status / Improvements / Special Equipment: Status - Inventory Management / Engineering: 578 CBSS/GBLB, Robins AFB, GA Technical Order: 11N-H5083-2

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Nomenclature: MHU-204/M

Name: Munitions Lift Trailer

Description: The MHU-204/M is a heavy-duty, U-type frame vehicle used for transporting munitions and in loading/unloading operations on strategic aircraft. The Munitions Lift Trailer is equipped to be attached to a tow vehicle having a pintle hook and safety pin, air connections for brakes, and electrical connections for running lights and hydraulic fluid circulation. Characteristics: Weight (lbs.) Height Width Length -

40,000 +/-500 4 feet 5 inches 9 feet 8 inches to 13 feet 1 inch (adjustable) 30 feet

Capacity: Lifting Capacity (net lbs.) - 40,000 maximum Contractor / Status / Improvements / Special Equipment: Status - Inventory Management / Engineering: 578 CBSS/GBLB, Robins AFB, GA Technical Order: 11N-H5083-2-1/4

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Nomenclature: MHU-226

Name: Munitions Handling Trailer

Description: The MHU-226 is a Universal Munitions Trailer designed for temporary storage and transportation of conventional and nuclear munitions. It is a four-wheeled munitions trailer with Double-Ackerman steering (four wheel coordinated). It is air-transportable, and capable of transporting loads up to 12,000 pounds conventional or 8,000 pounds for nuclear weapons. The MHU-226 is equipped for towing via a pintle-hook with safety pin and it has electrical connections for brake and tail-lights. The deck has three hinged door panel openings. With the center panels open, long loads can be carried. With the center panels closed, and the fore and aft panels open, smaller and combination loads can be carried. The trailer functions as a flat bed with all door panels closed. Two storage boxes at the front and three at the rear of the trailer provide for storage of accessories. A stowage container is provided to stow the wheel chocks. The tow bar is interchangeable with the MHU-141 and MHU-110. Explosive placards are attached to the trailer. The trailer is typically used to transport GP bombs, GBU’s, CBU’s, all up round containerized missiles (AURC), and the MAC/MACII Systems. Characteristics: Weight (lbs.) 3000 Height (in.) 31.5 Width (in.) 87.0 Deck Length (in.) 180.0 Wheel Base (in.) 156.0 Tongue Length (in.) 80.0 Brakes - Service - four Wheel Hydraulic, Parking - four Wheel Mechanical (two Hand Levers, one operates front axle and one operates rear axle) Capacity: Capacity (net lbs.) - 12,000 lbs conventional or 8,000 lbs nuclear Restraint Capacity - Main Deck Rings (lbs.) - 10,000, Side Deck Rings (lbs.) - 25,000 Contractor / Status / Improvements / Special Equipment: Status - Production/ Procurement Management / Engineering: 578 CBSS/GBLB, Robins AFB, GA Technical Order: 35D3-2-31-1

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Nomenclature: MJ-1

Name: Truck, Lift, Aerial Stores

Description: The MJ-1 Lift Truck is a self-propelled, hydraulic operated lift truck. The rear wheels are driven by a 27.5 HP gasoline/diesel engine and connected to a conventional differential by a hydraulically operated and controlled steering. It is used in the loading/unloading of munition items and normally installed equipment items. Characteristics: Weight (lbs.) 3,800 Width (in.) 52.25 Length (in.) 144.75 Capacity: Lift Capacity (net lbs.) - 3,000 Contractor / Status / Improvements / Special Equipment: Status - Inventory Management / Engineering: 578 CBSS/GBLB, Robins AFB, GA Technical Order: 35D3-2-25-1

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Nomenclature: MRA

Name: Mechanical Ram Assembly (MRA)

Description: The Mechanical Ram Assembly is a multiple sleeve, hydro-mechanical lifting device. The primary purpose is to increase the lift height capability of the MJ-40 and MHU-83D/E bomb lift trucks in support of the B-1B/B-2A aircraft. Characteristics: Weight (lbs.) Retracted Height (in.) Extended Height (in.) Lift Capacity (lbs.) -

500 37.0 83.0 5000

Contractor / Status / Improvements / Special Equipment: Status - Inventory Management / Engineering: 578 CBSS/GBLB, Robins AFB, GA Technical Order: 35D3-9-29-1

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Nomenclature: UALS

Name: 20mm Universal Ammunition Loading System (UALS) Loader Assembly

Description: The 20mm ammunition loading system loader assembly is used to transfer 20mm series ammunition into F-15, F-16 and F-22A aircraft gun systems on the flight line. While performing this loading function, the loader assembly simultaneously downloads cleared rounds and/or spent cases from the gun system. Characteristics: Weight (lbs.) Height (in.) Width (in.) Length (in.) -

3,100.00 (full) 37.50 68.00 189.38

Contractor / Status / Improvements / Special Equipment: Status - Inventory Management / Engineering: 578 CBSS/GBLB, Robins AFB, GA Technical Order: 35D30-4-15-1

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Munitions Materiel Handling Equipment (MMHE) Focal Point Description: The MMHE Focal Point, 688 ARSS/DO, Eglin AFB, FL, provides design and engineering support for MMHE/armament locally manufactured equipment (LME). The MMHE Focal Point’s web site (https://peonet.eglin.af.mil/mmhe) contains the most current list of available MMHE/LME drawings. On the web page, select “Drawings” for a listing of available drawing packages. Drawings may be ordered directly from the website. MMHE Focal Point Website Content: 105MM Ammunition Transport Module 105MM Breech Removal Tool 105MM Fuze Installation/Removal Tool 10K Test Weight Stand (also approved for munitions) 2.75 Inch Rocket Stand Assembly, Hardened Aircraft Shelter 2.75 Inch Rocket Storage Stand 2.75 Inch Rocket Warhead Stand 20MM Barrel Holding Fixture 20MM Barrel SFD Stand 20MM Gun Exit-Entrance Fixture 20MM Gun Maintenance Stand 20MM Gun Sling 20MM Gun Storage Stand 20MM Universal Delinker Loader (UDL) Chute 30MM Ammunition Container Handling Adapter 30MM Drum Stand 36-Inch Adapter Assembly 4X Missile Storage Stand 40MM Gun Maintenance Stand 50K ISO Maintenance Stand 6.5 Inch Height Adapter Adapter Assembly, MHU-83/MJ-4 to ADU-537 A/E A-10 Air & Fuel Plug Removal Tool A-10 Gun Sensor Tool AGM-65 Grounding Post Guide Tool AIM-120 Wing and Fin Maintenance Fixture AIM-120 Wing and Fin Unlock Tool AIM-7/120 Missile Lift Beam AIM-9 GCS Safety Stand AIM-9 GCS/Warhead Stand AIM-9 MBA Paint Stand AIM-9 Missile Stand Extension ALA-17 Flare Fixture ALE-40 Chaff/Flare Tool Kit ALE-48/49 (B-1 Chaff and Flare) Transport Module ALE-52 (F-22 Chaff and Flare) Transport Module AME Mobility Racks

F-22 Pylon Loading Adapter F-22 Pylon Maintenance Stand F-22 Pylon Storage Stand Flightline Service Cart Combination BDU/C&F Flightline Service Cart for Chaff and Flare Flightline Service Cart for Practice Bombs FMU-139 Cable Installation Tool FMU-139 Fuze Ring Spanner/Torque Adapter FMU-143 Locking Ring Removal Tool FMU-152 Fuze Ring Spanner/Torque Adapter Fuze Adapter for T46E5/E4 Tail Adapter Booster Fuze Retaining Nut Tool FZU-32 Locking Ring Tool GAU-8 Breech Bolt Maintenance Fixture GBU Fuze Well Seal Nut Wrench GBU-15 Wing/Control Surface Transport Rack GBU-24/27/28 Fin Transport Container GBU-28 Loading Adapter and Dolly GBU-28 Mobile Stand GCU-30 Adapter Tool Hardened Aircraft Shelter (HAS) Missile Rack HC-130 Pyrotechnics Transport Module Heavy AURC Dolly Initiator Well Gauge for General Purpose Bombs JASSM Container Latch Tool JDAM Strake Alignment Tool, MK-83 JDAM Strake Alignment Tool, MK-84 KMU-572 Nose Extension Spanner Wrench LALS Ammo Container Lift Sling LALS/UALS Checking Fixture LAU-106 Maintenance Stand Launcher/Bomb Rack Tool M206 Flare Can Cage M61A2 Gun Transport Stand MAC Dolly Stop Kit MAC Torque Retainer Fixture Maintenance Table

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AME Service Trailer ATU-35 Tab Tool AURC Bi-Level Dolly, Container AVEL Loading Adapter B-1B Conventional Bomb Module Adapter (T-Bar) B-1B Conventional Bomb Module Storage Stand B-1B Swing Arm Tool B-52 MER Pylon Transportation Rack (MHU-141) B-52 Pylon Lift Beam B-52 Pylon Loading Adapter B-52 Stub Pylon/HSAB Maintenance/Loading Stand B-52 Stub Pylon/HSAB Transport Adapter B-52 Yoke Handling/Loading Adapter B-52 Yoke Lift Beam (Aluminum) B-52 Yoke Maintenance Stand Modification B-52/B-2 Extender, Trolley, RLA B-52/B-2 Rotary Launcher Adapter BDU-33 Lug Installation Tool BDU-33 Practice Bomb Table BLU-109 Retainer Bolt Torque Collar Bobtail/Trailer/ Cable Electrical Tester Bomb Handling Fork Adapter Bomb Rack Maintenance Stand BRU-57 Handling Adapter Assembly BRU-57 Maintenance Stand Chaff/Flare Squibbing Fixture Clamp Ring Torque Tools Clamp Ring/Forward Adapter/Retainer Bolt Separation Fixture CNU-131 T-Bolt Removal Tool Combination Spanner Wrench Container Latch Tool, SDB Container Latch Tool Kit Crane Boom Extension DTU-31 Alignment Tool Kit F-15 Pylon Loading Adapter F-15 Pylon Loading Adapter - PLUS F-15 Weapons Pylon Storage Stand F-16 Ammo Drum Handling Bar F-16 Pylon/Launcher Storage Stand F-16 Wing Weapons Pylon Lift Adapter

MHU Strap Adapters MHU-101 Fork Adapter Assembly MHU-101 Fork Adapter Clamp MHU-101 Fork Adapter Dolly MHU-110 Rail Stop MHU-110 Rail Removal Tool MHU-110 Stabilizer Jack MHU-114 Stacking Stands Missile AURC Fork Hoist Adapter Missile Connector Alignment Tool Missile Dislodge Tool (AIM-9L/M, AIM-9X, AIM-120) MJ-1 Steps MK-82/84 Retainer Bolt Torque Collar Munitions Cradle Stand Munitions Maintenance/Inspection Table Munitions Trailer Stacking Ramps and Pushbar PBAR Loading Adapter RAM Maintenance and Handling Dolly Screw Removal Tool, 40MM Can Shipping and Storage Container, LAU-106/1760 Tray Slip Clutch Tool Mount (Vice Bench) Support Beam, MHU-141/226 Deck Lid T-2 Pallet Locking Device Kit TER Bucking Block TER Storage Rack Test Set Cart Thread Chase Tool, Fuze Well UALS Forklift Pockets UALS Front End Alignment Tool Universal AME Stand Universal Bomb Hoisting Adapter (6 Bomb Bar Beam) Universal Bomb Lifting Bar Universal Munitions Y-Stand Weapons Vault Trainer Wing and Fin Container Skid Pads with Modification Procedure Wooden Rail Set, 40 ft/25 ft Trailers Wooden Rail Set, MHU-110 Y Stand Dolly Y Stand Dolly, Expanded

Contractor / Status / Improvements /Special Equipment: Status - Active Management/Engineering: 688 ARSS/DO, Eglin AFB, FL

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INTENTIONALLY LEFT BLANK

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CHAPTER THIRTEEN 1 June 2009

EMERGING TECHNOLOGIES

FOR OFFICIAL USE ONLY

INTENTIONALLY LEFT BLANK

Nomenclature: TBD

Name: Accurate Low Collateral Munition (ALM)

Capability: Attack targets in no/low collateral damage environments. Description: Accurate Low Collateral Munition (ALM) prosecutes targets in collateral damage sensitive environments such as urban warfare and Close Air Support (CAS). Characteristics: Guidance - JDAM GBU-38 Warhead - MK82 composite case Explosive - Multiphase Blast Explosive (MBX) Fuzes FMU-139A/B, FMU-143, FMU-152A/B Carriage Options: Aircraft: (same as for MK82) A/OA-10A B-1B F-117A B-2A AV-8B B-52H F/A-18A-F F-15A-E S-3A F-16

Launcher/Rack: (14 in. Lug Spacing)

Contractor / Status / Improvements / Special Equipment: Status - Conceptual Design Management/Engineering: AFRL/RWOB /AGMSW Eglin AFB, FL Technical Order: TBD

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Nomenclature: TBD

Name: Advanced Precision Kill Weapon System (APKWS)

Capability: APKWS will provide low cost precision strikes against point targets while minimizing collateral damage, using a new semi-active laser seeker/guidance section, integrated with components of the Hydra-70, 2.75” Rocket system Description: APKWS provides an affordable means of assured kills of soft and lightly armored targets with minimal collateral damage based on precision guidance integrated with existing Hydra-70 components. APKWS is expected to be the weapon of choice for the above target set during operations in urban terrain or for aerial fire support missions in close proximity to friendly forces. The APKWS will be employed from attack, armed reconnaissance, or other helicopters equipped with a laser designator. Threaded interfaces at both ends of the APKWS semi-active laser guidance section allow for simple mechanical mating to the legacy Hydra-70 warhead and rocket motor. Key Performance Parameters (KPPs) are maximum range of 5,000 meters, minimum range of 1,500 meters, probability of hit of 80% within 2 meters of laser spot and guided rocket reliability of 94%. APKWS will IOC on the AH-1W in 1st Qtr FY11. Characteristics: Guidance - Semi-Active Laser Seeker Warhead - M151, 10-pound high explosive (see Chapter 18) Length 75 inches Weight 35 pounds Lock-on-after-launch mode Increased stowed kills Modular Upgradeable Carriage Options: AH-64 Apache OH-58D Kiowa Warrior AH-1W/Z Super Cobra AH-6 Little Bird UH-60 Direct Action Penetrator Contractor / Status / Improvements / Special Equipment: Contractor - BAE Status In Development Management/Engineering: U.S. Army PM JAMS Redstone Arsenal, AL; NAVAIR PMA-242 Patuxent River, MD; Technical Order: TBP

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Guidance Section

MK66 MOD 4 Solid Rocket Motor

M151 Warhead w/ M423 Fuze

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Nomenclature: TBD

Name: Area Dominator (AD)

Capability: Dominate enemy surface operations in a selected Area of the battle space, >24 hr Persistent ISR and ability to engage with lethal effect, full kill chain capability under Weapon System Operator (WSO) controlled ROE. Description: The Area Dominator (AD) is the equivalent of a Tier II armed Unmanned Aerial Systems (UAS) weapon system. Unlike UASs the AD is designed for compressed carriage delivery from either traditional aircraft suspension equipment or directly employed from its tactical shipping container system mounted in a wide variety of platforms. AD can operate independently or cooperatively in swarms and be deployed in mixed type applications. Operates under most weather and above most surface environments, persistence and standoff distances are allocated under mission requirements within the 24hr maximum endurance. CONOPS for this system is documented in AAC-XR-TR-06-001. Characteristics: Navigation - Anti-Jam GPS/INS with data link and other covert options, LADAR+ Sensors Carriage Dimensions Payloads: -Length 48 in. Type 1 -Width 7.5 in. Common Smart Submunition (CSS) -Height 7.75 in. 3 Tri-Mode Samara Wing Explosively Baseline Flight Configuration Formed Projectile (EFP) Submunition -Length 47.5 in. independently targetable and releasable; -Height 6 in. Army program development. -Span 12 ft -Operational Altitude >400 ft (AGL) Type 2 -Max Altitude >15,000 ft (MSL) Precision Guided Sub-Missile (PGSM) -Speed 60-120 knots 3 x 60mm 12.5” Semi-Active Laser, -Wpn Empty Weight 82 lbs. INS/GPS Guided sub-missile, multi-mode, -Wpn Fuel Weight 20 lbs. warhead, EFP, anti-personnel/materiel, -Endurance >24 hrs Unfunded. -No. of Submunitions 0-3 f(type) Estimated Cost (in production) - <$150K ea. Type 3 Near silent acoustic signature - <60 dBa Gateway, Extends Line-of-Sight Comm, Multi-Channel Relay, Digital Video Rec. Carriage Options: Links Airborne Network with Smart Military Aircraft: (Potential Full Integration) Munitions Network, may include more Fighter: F-22A, F-35 cueing sensors for increased area Bomber: B-52H, B-1B, B-2A search. Unfunded. Armed UAV: MQ-1, MQ9 Platform: (No Integration Required) Type 4 Any Military Cargo Aircraft, Combined Persistent ISR/Gateway with Any Military Utilty or Commercial Aircraft unitary warhead (10 lb) blast frag capable of open door operations penetrator for kamikaze attack mode. with cargo tie downs or accessible chair rail systems Any Submarine or Surface Vessel Any Ground Site or Vehicle

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Contractor / Status / Improvements / Special Equipment: Status - TD for Cargo Carriage Common Container Completed Rudder •Folding •All-Moving

Management/Engineering: AFRL/RWOB, Eglin AFB, FL Technical Order: TBP Flight control Strip Ailerons

Fuel High efficiency Powerplant

Deployable Refueling

Low acoustic signature folding Propeller Off-set Counter-balanced Single Bladed Folding Propeller is easily stowed & more efficient in low RN flight conditions

Sensor/Seeker and Laser Designator

Submunitions

Advanced Avionics Package

Compressed lift and control surface packaging

High L/D Wings •Folding •Telescoping

Bottom-Dispensing Skeet-type Munitions Top & Bottom-Dispensing Microprobes

Compressed Carriage Configuration 1.75

Refuel Probe

7.75 7.5

46 (Folded Wing) Folded Propeller

Army Common Smart Sub-Munition (CSS)

Precision Guided Sub-Missile (PGSM)

13-5

Store, Ship, Stack, Select, Shoot, Cargo Carriage Common Container Launcher

FOUO

Nomenclature: TBD

Name: Close Combat Lethal Recon (CCLR)

Capability: Locate, and destroy low collateral damage targets in urban terrain. Description: The Close Combat Lethal Recon (CCLR) is a short range anti-vehicle/personnel weapon with low explosive yield and low collateral damage that will engage targets that are hard to locate and track in close and urban terrain. Characteristics: Weight 5 lbs Range 5 km/ground Warhead NEW/Type explosive - < 1lb/frag Interface Data link via RF Guidance Man-in-loop utilizing optical seeker and data link Time of Flight unknown Technology Readiness Level - TRL4 Carriage Options: Aircraft: UAVs Ground Launch

Launcher/Rack:

Contractor / Status / Improvements / Special Equipment: Management/Engineering: AFRL, Eglin AFB, FL Technical Order: N/A

13-6

FOUO

Nomenclature: TBD

Name: Conventional Strike Missile (CSM)

Capability: Prompt, precise, global conventional strike from CONUS to neutralize fixed and fleeting time sensitive targets regardless of anti-access threats. Description: Conventional Strike Missile (CSM) is the Air Force Space Command vision for a weapon system capable of putting conventional payloads precisely on a target within minutes of release order. The key component of CSM is a hypersonic glide payload delivery vehicle designed to deliver and deploy a variety of conventional payloads worldwide. A CSM technology demonstration program provides the opportunity for an initial operating capability using residual assets in the FY13/14 timeframe. Characteristics: The CSM payload delivery vehicle will be capable of carrying ~1000 lbs of environmentally protected munitions or other payloads internally and, following re-entry, directly engage the target or decelerate to the appropriate release speed and altitude to dispense munitions/payloads over/near the target area. The vehicle’s high velocity and maneuvering capability provides the delivery vehicle relative immunity from future surface-to-air and spacebased threats. The booster range, combined with the delivery vehicle’s atmospheric glide capability, provides near global coverage. Additionally, the delivery vehicle’s significant aerodynamic cross-range capability allows compliance with any imposed overflight restrictions and avoids dropping booster stages on land. Carriage Options: Basing: CONUS coastal basing. Potential launch platforms include existing expendable commercial/excess rocket motors or by a tailored non-nuclear legacy booster stack drawn from a “family of motors.” Contractor / Status / Improvements / Special Equipment: Status - An operationally relevant FY12 CSM technology demonstration flight is currently funded in the context of the Congressionally established Defense-Wide Conventional Prompt Global Strike (CPGS) Account. As planned, the FY12 demonstration flight will leverage critical CPGS technologies matured in the context of the joint Air Force/DARPA Falcon Hypersonic Technology Vehicle Demonstration Program and will include the deployment of a Kinetic Energy Projectile (KEP) warhead against a representative CPGS target. Management/Engineering: SMC/XR, Los Angeles AFB, California Technical Order: N/A

Notional View of CSM Payload Delivery Vehicle

13-7

FOUO

Nomenclature: TBD

Name: Direct Attack Guided Rocket (DAGR)

Capability: Defeat targets in urban operations, while minimizing collateral damage. Description: DAGR is a semi-active laser guidance kit that adapts to 2.75-inch/70mm rockets to provide guided-rocket performance comparable to that of the precision-strike laser-guided HELLFIRE II missile. DAGR is being developed by Lockheed Martin as a non-developmental item to fill the gap between unguided rockets and the HELLFIRE weapon system by providing a precisionstrike, air-to-ground weapon for non-armored or lightly-armored high-value targets close to civilian assets or friendly forces, while limiting collateral damage. DAGR integrates proven seeker, guidance, electronics, integrated flight simulation, and countermeasures technologies developed on HELLFIRE and Joint Common Missile (JCM) to provide a highly lethal and precise 2.75-inch/70mm weapon. Our baseline DAGR guidance kit offers 2.75-inch/70mm rockets lock-on-after-launch and lock-on-before-launch capability, target handoff, enhanced built-in test, and laser coding from the cockpit. Its off-axis capability increases the engagement envelope, providing additional field of view for angle-of-attack, moving targets, and wind. Accompanied by Lockheed Martin’s 4-pack launcher, the DAGR system allows quick and easy integration on all HELLFIRE platforms including Cobra, Apache, Seahawk, Kiowa and Tiger helicopters. Fully compatible with the M299 and M310 “smart” launchers, DAGR increases launcher load out by up to four times and provides single-switch operational flexibility, drawing upon a payload that includes DAGR as well as multiple variants of HELLFIRE for multi-mission capability. Additionally, due to DAGR’s compatibility with the HELLFIRE weapon system, the usual resources for fielding a new weapon system – development, training, additional equipment and force structure – are avoided. Characteristics: Carriage Options: Any fixed or rotary wing aircraft that currently is carrying 2.75 inch rockets or the AGM-114 Hellfire. Contractor / Status / Improvements / Special Equipment: Contractor - Lockheed Martin Corporation Missiles and Fire Control Business Development Status - Integrated and test fired from AH-64D Longbow Apache Management/Engineering: Technical Order: N/A

13-8

FOUO

Nomenclature: TBD

Name: Hard Target Void Sensing Fuze (HTVSF)

Capability: Penetrate, survive and function in legacy BLU-109 and BLU-113 warheads against hardened targets/ hard and deeply buried targets (HDBT) by using void sensing algorithms or preset time delays fuzing functions. Description: The Hard Target Void Sensing Fuze (HTVSF) is an advanced system that will provide programmability, in-flight cockpit selectability, safing and multi-time delay arming, and multifunction (time delay and void sensing) fuzing for legacy weapon systems (GBU-31 & EGBU-28) to penetrate and destroy hardened targets protected by multiple layers of reinforced concrete, and Hard and Deeply Buried Targets. HTVSF Program Priorities: Survivability in hard concrete (5,000 PSI to 15,000 PSI), Void Sensing, Cockpit Selectability, and Compatibility with GBU-31 and EGBU-28 weapon systems. Characteristics: Fuze Type - Programmable, Cockpit Selectable (in flight prior to release), Multi-Time Delay Arming, and Void Sensing/Multi-Time Delay Fuzing functions Interface - GBU-31 & EGBU-28 weapon systems Power/Safety - Air Turbine (FZU) or any alternate power source that complies with safety requirements Employment Options: Weapons Used On: GBU-31 & EGBU-28 Contractor / Status / Improvements / Special Equipment: Status - JCTD awarded a contract on 31 Mar 2008 for 27 months Management/Engineering: Planning - 679 ARSS Eglin AFB, FL JCTD, Engineering Manufacturing Development (EMD), and Production - 679 ARSS Eglin AFB, FL Technical Order: N/A

13-9

FOUO

Nomenclature: TBD

Name: High Speed Strike Weapon (HSSW)

Capability: Prompt, precise, strike from outside area defense to neutralize fixed and fleeting time sensitive targets regardless of anti-access threats. Description: High Speed Strike Weapon (HSSW) is a multi-spiraled program developing a high speed weapon system effective against a set of time critical targets and compatible with current fighter and bomber aircraft. The goal is to use a near-term technology demonstration to support feasibility of a cost-effective HSSW in the 2015 timeframe. Conceptual designs are being developed by integrating existing weapon technologies including: guidance, propulsion, avionics, warhead, airframe, and seeker. Focus has been aimed at an F-35 internal carriage weapon system with non-traditional range extension technology. Characteristics: High Speed Strike Weapon (HSSW) Guidance GPS/INS, Network Centric, Seeker Cruise Speed Mach 3-5 Range 50-500 NM Time of Flight <15 minutes Propulsion SRM, LFRJ, Turbojet, Ramjet Payload Weight - 50-100 lbs Carriage Options: Aircraft: Threshold: F-35 Objective: B-52H, B-2A Contractor / Status / Improvements / Special Equipment: Contractor - Miltec Missiles & Space Company Status Progress includes the development of conceptual designs for a demonstrator and tactical platform. Preliminary system requirements are set at Mach 3-5, mass 1000 lbs, and range of 350+ for the most restrictive case, internal to JSF weapons bay. Miltec will also look at possible load outs for a bomber class weapon. In the concept phase of the program, Miltec reviewed HSSW system trades to include the propulsion, warhead, navigation, aerodynamics, and trajectory shaping. Current efforts for Task I include on-going concept design development of the payload, trajectory, packaging, control system, aerodynamics, navigation, propulsion, and lethality. Future tasks planned include a detailed design, fabrication, subsystem testing, system integration, ground tests, and flight test. Management/Engineering: AFRL/RWAV, Eglin AFB, FL Technical Order: N/A

13-10

FOUO

Nomenclature: TBD

Name: I-500 Warhead Technology Demonstration (TD)

Capability: Defeat Hard and Deeply Buried Targets. Description: The I-500 is a small penetrator to attack Hard and Deeply Buried Targets, with a blast-frag capability similar to an Mk-82 GP bomb. Characteristics: Guidance -KMU-582 JDAM Guidance Kit (GBU-38) Warhead - 500 lb class warhead, leverages legacy penetrator design of scaled Joint Advanced Strike Technology (JAST), employs Eglin Steel-1 and AFX-757 Explosive, utilizes thermoplastic shell technology, I-500 with shell matches Mk-82 shape and mass properties. Explosive - 120 lbs AFX-757 Fuze - FMU-143 and FMU-152 (JPF) Carriage Options: Aircraft: Objective: B-2A Threshold: F-18 F-15A-E F-16A-D

Launcher/Rack: SBRA

BRU-57

Contractor / Status / Improvements / Special Equipment: Contractor - GD-OTS (penetrator), Triton Systems (Shell) Status AFRL Technology Demonstration Management/Engineering: AFRL/RWAV and AAC/XRS, Eglin AFB, FL Technical Order: N/A

13-11

FOUO

Nomenclature: TBD

Name: I-1000 Warhead Technology Demonstration (TD)

Capability: Defeat Hard and Deeply Buried Targets. Description: The I-1000 warhead is a penetrator munition to attack Hard and Deeply Buried Targets. Characteristics: Guidance - GBU-32 JDAM Guidance Kit Warhead - 1000 lb class warhead, employs Eglin Steel-1 and AFX-757 explosive, robust fuze well assembly w/integral booster, utilizes syntactic foam shell technology; I-1000 with shell matches Mk-83 shape and mass properties. Explosive - 125 lbs AFX-757 Fuze FMU-143 and FMU-152 (JPF) Carriage Options: Aircraft: F/A-18C-F F-22A AV-8B Planned: F-35 (Navy)

Launcher/Rack:

Contractor / Status / Improvements / Special Equipment: Contractor - Dynetics (Penetrator), Triton Systems (Shell) Status AFRL Technology Demonstration, In-house R&D Program Management/Engineering: AFRL/RWAV and AAC/XRS, Eglin AFB, FL Technical Order: N/A

Shell Matches Mk-83 Shape

13-12

FOUO

Nomenclature: TBD

Name: Joint Air-to-Ground Missile (JAGM)

Capability: Advanced Line of Sight (LOS) and Beyond LOS, Precision Point and Fire-and-Forget (active and passive) seeker targeting modes, Increased Range, Increased Lethality, Adverse Weather, Multi-purpose Killer (Moving and Stationary Hard and Non-Armored Targets and Military Operations on Urban Terrain (MOUT)), Autonomous Target Acquisition, Inherent Countermeasure Capability, Lock-on Before Launch (LOBL) and Lock-on After Launch (LOAL). Description: The JAGM system is an ACAT 1D Joint Army/Navy/USMC program with the Army as lead service. The JAGM system will be a common air-to-ground precision guided missile for use by joint service manned and unmanned aircraft to destroy high value stationary, moving, and relocatable land and naval targets from standoff range in day, night, adverse weather and obscured battlefield conditions. JAGM will provide a common, multi-mode weapon capable of providing both current and future aviation platforms with reactive targeting capabilities satisfying the sum of needs across the joint platforms and eliminating the requirement for separate upgrades to multiple existing missile systems. The ability to be employed from air and potential ground platforms provides increased operational flexibility and increased survivability (both missile and platform) while reducing the logistic footprint in theatre. JAGM will utilize modularity in design to provide for shelf life extension, enable technology insertion for future required capabilities, and aide eventual demilitarization. The JAGM will replace the HELLFIRE and Maverick family of missiles as well as the aviation-launched TOW. Characteristics: Guidance Multi-mode seeker Weight (lbs) 108 Diameter (in) 7 Length (in) 70 Warhead Multi-purpose Propulsion Boost-Sustain Carrier / Shipboard Operability Carriage Options: Milestone C Threshold Platforms: Apache (AH-64D) Super Cobra (AH-1Z), Super Hornet (F/A-18 E/F) Other Threshold Platforms: Seahawk (MH-60R) SkyWarrior Unmanned Aerial System (UAS) and Army Recon/Attack Rotary Wing Objective Platforms: Joint Strike Fighter (JSF) Hornet (F/A-18 C/D), Harrier II Plus (AV-8B) Super Cobra (AH-1W) Apache (AH-64A), Kiowa Warrior (OH-58D) Blackhawk (MH-60M DAP) Little Bird (AH-6M), Multi-Mission Maritime Aircraft (MMA)

13-13

FOUO

Launcher: Fixed Wing Launcher, M299 Launcher, Modified M299 Launcher Contractor / Status / Improvements / Special Equipment: Status - 27-Month Technology Development (TD) Phase Contract awarded 11 Sep 2008. - Milestone B and Engineering and Manufacturing Development (EMD) Contract Award scheduled for 1st Quarter FY 2011. - Milestone C is scheduled for FY 2015 followed by Initial Operational Capability (IOC) in FY 2016. Management/Engineering: Joint, Army led program with the Navy and USMC, under Program Executive Office (PEO), Missiles and Space, Joint Attack Munition Systems (JAMS) Project Office, Redstone Arsenal, Alabama Technical Order: N/A

13-14

FOUO

Nomenclature: TBD

Name: Low Cost Guided Imaging Rocket (LOGIR)

Capability: LOGIR will provide a low cost, inertially guided with terminal infrared image homing weapon capability to the current family of unguided 2.75” rockets for engagement of a wide variety of soft to lightly armored moving and fixed targets. Description: LOGIR is a low cost accuracy enhancement kit for existing rockets. LOGIR offers precision accuracy and maximum stowed kills per sortie with minimum collateral damage concerns. The LOGIR Launcher provides pre-launch communications and individual tube select capabilities. The LOGIR project began in 2000 and is still under way. Its primary objective is to significantly improve the warfighter's ability to address moving and fixed targets with an emphasis on moving targets. LOGIR allows the warfighter to designate the target using the existing targeting Forward Looking Infrared Radar (FLIR). Once designated, the pilot can fire the rocket and leave the area. LOGIR will use the FLIR targeting data to fly to the target, and acquire and track the target to weapon impact. Characteristics: Guidance - Fire & Forget imaging IO/ER Seeker Warhead - M151, 10-pound High Explosive (see Chapter 18) Carriage Options: H-60 Series AH-64 Apache OH-58D Kiowa Warrior AH-1W/Z Super Cobra AH-6 Little Bird Contractor / Status / Improvements / Special Equipment: Status - Science and Technology Program Management/Engineering: Science and Technology Manager-NAWC China Lake; Transition Manager-NAVAIR PMA242/Engineering-NAWC, China Lake Technical Order: TBP

13-15

FOUO

Nomenclature: TBD

Name: Low Cost Mini-Cruise Missile (LCMCM)

Capability: “Kick down the door” into denied battlespace, degrade and defeat anti-access capabilities, and strike high-value targets in the opening phase of major conflict. Description: The Low Cost Miniature Cruise Missile (LCMCM) is an interdiction weapon that provides long stand-off capability against a variety of land and sea targets in an anti-access or other scenario. The LCMCM provides the new capability to defeat mobile targets from long standoff (up to 1100 nm) while also having the capability to defeat light fixed structures, provide ISR data en route, and provide bomb damage information. Characteristics: Guidance: Cruise Missile - Anti-jam INS/GPS, datalink for enroute updates, low cost Wide Area Search Synthetic Aperture Radar (SAR) which includes Ground Moving Target Indicator (GMTI), High Resolution Radar (HRR), and SAR modes for onboard F2T2 Precision Guided Sub-munitions - datalink from missile, I2R and/or SAL Warhead: Advanced combined effects for soft, medium, hard, mobile targets and light fixed Propulsion: Turbofan Dimensions Payloads: -Length 144 in. Type 1 -Width 14 in. Precision Guided Submunitions (PGS) -Height 14 in. with low cost datalink, uncooled IR -Wing Span 12 ft. terminal seeker, and combined effects -Cruise Altitude 30K ft warhead -Cruise Speed 0.7 Mach -Total Weight 980 lbs. Type 2 -Range >1100 NM Unattended ground sensors and -No of Submunitions 4 multi-function probes Estimated Cost (in prod) $350K ea. Carriage Options: Internal on F/A-22, F-35, B-1B, B-2A, and B-52H and external on F-15 and F-16 Contractor / Status / Improvements / Special Equipment: Contractor - NA Status - AFRL Tech Development Management/Engineering: AFRL/RWOB Technical Order: N/A

13-16

FOUO

Turbofan Propulsion

LCMCM with Submunitions

13-17

FOUO

Nomenclature: BLU-127/B GBU-57/B

Name: Massive Ordnance Penetrator (MOP)

Capability: Penetrate hard and deeply buried targets (HDBT) or large blast/frag for surface targets. Description: Massive Ordnance Penetrator (MOP) Concept: Penetrator for hard and deeply buried target defeat and large blast & fragment damage for tunnel and above ground targets. MOP Program Priorities: Survivability, Lethality, Penetration. Characteristics: Guidance - INS/GPS w/Grid Fin Control Warhead - Total Weapon Assembled Weight: 28,914 lb Dimensions - Length: 246 in. (excludes Aft Carriage Bracket); Outer Diameter: 31.5 in.; Inner Diameter 24.5 in. Penetrator - Case Material: Forged HP 9-4-20M Steel; Case wall thickness: 3.5 in.; Caliber Radius Head Ratio: 2.0 Explosive - 5593 lbs PBXN-113 / AFX-757 Explosive Fill w/ 40 lbs PBXN-109 in Fuze Shroud Fuze SDB Fuze / MAFIS Fuze Tail kit JDAM Guidance Control Unit (GCU) ATACMS Actuation System (4 actuators, 1 control unit) ATACMS batteries (2 each) Fuze Interface Electronics (1 each) SDB Arming Generators (3 each) BDI canisters (2 each) Carriage Options: Aircraft: (Objective) B-2A B-52H

Launcher/Rack: Bomb-as-Launcher Carriage concept, MOP replaces internal rotary launcher in B-2A/B-52H weapon bay.

Contractor / Status / Improvements / Special Equipment: Boeing (Prime), Dynetics, General Dynamics & Ellwood National Forge Management/Engineering: Funded by DTRA, contracted through AFRL/RWAV Eglin AFB, FL Technical Order: N/A

13-18

FOUO

Nomenclature: TBD

Name: Shredder

Capability: Disrupt enemy access to hardened chemical/biological agent storage and production facilities while minimizing agent release Description: Shredder is a modified BLU-109 designed to deny/disrupt Chemical/Biological (CB) Agent storage and production facilities, and limit collateral damage from release of CB Agent. It will deny the use of stored CB Agents and render unusable fixed, hardened CB agent storage and production facilities. The explosive charge will rupture metal and plastic containers of CB Agents and the agent defeat fill will create a large intense fireball that will neutralize agents in powder, liquid, or aerosol form. Characteristics: Guidance - INS/GPS (GBU-31 JDAM) Warhead - 2,000 lb Penetrator (modified BLU-109) - 100 lb PBXN-109 HE - 400+ lb Agent Defeat Fill Fuze - FMU-143 (modified) Carriage Options: Aircraft: (Objective) B-1B B-2A B-52H F-15 E

Launcher/Rack:

Contractor / Status / Improvements / Special Equipment: Contractor - ATK Status ATD Completed Management/Engineering: AFRL/RWMO, Eglin AFB, FL Technical Order: N/A

Modified Closure Plate

Fill Port and Covers Arming Well Modified (welded)

BLU-109 Bomb Body Modified

AD Fill

Standard Explosive Fill Retaining Fuze Liner Modified BLU-109 Ring Burster Tube (Roller and Welded 4130 Steel)

Nose Tube Support Formable material

Nose Cap

Anti-Slosh Baffle Welded to Burster Tube

13-19

FOUO

Nomenclature: TBD

Name: Small Diameter Bomb Increment II (SDB II)

Capability: Adverse Weather, Standoff, Precision Autonomous Attack against Fixed/Movable/Moving Time Sensitive Targets. Description: SDB II is a 250 lb-class weapon and is designed as a small autonomous, conventional, air-toground, precision bomb able to strike mobile and stationary/re-locatable targets from a standoff range. The SDB II weapon system consists of the weapon; a 4-place common carriage system; and a mission planning system. SDB II provides increased load-out and kills per sortie on current and future aircraft, such as the Joint Strike Fighter (F-35). Characteristics: CRD Weapons Code - None Guidance Midcourse: INS/GPS with Weapon Data Link updates; Terminal: Onboard Multi-mode Seeker (MMW/IR), Semi-Active Laser (SAL), or differential INS/GPS Control Tail Aerodynamic Autopilot Proportional Guidance Class 250 lb Guided Munition Weight (lbs.) - TBD Length (m) TBD Diameter (mm) - TBD Warhead TBD Blast/Frag modes available Range 40 NM Standoff Explosive TBD Fuze Part of All-Up-Round Carriage Options: Aircraft: Threshold: F-15E (USAF) F-35B (USMC) F-35C (USN) Objective: F-22A F-35 (USAF) F-16 A-10 MQ-9 B-1B B-2A B-52H F/A-18E/F

Launcher/Rack: BRU-61A (4-place Common Carriage System)

Contractor / Status / Improvements / Special Equipment: Contractors - Boeing and Raytheon Status Risk Reduction (RR) (FY 06 though FY09) F-15E RAA - FY14, F-35B/C (USMC/USN) RAA - FY16 Management/Engineering: 682 ARSS, Eglin AFB, FL Technical Order: Will be included in 11K39-2-7 before fielding

13-20

FOUO

Nomenclature: TBD

Name: Small Smart Weapon (SSW)

Capability: SSW is the warfighter’s answer to precision attack using a small, lethal warhead against targets in areas requiring low collateral damage. Description: The Small Smart Weapon (SSW) is a lightweight, compact munition that provides the warfighter with low cost lethality against a broad target set. SSW is adaptable to multiple launch platforms, including manned or unmanned systems. Targets include structures, personnel, lightly armored vehicles, trucks, cars, missile launchers, and artillery or gun positions. SSW uses a semi-active laser (SAL) seeker for man-in-the-loop terminal guidance, and can be tailored to use planned, imaging infrared (I2R), shortwave infrared (SWIR), or millimeter wave (MMW) seekers. The precision provided by these seeker types ensures accuracy to less than one meter and dramatically reduces the possibility of collateral damage. SSW can be deployed from various tube launch systems currently in use or from the M-299/M-310 launch system used to launch Hellfire missiles from helicopters and Predator UAVs. When used with the M-299/M310, SSW slides onto the rail and communicates with the launch platform in exactly the same way as the Hellfire. Three SSW weapons can be deployed on a single rail used for one Hellfire. When used from a tube launcher, up to two SSW weapons can be launched from a single tube to enhance the load-out of the launch platform. Features: • Design uses Commercial Off-the-Shelf (COTS) components • Various seeker types available as needed • Adaptable front end works with each seeker type • Multiple warhead options available for use against various target types • Deployable in adverse weather • Less than one meter Circular Error Probability (CEP) • Compatible with Adaptive Carriage Environment (ACE) Tube launch System, SUU-25 Tube Launch System, and M-299/M-310 Launch System Characteristics: Range Over 10 nautical miles maximum Weight Less than 35 pounds Length 21.5 in Diameter - 4.25 in Warhead - BattleAxe Carriage Options: (Possible) Aircraft: MQ-1B Predator Unmanned Aerial Vehicle (UAV) MQ-9 Reaper UAV C-130 Caravan Armed ISR Platforms

Launcher: Modified M299 Rail Modified M299 Launcher

Contractor / Status / Improvements / Special Equipment: Contractor - Lockheed Martin Corporation Missiles and Fire Control Business Development

13-21

FOUO

Management/Engineering: Technical Order: N/A

M229 Missile Launcher

2 Hellfire Missiles

Push Plate

Interface Adapter

FZU inlet covered by mount Retaining 6 SSW

Six SSW Mounted on M229 Missile Launcher

13-22

FOUO

Nomenclature: TBD

Name: Very Small Missile (VSM)

Capability: Persistent Close and Danger Close Air Support (CAS) with Minimal Collateral Damage/Fratricide Description: Very Small Missile (VSM) is an air-to-ground (low collateral damage) missile that will be capable of prosecuting multiple/simultaneous engagements in day/night and adverse weather conditions. Due to its size and weight it can be mounted on persistent aerial systems to provide rapid response to support troops on the ground. It will be ideal to engage stationary/mobile light armor vehicles in an urban or open terrain environment. This stand-off precision weapon will provide close and danger close air support. Target set includes non-hardened, stationary/mobile and light armor. Will have a 10-15 nm range for firing altitudes of 25-40 K ft AGL. Characteristics: Guidance - GPS/INS with in-flight updates, plus laser seeker for optimal terminal guidance Warhead - Lethal and Non-Lethal 10-12 lbs with various fuzing and blast effects -- HE Blast-frag. proximity/impact/delayed fuzing for soft targets -- Shaped charge, impact fuzing for hardened and discrete targets -- Less-than-lethal, flash/bang, pepper spray, etc. Concept of employment - Prior to launch, missile(s) selected and programmed with target coordinates, laser code and fuzing option. It will be launched or pneumatically tube-ejected from the aircraft. Length 57 in Diameter - 5 in Weight 55 lbs Carriage Options: Aircraft: AC-130 Persistent Surface Attack Systems (PSAS) MQ-1L Predator MQ-9 Reaper Extended Range Multi-Purpose (ERMP) UAV (Army)

Launcher/Rack BRU-61

Contractor / Status / Improvements / Special Equipment: Status - Concept Development Management/Engineering: AAC/XRS Eglin AFB, FL Technical Order: N/A

13-23

FOUO

Nomenclature: TBD

Name: Tactical Wide Area Search Munition (WASM) (Powered Low Cost Autonomous Attack System (PLOCAAS))

Capability: Air to Surface, Standoff against Mobile and Relocated vehicles and Time Sensitive Targets Description: The recently completed Powered Low Cost Autonomous Attack System (PLOCAAS) Advanced Technology Demonstration (ATD) developed a suite of technologies to provide Wide Area Search Munition (WASM) capability with human in the loop control provided via datalink, with the ability to search, identify and service ground mobile targets with significant target location error unable to be targeted otherwise. The LADAR sensor technology is coupled with advanced Autonomous Target Recognition (ATR) algorithms to cue the human operator to the location of targets and then as directed execute an attack against those targets using a multimode warhead whose lethal mechanism can be selected on the fly to maximize the effect upon the target. The ability to search an extended area after ingress is provided by a high lift to drag airframe and a highly efficient and affordable small turbojet engine specifically developed by AFRL. These coupled technologies provide a robust wide area search munition capability. Characteristics: Weight 95 lbs (configuration flown during ATD) / 140 lbs (Tactical configuration, BRU-61 compatible) Length 3 ft (configuration flown during ATD) / 6 ft (Tactical configuration, BRU-61 compatible) Range 100 NM (configuration flown during ATD) / 250 NM (Tactical configuration, BRU-61 compatible) Warhead NEW/Type explosive – 17 lbs / (multimode) EFP and blast frag Interface MMSI (Miniature Munitions Stores Interface) Guidance Midcourse INS/GPS, wide area search and terminal LADAR with datalink Time of Flight - up to 30-120 min (configurations noted above) range dependent on standoff requirements and required search area. Links (TBD) possibly Airborne Network with Smart Munitions Network. Carriage Options: Aircraft: B-1B B-2A B-52H F-22A F-35 (Internal storage) C-17 C-130 MQ-1 MQ-9

Launcher/rack: Tactical outer mold line implementation with 4 Per BRU-61 rack (tactical WASM fits SDB dimensions volume)

13-24

FOUO

Contractor / Status / Improvements / Special Equipment: Contractor - Lockheed Martin Missiles and Fire Control- Dallas Status - ATD successfully completed December 2005. ATD demonstrated LADAR, ATR, Turbojet Engine, and Multimode Warhead. Further USAF Development -TBD (note: USAARMDEC currently leveraging PLOCAAS ATD developed LADAR and small turbojet technology in the Non Line of Site Loitering Attack Missile (NLOS-LAM) program). That program has also been suspended and future of this technology is uncertain at the present time. ATD investigated mission planning, operator command and control interface, development cost, and promoted development of MMSI standard. Management/Engineering: AFRL/RWOB/RWAV, Eglin AFB, FL Technical Order: N/A

Figure 1 ATD Tactical Configuration (6 ft long)

Figure 2 Flight Test Configuration (3 ft long)

13-25

FOUO

INTENTIONALLY LEFT BLANK

13-26

FOUO

CHAPTER FOURTEEN 1 June 2009

PERSONAL WEAPONS INDIVIDUAL WEAPONS CREW SERVED WEAPONS MISSION SPECIFIC WEAPONS

FOR OFFICIAL USE ONLY

14-0

FOUO

INTENTIONALLY LEFT BLANK

Nomenclature: M9

PERSONAL WEAPONS Name: 9mm Pistol (Personal Defense Weapon (PDW))

Capability: Provides a self defense capability to AF personnel. Description: The M9 is a 9mm pistol which replaced the M1911A1 .45 cal pistol and .38 cal M15 revolvers (that were the general issue handguns for Air Force (AF) personnel). The M9 is a semiautomatic, double-action pistol that is lighter, and safer than the M1911A1 pistol. The weapon is carried by service members who are not issued rifles and by others who have a personal defense requirement.

Characteristics: Caliber: Ammunition: Weight: Range: Magazine Capacity: Length: Width: Height: Barrel length: Bore diameter: Muzzle velocity:

9mm M882 Ball 2.6 lbs (loaded) 50 meters 15 rounds 8.54 inches (21.69 centimeters) 1.50 inches (3.81 centimeters) 5.51 inches (14 centimeters) 4.92 inches (12.5 centimeters) 9mm (approximately .355 inches) 1,200 feet (365 meters) per second

Management: 575 CBSS/GBLC, Robins AFB, GA Technical Order: 11W3-3-5-1 and 11W3-3-5-4

14-1

FOUO

Nomenclature: M11

Name: 9mm Compact Pistol

Capability: Provides a self defense capability to AF personnel. Description: The M11 is a 9mm semiautomatic, double-action, compact pistol issued to OSI agents. It replaced the M9 pistols the OSI agents used to carry.

Characteristics: Caliber: Ammunition: Weight: Range: Magazine Capacity:

9mm NATO M882 Ball 1.8 lbs (loaded) 50 meters 13 rounds

Management: 575 CBSS/GBLC, Robins AFB, GA Technical Order: 11W3-3-4-11 and 11W3-3-4-12

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INDIVIDUAL WEAPONS Nomenclature: M16/M16A2 Name: 5.56mm Rifle Capability: Destroy moving and stationary light materiel targets and neutralize identified traditional and nontraditional combatants. Description: The M16A2 rifle is an improved version of the M16 rifle and is being issued to AF personnel as the primary combat rifle. The M16A2 rifle is a lightweight 5.56mm, air-cooled, gas-operated, magazine-fed, selective fire, shoulder- or hip-fired weapon designed for either automatic fire (3round bursts) or semiautomatic fire (single shot) through the use of a selector lever. They incorporate improvements in sight, pistol grip, stock and overall combat effectiveness. Accuracy is improved by incorporating an improved muzzle compensator, three-round burst control, a heavier barrel with a tighter twist ratio to accommodate the new heavier NATO standard ammunition.

M16 Characteristics: Caliber: Length: Weight: Ammunition:

M16A2

5.56mm 39.63 inches 8.9 lbs (loaded) M855 Ball, M856 Tracer, XM995 AP, XM996 Dim Tracer Range: 550 meters Type of fire: Semi-Auto, 3-rd burst (A2), Full Auto (M16) Magazine Capacity: 30 rounds Maximum range: 3,600 meters Maximum effective range: Area target: 2,624.8 feet (800 meters) Point target: 1,804.5 feet (550 meters) Muzzle velocity: 2,800 feet (853 meters) per second Rate of fire: Cyclic: 800 rounds per minute Sustained: 12-15 rounds per minute Semiautomatic: 45 rounds per minute Burst: 90 rounds per minute Management: 575 CBSS/GBLC, Robins AFB, GA Technical Order: M16 - 11W3-5-5-24 and 11W3-5-5-61 M16A2 - 11W3-5-5-41 and 11W3-5-5-42

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Nomenclature: M4/M4A1

Name: 5.56mm Carbine

Capability: Destroy moving and stationary light materiel targets and neutralize identified traditional and nontraditional combatants. Description: The M4 Carbine is a 5.56mm, gas operated, air cooled, magazine fed, selective fire, shoulder fired weapon with a telescoping stock. The M4 has selective fire options including semiautomatic and three-round burst (like the M16A2), while the M4A1 has a "full auto" option in place of the three-round burst. The M4 Carbine will replace selected M16A2 Rifles where a shorter, lighter, more portable weapon is needed. The M4 is used by the AF Security Forces while the M4A1 is unique to HQ AFSOC elements.

M4 without Optic

M4 with Optic M4A1 with Carrying Handle Characteristics: Caliber: 5.56mm Ammunition: M193 Ball, M196 Tracer, M200 Blank, M855 Ball, M856 Tracer, XM995 AP, XM996 Dim Tracer Weight: 6.7 lbs (loaded) Type of fire: Semi-Auto, 3-rd burst or Full-Auto (M4A1) Magazine Capacity: 30 rounds Maximum range: 3,600 meters Maximum effective range: Area target: 2,165.4 feet (600 meters) Point target: 1,804.5 feet (500 meters) Muzzle velocity: 2,800 feet (853 meters) per second Rate of fire: Cyclic: 800 rounds per minute Sustained: 12-15 rounds per minute Semiautomatic: 45 rounds per minute Burst: 90 rounds per minute Management: 575 CBSS/GBLC, Robins AFB, GA Technical Order: 1W3-5-5-41 and 11W3-5-5-42

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Nomenclature: MK-14 Mod 0

Name: 7.62mm Enhanced Battle Rifle (EBR)

Capability: Destroy moving and stationary light materiel targets and neutralize identified traditional and nontraditional combatants. Description: The 7.62mm MK-14 MOD 0 EBR will be used by the operator to engage and destroy enemy personnel at any range out to 600 yards for point targets and 1,000 yards for area targets. The 7.62mm MK-14 MOD 0 EBR deliberately capitalizes on prior shooting and maintenance skills of individuals trained and proficient with M14 type rifles, but provides an inherently more robust and precision arm. A complete kit of accessories is provided for sustained deployment in remote areas. A variety of capabilities may be obtained by the combination of basic issue items and auxiliary items that can be tailored for a variety of tactical applications. These range from actions conducted by local and federal level law enforcement agencies, to the most severe operational environments which Forward Deployed and Special Operations Forces may encounter.

Characteristics: Caliber: 7.62mm Ammunition: M80, M118LR Weight: No magazine, iron sights Empty Magazine, sling vertical grip Type of fire: Magazine Capacity: Maximum range: Maximum effective range: Muzzle velocity: M-80 M118LR

11.0 lbs . 12.4 lbs. Semi-Auto 20 rounds 600 yards Area target: 1000 yards Point target: 600yards 2675 fps 2511 fps

Management: 575 CBSS/GBLC, Robins AFB, GA Technical Order: 11W3-5-4-61

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Nomenclature: M-32

Name: 40mm Multiple Grenade Launcher (MGL)

Capability: Destroy moving and stationary light materiel targets and neutralize identified traditional and nontraditional combatants. Description: The M-32 40mm Multiple Grenade Launcher (MGL) or Multiple-shot Grenade Launcher (MSGL) is a modified Milkor MGL-140 with additional features like the buttstock, sights, and foregrip. The M-32 six-shot 40mm grenade launcher can put all 6 rounds on target in under 3 seconds, and can fire "normal" M433 40mm grenades or specialty rounds. The M32 is equipped with a MIL-STD-1913 quad rail system on the foregrip to accommodate current issue weapon accessories such as grips, laser illuminators/designators, and flashlights, as well as a collapsible butt stock. Sighting is accomplished through a parallax free electro-optical night vision compatible holographic sight that can be adjusted to compensate for long range shooting. This weapon is currently used only by the Marines. NOTE: M203 ammo and MK 19 ammo are not interchangeable; the MK 19 ammo has 3-4 times as much propellant charge as the M203 ammo. If you fire the MK 19 ammo in the M203 the round will explode in the chamber. Characteristics: Weight: Total (including 6 rounds) Maximum effective range: Area target: Point target: Max range: Minimum safe range: Training: Combat:

13 lbs. 16.5 pounds 400 meters 150 meters 400 meters 130 meters 31 meters

Management: Technical Order:

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Nomenclature: M203, A1, and A2

Name: 40mm Grenade Launcher

Capability: Destroy moving and stationary light materiel targets and neutralize identified traditional and nontraditional combatants. Description: The M203 Grenade Launcher is a breech loading, pump-action, single shot manually operated, capable of firing a variety of 40mm ammunition. Engaging targets out to 400 meters, it has a leaf sight and a quadrant sight. The M203 is mounted on the M16A2. The M203A1 is the version that is a permanent mount to the M4 Carbine. The M203A2 is the version that is a quick mount/dismount for the M4 carbine. The grenade launcher is comprised of the following: barrel, receiver, hand guard, leaf sight and quadrant sight. NOTE: M203 ammo and MK 19 ammo are not interchangeable; the MK 19 ammo has 3-4 times as much propellant charge and the case is 9mm longer than the M203 ammo. If you fire the MK 19 ammo in the M203 the round will explode in the chamber.

Characteristics: Weight:

Launcher: 3.0 lbs Rifle (M16A2): 8.79 pounds Total (including 30 rounds): 11.79 pounds Barrel Length: 12 inches Maximum effective range: Area target: 1,148.35 feet (350 meters) Point target: 492.15 feet (150 meters) Max range: 1,312.4 feet (400 meters) Minimum safe range: Training: 541.2 feet (165 meters) Combat: 101.71 feet (31 meters) Management: 575 CBSS/GBLC, Robins AFB, GA U.S. Army ARDEC, Picatinny Arsenal, NJ Technical Order: 11W3-9-4-1 and 11W3-9-4-2

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Nomenclature: XM320

Name: 40mm Grenade Launcher Module (GLM)

Capability: Destroy moving and stationary light materiel targets and neutralize identified traditional and nontraditional combatants. Description: The XM320 will provide a common grenade launcher that can be used on current (M16A2 and M-4) and future platforms through the use of various mounting adapters. It has five main system components: Side-opening add-on 40X46mm launcher, various optional sighting devices including day/night/ranging sighting system, detachable multi-position retractable buttstock, carrying sling for stand-alone use and field cleaning kit. The XM320 insures improved first round hit probability by providing accurate range-to-target data and 5 meter aiming increments to engage and defeat enemy targets with the first round.

Production Configuration

BLM with day/night/ranging with sighting system attached

Characteristics: Weight:

4.02 lb (stand alone unit with stock_ 3.39 lb (mounted on M4) 3.98 lb (mounted on M16A2) Barrel Length: 8.47 in. Over all Length: 11.81 in. (w/0 stock) Height : 8.07 in (w/o stock) 17.71 in. (with stock in) 3.5 (with stock in) 20.1 in. (with stock our) Trigger Pull: Double-action Maximum effective range: Minimum safe range: Area target: 1,148.35 feet (350 meters) Training: 426.53 feet (130 meters) Point target: 492.15 feet (150 meters) Combat: 101.71 feet (31 meters) Max range: 1,312.4 feet (400 meters) Management: U.S. Army ARDEC, Picatinny Arsenal, NJ Technical Order: TBP

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Nomenclature: M249

Name: 5.56mm Automatic Rifle (AR)

Capability: Destroy moving and stationary light materiel targets and neutralize identified traditional and nontraditional combatants. Description: The M249 AR is a 5.56mm lightweight, one-man-portable automatic rifle capable of delivering a large volume of effective fire to support squad operations. It is belt-fed, gas-operated, air-cooled, and fires from the open bolt position. The maximum range for a point target is 600 meters while 800 meters is the distance for area targets. It also has a 30-round magazine feeding capability for emergency firing procedures. It can be fired from the shoulder hand-held position or the bipod position. It has two barrel assemblies to extend the life of the barrels, retain accuracy and allow for continuous firing over long periods of time. It can be fed from a 200 round box via linked ammo, or from normal 30 round M-16 magazines. The box fits on the bottom of the receiver and feeds from the side. The magazine also feeds into the side.

Characteristics: Caliber: Ammunition: Weight: Length: Rate: Range:

Capacity:

5.56mm M193 Ball, M196 Tracer, M200 Blank, M855 Ball, M856 Tracer, XM995 AP, XM996 Dim Tracer 23.9 lbs (loaded) 40.87 inches 850 rds/min 600 meters (point) 800 meters (area) 1,000 meters (suppression) 200 rounds

Management: 575 CBSS/GBLC, Robins AFB, GA Technical Order: 11W3-5-5-51 and 11W3-5-5-52

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CREW SERVED WEAPONS Nomenclature: M240B Name: 7.62mm Machine Gun (MG) Capability: Destroy moving and stationary light materiel targets and neutralize identified traditional and nontraditional combatants. Description: The M240B is a 7.62mm medium machine gun and is the improved ground mounted version of the original M240 machine gun, which is utilized on tanks and light armored vehicles. It is beltfed, gas-operated, air-cooled, and fires from the open bolt position. The weapon feeds from the left, ejecting links to the right and spent cartridge underneath the receiver. The M240B is modified for ground use by the installation of an “Infantry Modification Kit.” comprised of a flash suppressor, front sight, buttstock, pistol grip, bipod, rear sight assembly, feed tray cover with a M1913 rail that allows the use of rail mounted accessories, protective heat shield for the barrel, and a carrying handle for the barrel. It has two barrel assemblies to extend the life of the barrels, retain accuracy and allow for continuous firing over long periods of time.

Characteristics: Caliber: Ammunition: Weight: Length: Maximum Range: Maximum Effective Range: Maximum Grazing Fire: Maximum Tracer Burnout: Rates of Fire:

7.62mm Same as M60 MG 27.6 lbs 47.5 inches 3,725 meters 1,100 meters 600 meters 900 meters Sustained -100 rds/min Rapid - 200 rds/min

Management: 575 CBSS/GBLC, Robins AFB, GA Technical Order: 11W2-6-5-1 and 11W2-6-5-2

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Nomenclature: MK 19

Name: 40mm Grenade Machine Gun (GMG)

Capability: Destroy moving and stationary light materiel targets and neutralize identified traditional and nontraditional combatants. Description: The MK 19 40mm GMG is designed to deliver accurate, intense, and decisive firepower against enemy personnel and lightly armored vehicles to a maximum effective range of 1,600 meters against point targets and 2,057 meters against area targets. It is used in offensive and defensive operations in the main battle area. The MK 19 can be tripod or vehicle mounted. The MK 19 is an air-cooled, disintegrating metallic link-belt fed, blowback operated, fully automatic weapon and is crew transportable over short distances with limited amounts of ammunition. It can fire a variety of 40mm grenades. The M430 High Explosive Dual Purpose (HEDP) 40mm grenade will pierce armor up to 2 inches thick, and will produce fragments to kill personnel within 5 meters and wound personnel within 15 meters of the point of impact. Associated components are: MK 64 Cradle Mount, MOD 5; M3 Tripod Mount; and the AN/TVS5 Night Vision Sight. NOTE: M203 ammo and MK 19 ammo are not interchangeable; the MK 19 ammo has 3-4 times as much propellant charge as the M203 ammo. If you fire the MK 19 in the M203 the round will explode in the chamber.

Characteristics: Caliber: Ammunition: Weight: Length: Range: Rate of fire:

Muzzle velocity:

40mm M383 HE, M384 HE, M430 HE, M430A1 HE 76.5 lbs 43.1 inches 1,500m (point tgt) 2,200m (area tgt) Cyclic: 325-375 rounds per minute Rapid: 60 rounds per minute Sustained: 40 rounds per minute 790 feet (240.69 meters) per second

Management: 575 CBSS/GBLC, Robins AFB, GA Technical Order: 11W2-5-16-1 and 11W2-5-16-2

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Nomenclature: M2

Name: Cal .50 Machine Gun (MG)

Capability: Destroy moving and stationary light materiel targets and neutralize identified traditional and nontraditional combatants. Description: The M2 Browning Caliber .50 Heavy Barrel MG is a belt-fed, recoil-operated, air-cooled, crew-operated MG. The MG provides a heavy volume of close, accurate, and continuous fire necessary to form an integral part of the unit's defensive fires.

Characteristics: Caliber: Ammunition:

.50 M1/M1A1 Blank, M8 API, M17 Tracer, M20 APIT, M33 Ball, MK211, M903 SLAP, M962 SLAP- T Weight: 84 lbs (unloaded) M3 Tripod (Complete): 44 pounds Total: 128 pounds Length: 61.42 inches Maximum range: 4.22 miles (6.8 kilometers) Maximum effective range: 2,000 meters with tripod mount Maximum effective range: 1,830 meters Rate of fire: Cyclic - 450-550 RPM Management: 575 CBSS/GBLC, Robins AFB, GA Technical Order: 11W2-6-3-172 and 11W2-6-3-184 11W2-6-6-1

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MISSION SPECIFIC WEAPONS Nomenclature: Shotguns Name: 12 gauge Shotguns Capability: Destroy moving and stationary light materiel targets and neutralize identified traditional and nontraditional combatants. They can also be used to breech locked doors. Description: There are four basic 12 gauge shotguns used by AF personnel: Winchester M1200, Remington M870, Remington Modular Combat Shotgun (MCS), and Mossberg M500. They are manually operated, repeating shotgun of the slide action, hammerless, and take down type with 18 to 20 inch barrels. They have a minimum capacity of five rounds. Security Forces personnel are the primary users of these shotguns.

Mossberg 12 ga

Remington 12 ga

Remington MCS 12 ga

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Winchester 12 ga Characteristics: Caliber: Ammunition: Weight: Range:

12 gauge #OO Buckshot, #7 1/2 Shot, #9 Shot 7 lbs 50 meters

Management: 575 CBSS/GBLC, Robins AFB, GA Technical Order: 11W3-6-1-114 and 11W3-6-1-154 and 11W3-6-1-171 11W3-6-2

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Nomenclature: M24

Name: 7.62mm Sniper Weapon System Rifle (USA)

Capability: Provides precision long-range offensive/defensive capability to neutralize identified traditional and nontraditional combatants. Description: The M24 Sniper Weapons System (SWS) rifle is a 7.62mm bolt action, 6 shot, repeating rifle. The system consists of the rifle, day optic sight, metallic (iron) sights, bipod, deployment kit, cleaning kit, soft rifle carrying case, optic case, and system case. Match quality ammunition works best in the M24; however, it can fire standard ammunition.

Characteristics: Caliber: 7.62 mm NATO Ammunition: M118 Match Weight: 12.1 lbs (loaded) Length: 44.14 inches (112.12 centimeters) Length of Barrel: 22 inches (55.88 centimeters) Range: 800 meters Magazine Capacity: 5 rounds Muzzle velocity: 2,800 feet (853 meters) per second Management: 575 CBSS/GBLC, Robins AFB, GA Technical Order: 11W3-5-4-10-1

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Nomenclature: M107

Name: Cal .50 Special Application Sniper Rifle (SASR)

Capability: Provides precision long-range offensive/defensive capability to neutralize identified traditional and nontraditional combatants. It is utilized by Explosive Ordnance Disposal to render safe unexploded ordnance. Description: The M107 .50-caliber SASR is a bolt-action, rapid-fire; man portable, shoulder-fired, recoil operated, semi-automatic magazine fed special application rifle utilizing military standard .50 caliber ammunition. The system consists of the rifle, a variable 10 power day optic sight, a backup iron sight, detachable 10 round magazine, transport case, tactical soft case, cleaning /maintenance equipment, detachable sling, adjustable bi-pod, manuals, and a muzzle brake to reduce recoil. This weapon is primarily employed against high value materiel targets, and is used by the Explosive Ordnance Disposal teams to detonate unexploded ordnance. Air Force Security Forces, Explosive Ordnance Detachment (EOD) and Pararescue personnel utilize this rifle. Match quality ammunition works best in this weapon, however, it can fire standard ammunition.

Characteristics: Caliber: Ammunition: Weight: Length: Barrel length: Muzzle velocity: Range: Magazine Capacity:

.50 Mk211 Multi Purpose 28.4 lbs 57 inches (144.78 centimeters) 29 inches (73.67 cm) 2,800 feet (854 meters) per second 1,800 meters 10 round detachable box magazine

Management: 575 CBSS/GBLC, Robins AFB, GA Technical Order: 11W2-5-7-1 and 11W2-5-7-2 11W3-5-1-111

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Nomenclature: M110

Name: 7.62mm Semi-Automatic Sniper System (SASS)

Capability: Provides precision long-range offensive/defensive capability to neutralize identified traditional and nontraditional combatants. Description: In 2007 the Army deployed the M110 Semi-Automatic Sniper System (SASS) to Afghanistan, in the first combat deployment of the new weapon. The rifle has several new features, the most prominent being an improved rate of fire. The automatic firing capabilities of the SASS will decrease lag time in between shots. The rifle has an improved flash suppressor which significantly reduces blast signature and eliminates the small cloud of dust that rises off the ground from the gases emitted through the barrel, thus making locating snipers in the field, even after they have fired a shot, difficult for the enemy. The buttstock is fixed, however the buttplate is adjustable for length of pull to match the user’s hand side of the stock. The adjustment can be made without tools via a notched hand-tightened knob on the fight-hand side of the stock. The rifle has ambidextrous features such as a double sided magazine release, safety selector switch, and bolt catch. It is manufactured by Knight's Armament Company (KAC). Refinements instituted by KAC maximize parts commonality with the AR15 / M16, improve weapon reliability, and increase accuracy. The M110 is used by only the Army. Characteristics: Caliber: Ammunition: Weight: Length: Length of Barrel: Effective Range: Muzzle velocity: Action: Rate of Fire Feed system:

7.62 mm NATO 7.62 x 51mm NATO 15.3 lbs. total (including scope, bipod, and loaded 20 round magazines 40.5 inches (1,029 mm) (buttstock fully compressed) 46.5 inches (1,181 mm) (buttstock fully extended) 20 inches (508 mm) 1000 meters 2,571 feet (783 meters) per second Gas-operated, rotating bolt Semi-automatic 10 or 20 round detachable box magazine

Management: Technical Order:

M110 Semi-Automatic Sniper System (SASS)

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Nomenclature: M40A3

Name: 7.62mm Sniper Rifle

Capability: Provides precision long-range offensive/defensive capability to neutralize identified traditional and nontraditional combatants. Description: The M40A3 is a bolt-action sniper rifle used by the United States Marine Corps. It has had three variants: the M40, the M40A1 and the M40A3. The M40 was introduced in 1966. The changeover to the A1 model was completed in the 1970s, and the A3 in the 2000s. Each firearm begins life as a Remington 700, and is then extensively modified by hand by USMC 2112/gunsmiths at Marine Corps Base Quantico, using components from a number of suppliers. New M40A3s are being built, and A1s are upgraded to A3s as they rotate into the armory for service and repair. The rifles have had many sub-variations in telescopic sights, and smaller user modifications. Characteristics: Caliber: Ammunition: Weight: Length: Length of Barrel: Max Effective Range: Max Range: Muzzle velocity: Action: Feed system: Sights: Stock:

7.62 mm (308win) 7.62 x 51mm NATO 16.54 lbs. (total); 14.44 lbs. (rifle w/5 rounds); 2.2 lbs. (scope) 44.25 inches (1,124 mm) 24 inches (610) (1:12 right hand twist) 1000 yards 5,000 yards 2,670 feet per second with M117 LR Bolt Action 5 round detachable box magazine Unertl 10X telescopic sight with Mil-Dots and BDC (specially designed for USMC, 12.5 in. long, windage adjustable .5 degree increments) Fiberglass

Management: Technical Order:

M40A3 Sniper Rifle (USMC)

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CHAPTER FIFTEEN 1 June 2009

SMALL ARMS/GUN MUNITIONS

FOR OFFICIAL USE ONLY

INTENTIONALLY LEFT BLANK

Nomenclature: 5.56mm

Name: Ammo

Capability: Destroy moving and stationary light materiel targets and neutralize identified traditional and nontraditional combatants. Description: The 5.56mm (0.223 inch) ammunition is typically fired from the M16 series rifle, M4 series carbine, and the M249 Squad Automatic Weapon (SAW). This ammunition can be deployed as individual rounds, within 10 or 30-round magazines, or linked by M27 links for firing from an ammunition box. The following are 5.56mm cartridges used by the Air Force: M193 Ball Cartridge has a 56 grain, gilding metal-jacketed bullet with a lead antimony core. It is identified by a non-painted tip. Performs best when fired in 1 in 12” barrel twist guns (M249), but can be used in 1 in 7” barrel twist with reduced range. DODIC A071 M196 Tracer Cartridge has a 54 grain bullet without a steel penetrator and is identifiable by a painted red tip. Used for observation, incendiary effect, and signaling. Like the M193, works best in a 1 in 12” twist barrel. DODIC A068 M199 Dummy Cartridge can be identified by the six grooves along the side of the case beginning about one-half inch from its head. It contains no propellant or primer. The primer well is open to prevent damage to the firing pin. The dummy round is used during mechanical training, dry-fire exercises, and function checks. DODIC A060 M200 Blank Cartridge has no projectile but is used during training to simulate live ammunition noises and flash. It is identifiable by a rose petal crimp. DODICs A075, A080 M855 Ball Cartridge has a 62 grain gilding, metal-jacketed, lead antimony core bullet with a steel penetrator. It is identifiable by a green tip. The steel penetrator increases its helmetpenetration range substantially more than the M193 round. This is the NATO standard round. It is optimized to shoot in a 1 in 7” twist barrel. It is effective against personnel and light materials. DODICs A059, A062, A064 M856 Tracer Cartridge has a 63 grain bullet with a lead antimony slug. It is identified by an orange tip. The tracer is used for adjustments after observation, incendiary effects, and signaling. This tracer round has a longer tracer column and an improved pyrotechnic mixture, which results in an increased daylight trace range compared to the 5.56mm M196 tracer round. When tracer rounds are fired, they are usually mixed with ball ammunition in a ratio of four ball (or armor piercing) rounds to one tracer round. DODICs A063, A064, AA02 M862 Short Range Training Ammunition (SRTA) provides a restricted range training alternative to M193/M855 service rounds. The 5.56mm SRTA has a maximum range of 250 meters; an effective range of 25 meters (trajectory match and round to round dispersion comparable to the service ammunition); and provides a functional capability when used in the M16A2 Rifle with the M2 Training Bolt. DODIC A065 M995 Armor Piercing (AP) Cartridge is a 5.56mm Armor Piercing (AP) cartridge that provides an increased AP capability over the M855 ball round. DODICs AA01, AA02

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Frangible Cartridge (Reduced Ricochet Limited Penetration (RRLP)) is a round used for training only. This round features a lead-free bullet and nylon composite filler, with or without a partial copper jacket; a lead-free powder, and lead-free primer; making it a 100% non-toxic round. The bullet is meant to break up on impact - eliminating ricochet and penetration hazards. DODICs AA40, AA85 Mk 262 Special Ball Cartridge is for AFSOC use only. It features a 77-grain Sierra MatchKing bullet. It is a long range round and enables engagements out to 600 meters (800 possible depending on conditions). It greatly enhances the capability of the M16 or M4A1 Carbine. DODIC AA53 Typical Characteristics: Height: Weight: Muzzle Velocity:

2.26 inches 180 grains 3,000+ fps

Weapons: M16A1, M16A2, M4, M4A1, M249 Management: 506 CBSS/GBLB, Hill AFB, UT Technical Orders: 11A13-10-7

M995 5.56mm Armor Piercing Cartridge

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Nomenclature: 7.62mm

Name: Ammo

Capability: Destroy moving and stationary light vehicles and materiel targets and neutralize identified traditional and nontraditional combatants. Description: The 7.62mm (0.30 inch) ammunition is used in the M14, M24 rifles, M110, M40A3, the M240 (B&D) machine guns, and the GAU-2B/A mini gun. This ammunition can be deployed as individual rounds, within five round clips, or linked by the M13 disintegrating metallic splitlinked belt for firing from an ammunition box. The rounds used by the USAF are as follows: M62 Tracer Cartridge is identified by an orange tip; the tracer is used for adjustments after observation, incendiary effects, and signaling. It has a 142 grain bullet. The tracer is typically linked in a mix with other rounds - usually four ball (or armor piercing) rounds to each tracer. It can also be found in a nine to one mix. DODICs A140, A146, A151, A165, A168, AA04 M80 Ball Cartridge has a 145 grain lead antimony filled bullet covered by a gliding copper jacket. Bullet is unpainted for identification. DODICs A131, A143, A151, A164, A165, A168, A257 M82 Blank Cartridge is used during field training. It provides the muzzle blast and flash that can be detected by trainers during exercises. DODICs A111, A112 M118 Special Ball Cartridge is used in sniper weapons and is a long range high accuracy bullet. It consists of a 173 grain bullet with a gilding metal jacket and a lead antimony slug. The tip of the bullet is not colored. Its spread for a 10-shot group is no more than 7 inches at 600 yards. DODICs A136, AA11 M172 Dummy Cartridge is identified by six flutes in the side of the casing. It contains no propellant or primer. The primer well is open to prevent damage to the firing pin. The dummy round is used during mechanical training, dry-fire exercises, and function checks. DODIC A159 M276 Dim Tracer Cartridge provides the user community with a tracer cartridge which is visible only when viewed through night vision devices and does not cause visual interference to the wearer. It has a 140 grain full jacketed bullet with a lead slug and tracer filler. It is identified by a purple tip. The tracer is typically linked in a mix with other rounds - usually 4 ball (or armor piercing) rounds to each tracer. It can also be found in a 9 to 1 mix. DODIC A257 M993 Armor Piercing (AP) Cartridge is an AP cartridge which provides an AP capability for the M60 machine gun and the M24 sniper rifle. It is identified by a black tip. DODICs AA03, AA04 Typical Characteristics: Height: Weight: Muzzle Velocity:

2.80 inches 350 grains 2,750+ fps

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Weapon: GAU-2 Mini-Gun, M240 Machine Gun, M14 rifle, and M24 Sniper Rifle Platforms: MH-53, MH-60G, HH-60 (GAU-2), and HMMWV Management: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A13-10-7

M276 7.62mm Dim Tracer Cartridge

M993 7.62mm Armor Piercing Cartridge

M62

M80

M993

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Nomenclature: 9mm

Name: Ammo

Capability: Neutralize moving and stationary traditional and nontraditional combatants. Description: The 9mm (0.354 inch) ammunition is typically used in the M9 and M11 hand guns. The 9mm is intended for use against personnel. This ammunition is deployed as individual rounds and loaded in 15 or 12 round clips. The rounds used by the USAF are as follows: M882 NATO Ball is the standard 9mm round. It has a 124 grain bullet with a full metal jacket, filled with a lead antimony slug. The tip is not painted. DODIC A363 M917 Dummy Cartridge is an inert round used for mechanical training, dry-fire exercises, and function checks. DODIC A359 9MM Hollow Point is used only as a Law Enforcement round. It cannot be used for combat. It has a partial metal jacket, with a lead antimony slug. DODIC A260 9MM Frangible Ball is a target/practice round only. This round features a lead-free bullet with a partial copper jacket and nylon composite filler; a lead-free powder, and lead-free primer; making it a 100% non-toxic round. The bullet is meant to break up on impacteliminating ricochet and penetration hazards. DODIC AA16 Typical Characteristics: Height: Weight: Muzzle Velocity:

1.165 inches 179 grains 1,250+ fps

Weapon: M9 and M11 Hand Guns Management: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A13-10-7

M882

Hollow Point Bullet

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Nomenclature: Caliber .50

Name: Ammo

Capability: Destroy moving and stationary lightly armored vehicles and materiel and neutralize identified traditional and nontraditional combatants. Description: The caliber .50 round is used in the GAU-18/A and M2 machine guns and the M82A1/M82A1A/M107 sniper rifles. The round can be deployed as individual rounds or linked with M9 links to be belt-fed into the machine guns. The following are caliber .50 rounds used by the Air Force: M1 Blank is for simulated fire. It provides a sound and muzzle flash. DODIC A559 M1A1 Blank is also for simulated fire. It is distinguished from the M1 by its rosette crimped cartridge case. It also uses a different propellant than the M1. DODIC A598 M1 Incendiary Cartridge has a 633 grain projectile that bursts into a high temperature flame that ignites any flammable material when it impacts the target. It has a blue painted bullet tip. DODIC A564 M2 Armor Piercing Cartridge is used against armored aircraft and lightly armored vehicles, concrete shelters, and other bullet-resisting targets. It has a 660 grain bullet with a hardened manganese and steel core. It is identified by a black painted tip. DODICs A525, A527, A530 M2 Dummy is for mechanical training, dry-fire exercises, and function checks and is completely inert. Three holes are drilled into the case and there is an absence of a primer. DODIC A560 M8 Armor Piercing Incendiary (API) has a 660 grain projectile that has a combined armorpiercing and incendiary effect for use against flammable, lightly or unarmored targets. It is identified by an aluminum painted tip. DODICs A545, A576 M17 Tracer has a brown bullet tip and produces a red trace. It is used against unarmored targets. DODICs A557, A571 M20 Armor Piercing Incendiary Tracer (APIT) has a red bullet tip with an aluminum color annulus. Its 619 grain bullet with a hardened steel core and combined incendiary effect are used against armored aircraft and lightly armored vehicles, concrete shelters, and other bulletresisting targets - with the additional tracer feature. The tracer is typically linked in a mix with other rounds - usually 4 ball (or API) rounds to each tracer. It can also be found in a 9 to 1 mix. DODICs A576, A585 M33 Ball Cartridge has a 660 grain bullet with a soft steel core. It is used for marksmanship training and against light materiel targets. It is identified by an unpainted bullet tip. DODICs A555, A557

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MK211 Armor Piercing Incendiary (API) has a green bullet tip with an aluminum color annulus. This 668 grain bullet is designed for use in the sniper rifle. It provides similar effect as the M8 round, only with a harder tungsten core. DODIC A606 MK257 Armor Piercing Incendiary Dim Tracer is identified by a lavender bullet tip with a gray annulus. It provides similar effect as other API rounds but with the added benefit of the dim tracer which is visible only with night vision devices - which reduces the possibility of locating the weapon during firing. The tracer is typically linked in a mix with other rounds - usually 4 ball (or API) rounds to each tracer. It can also be found in a 9 to 1 mix. DODIC AA50 MK263 Armor Piercing Cartridge has a black tip and is meant for use against lightly armored targets. The bullet is a COTS item. DODIC AA58 T249E2 Target Practice Round is for target practice only. Its composite bullet produces a puff of smoke on impact with a steel surface. For use only the M8C spotting rifle as it is a full inch shorter than standard caliber 50 rounds. It is identified by a green tip. Typical Characteristics: Height: Weight: Muzzle Velocity:

5.45 inches 1,750 grains 2,910 fps

Weapon: M2, GAU-18 Machine Gun, GAU-19/A Gatling Gun and M82A1/M82A1A/M107 Sniper Rifles Platforms: MH-60G, MH-53, HH-60, HMMWV Management: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A13-10-7

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Nomenclature: 12 Gauge Cartridges

Name: Ammo

Capability: The 12-gauge shotgun is usable by military forces in protection of key facilities, security, or crowd control. It enables field commanders and soldiers to have lethal and effective non-lethal capability, increasing flexibility in the application of force during military operations. Description: The 12-guage shot/shells are deployed individually. The following are the shot/shells in use by the Air Force, both lethal and non-lethal: #00 Buckshot has nine lead pellets of 0.33 inches in diameter. This round is used for convoy protection and door breaching. DODIC A011 #00 Frangible is a training round that features 9 pellets of nylon composite; a lead-free powder, and lead-free primer; making it a 100% non-toxic round. The round is meant to break up on impact - eliminating ricochet and penetration hazards. DODIC AA82 #7 ½ Birdshot is an EOD round used in their bomb-disposing robot. DODIC A014 Non-Lethal Bird Scare is a round used to scare birds away from runways. It produces a loud bang and flash. DODIC AY04 Dummy Cartridge is used for mechanical training, dry-fire exercises, and function checks and is completely inert. DODIC AA55 Non-Lethal Bean Bag is a non-lethal round that fires a single two inch square 620 grain bean bag meant to provide enough impact to stun an individual. Effective range of 10 to 30 yards, beyond 30 yards, the projectile loses accuracy and may no longer have the velocity required to stun. DODIC AA29 M1012 Non-Lethal Point Target Cartridge Round stuns an individual by delivering a strong blow to the body without penetrating using a single rubber projectile. Effective range of 10 to 30 yards, beyond 30 yards; the projectile loses accuracy and may no longer have sufficient velocity to stun. DODIC AA51 M1013 Non-Lethal Crowd Dispersal Round is for use against two or three individuals and stuns them without penetrating the skin using many small rubber projectiles. The effective range is 10 to 30 yards and beyond 30 yards the round loses effectiveness. DODIC AA52 Typical Characteristics: Height: Weight: Muzzle Velocity:

2.75 inches Varied 250 to 1,550 fps depending on lethality

Weapon: Remington 12 Gauge Shotguns

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Management: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A13-10-7

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INTENTIONALLY LEFT BLANK

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CHAPTER SIXTEEN 1 June 2009

GROUND DEFENSE MUNITIONS

FOR OFFICIAL USE ONLY

INTENTIONALLY LEFT BLANK

Hand Grenades Nomenclature: MK1A1

Name: Training Hand Grenade

Capability: Training hand grenade. Description: The MK1A1 training grenade simulates the MK2 “Pineapple” hand grenade. The grenade is inert and is used only for training in handling and throwing. DODIC G965

Characteristics: Height: Weight: Color/Markings: Range: Casualty Radius: Fuze: Fuze Type: Filler:

4.5 inches 21 ounces Painted Black, Green, or Blue Average soldier can throw the grenade 30 yards None Inert version of M204A2 None Inert

Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A8-5-7

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Nomenclature: MK3A2

Name: Concussion Offensive Hand Grenade

Capability: Suppress/incapacitate traditional and nontraditional combatants and damage light materiel targets during close combat while minimizing danger to friendly personnel. Description: The MK3A2 offensive hand grenade, commonly referred to as the concussion grenade, is designed to produce casualties during close combat while minimizing danger to friendly personnel. The grenade is also used for concussion effects in enclosed areas, for blasting, or for demolition tasks. The shock waves (overpressure) produced by this grenade when used in enclosed areas are greater than those produced by the fragmentation grenade. The lethal over-pressure created by the detonation will penetrate twisted confines where fragmentation grenades will not. It is, therefore, very effective against enemy soldiers located in bunkers, buildings, and fortified areas. The MK3A2 has an effective casualty radius in open areas of 2 meters. Secondary missiles and bits of fuze may be projected as far as 200 meters from the detonation point.

Characteristics: Body: Height: Weight: Color/Markings: Range: Casualty Radius: Fuze: Fuze Type: Filler: Safety Clip:

Fiber (similar to the packing container for the fragmentation hand grenade) 5.7 inches 15.6 ounces Black with yellow markings around its middle Average soldier can throw the grenade 35 yards Casualty radius in open areas of 2 meters M206A1 or M206A2 Delay (4-5 second) 8 ounces of TNT Yes

Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A8-5-7

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Nomenclature: M7A3

Name: Riot Control Grenade

Capability: Non-lethal ability to subdue and control riots and mobs and temporarily incapacitate traditional and nontraditional combatants. Description: The ABC-M7A3 is a riot control hand grenade that contains the irritant agent CS gas (O-Chlorobenzylidenemalononitrile), that causes the eyes to sting and water. CS is also referred to as tear gas. Used to non-lethally subdue and control riots and mobs. DODIC G963

Characteristics: Body: Height: Weight: Color/Markings: Range: Casualty Radius: Fuze: Fuze Type: Filler:

Sheet metal with four emission holes at the top and one at the bottom 5.7 inches 15.5 ounces Gray body with a red band and red markings Average soldier can throw the grenade 35 yards Irritant cloud lasting 15 to 35 seconds (depends on conditions) M201A1 Delay 7.5 ounces of burning mixture and 4.5 ounces of pellet CS agent.

Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A8-5-7

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Nomenclature: M8

Name: White Smoke Grenade

Capability: Provides smoke for screening friendly forces from enemy observation or as a signal to mark locations or helicopter landing sites. Description: The M8 is used to produce dense clouds of white smoke for signaling and screening. The smoke cloud can be irritating; consequently, the grenade should not be deployed in an area without proper ventilation. DODIC G930

Characteristics: Body: Height: Weight: Color/Markings: Range: Radius: Fuze: Fuze Type: Filler:

Sheet metal 5.7 inches 24 ounces Light green body with black markings and a white top Average soldier can throw the grenade 35 yards Dense cloud emits for 105 to 150 seconds M201A1 Delay 19 ounces of Type C, HC smoke mixture.

Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A8-5-7

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Nomenclature: M14

Name: Incendiary Grenade

Capability: Start fires in areas containing flammable materials and to render vehicles and equipment unusable. Description: The AN-M14 TH3 incendiary hand grenade is used to destroy equipment. It can damage, immobilize, or destroy vehicles, weapons systems, shelters, or munitions. The thermite filler converts to molten iron, burns 40 seconds and melts through or fuses together metallic objects it contacts. It will burn under water. The grenade may also be used to start fires in areas containing flammable materials. DODIC G900

Characteristics: Body: Height: Weight: Color/Markings: Range: Casualty Radius: Fuze: Fuze Type: Filler:

Sheet metal 5.7 inches 32 ounces Gray with purple markings and a single purple band Average soldier can throw the grenade 20 yards Contact M201A1 Delay 26.5 ounces of thermite (TH3) mixture.

Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A8-5-7

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Nomenclature: M18

Name: Colored Smoke Grenade

Capability: Provides smoke for screening friendly forces from enemy observation or as a signal to mark locations or helicopter landing sites. Description: The M18 grenade produces large amounts of colored smoke. It is used mainly as a ground-toground or ground-to-air signaling device, a target or landing zone marking device, or a screening device for unit movements. DODICs G955, G950, G945, G940

Characteristics: Body: Height: Weight: Color/Markings: Range: Radius: Fuze: Fuze Type: Filler:

Sheet steel cylinder with an emission hole at the bottom (and four on the top for Green only) to allow smoke release when the grenade is ignited. 5.75 inches 19 ounces Olive drab body - the top of the grenade is colored the color of the smoke (red, green, yellow, or violet) Average soldier can throw the grenade 40 yards Large, depends on conditions, smoke cloud is emitted for 50 seconds M201A1 Delay 11.5 ounces potassium chlorate, sulphur, baking soda, and dye

Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A8-5-7

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Nomenclature: M25A2

Name: Riot Control Hand Grenade

Capability: Non-lethal ability to subdue and control riots and mobs and temporarily incapacitate traditional and nontraditional combatants. Description: The M25A2 riot control hand grenade is a bursting munition with an integral fuze. It releases a tear gas to subdue riots/crowds of people. It can be filled with CN1, CS1, or DM1 agents. DODIC G927

Characteristics: Body: Height: Weight: Color/Markings: Range: Casualty Radius: Fuze: Fuze Type: Filler:

Compressed fiber and plastic 3+ inches 8 ounces Gray body with red band and red markings Average soldier can throw the grenade 55 yards Medium, depends on conditions, radius is about 5 yards of agent Integral Delay 2.3-3.2 ounces, depending on which (CN1, CS1, or DM1).

Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A8-5-7

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Nomenclature: M67

Name: Fragmentation Hand Grenade

Capability: Suppress/incapacitate traditional and nontraditional combatants and damage light materiel targets. Description: The M-67 hand grenade is designed to burst into numerous fragments when detonated. It produces casualties within an effective range of 20 yards by the high velocity projection of fragments. DODIC G881

Characteristics: Body: Height: Weight: Color/Markings: Range: Casualty Radius: Fuze: Fuze Type: Filler:

Steel sphere 3.53 inches 14 ounces Olive drab body with yellow band at neck and yellow markings Average soldier can throw the grenade 45 yards Large - killing radius is about 5 yards, casualty radius 20 yards, and fragments can disperse as far away as 250 yards. M213 Delay 6.5 ounces of composition B high-explosive

Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A8-5-7

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Nomenclature: M69

Name: Practice Hand Grenade

Capability: Training hand grenade. Description: The M69 practice hand grenade simulates the M67 fragmentation hand grenade for training purposes. The grenade provides realistic training and familiarizes the soldier with the functioning and characteristics of the fragmentation hand grenade. DODIC G811, G878 (Fuze)

Characteristics: Body: Height: Weight: Color/Markings: Range: Casualty Radius: Fuze: Fuze Type: Filler:

Steel sphere 3.53 inches 14 ounces Light blue with white markings Average soldier can throw the grenade 45 yards None M228 Delay Small charge that emits puff of smoke when fired.

Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A8-5-7

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Nomenclature: M83

Name: Practice Smoke Grenade

Capability: Training smoke grenade simulates the M8 White Smoke Grenade. Description: The M83 hand grenade is a practice grenade for the M8 White Smoke Grenade. It emits smoke for 25 to 70 seconds. DODIC G982

Similar to this Picture Characteristics: Height: Weight: Color/Markings: Range: Radius: Fuze: Fuze Type: Filler:

5.7 inches 24 ounces Forest green body with light green markings, a blue band and a white top Average soldier can throw the grenade 35 yards Medium, a dense cloud emits for 25 to 70 seconds M201A1 Delay Single slug of TA.

Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A8-5-7

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Nomenclature: M84

Name: Stun Grenade

Capability: Non-lethal ability to neutralize and disorient traditional and nontraditional combatants. Description: The XM84 Stun Grenade is a non-fragmentation, non-lethal "Flash and Bang" stun grenade that is intended to provide a reliable, effective non-lethal means of neutralizing and disorienting enemy personnel. DODIC GG09

Characteristics: Height: Weight: Color/Markings: Range: Radius: Fuze: Fuze Type: Filler:

5.25 inches 14 ounces Olive drab body with white markings with a pastel green band on body and a brown band on the safety lever Average soldier can throw the grenade 35 yards Small, emits a loud bang and a bright flash to startle/distract M201A1 with a short delay (1 to 2.3 seconds) Delay Magnesium and Ammonium mix

Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A8-5-7

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Nomenclature: Rubber Ball

Name: Riot Control Grenade

Capability: Non-lethal ability to subdue and control riots and mobs. Description: The rubber ball grenade is a non-lethal riot control hand grenade that propels 100 rubber balls to stun and incapacitate a crowd of people. DODIC GG04

Characteristics: Height: Weight: Color/Markings: Range: Casualty Radius: Fuze: Fuze Type: Filler:

5.25 inches 10 ounces Gray body with red band and red markings Average soldier can throw the grenade 35 yards Radius of about 15 yards (Non-Lethal) M201A1-1 Delay Explosives to propel 100 each 0.25 inch diameter rubber balls

Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A8-5-7

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40mm Grenades Nomenclature: M385A1

Name: 40mm Target Practice

Capability: 40mm training round. Description: The M385A1 cartridge is for target practice using the MK19 Grenade Machine Gun. The projectile is made of solid aluminum. It is a ballistic match for the M430A1. DODIC B576

Characteristics: Height: Weight: Color/Markings: Muzzle Velocity: Casualty Radius: Range: Fuze: Fuze Type: Filler:

4.415 inches 0.75 pounds Projectile is light blue with black markings 790 fps None 1600 yards None None Solid Aluminum

Weapon: MK19 Grenade Machine Gun Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A13-6-7

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Nomenclature: M406

Name: 40 mm High Explosive (HE)

Capability: Suppress/incapacitate traditional and nontraditional combatants and damage light materiel targets. Description: This grenade is a high explosive with an impact fuze. When impacted, the grenade explodes, propelling shrapnel to wound personnel and destroy materiel targets. DODIC B568

Characteristics: Height: Weight: Color/Markings: Muzzle Velocity: Casualty Radius: Range: Fuze: Fuze Type: Arming Distance: Filler:

3.9 inches 0.5 pounds Olive drab with gold ogive and markings 250 fps 16 feet 450 yards M551 Point Detonating 46 and 92 feet Composition B

Weapon: M203, M79 Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A13-6-7

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Nomenclature: M430A1

Name: 40mm High Explosive Dual Purpose (HEDP)

Capability: Destroy stationary armored vehicles and suppress/incapacitate traditional and nontraditional combatants. Description: The M430A1 High Explosive Dual Purpose (HEDP) round is meant to penetrate up to 3 inches of steel at a 0 degree angle and then inflicts personnel casualties with the shrapnel produced from the high explosive shape charge. DODIC B542

Characteristics: Height: Weight: Color/Markings: Muzzle Velocity: Casualty Radius: Range: Fuze: Fuze Type: Arming Distance: Filler:

4.42 inches 0.75 pounds Gold ogive with a black body and black markings 780 fps 23 feet for kill and 50 feet casualty 1600 yards Effective M549 PIBD (Armed from rotation) 60 feet minimum Composition B

Weapon: MK19 Grenade Machine Gun Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A13-6-7

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Nomenclature: M433E1

Name: 40mm High Explosive Dual Purpose (HEDP)

Capability: Destroy stationary armored vehicles and suppress/incapacitate traditional and nontraditional combatants. Description: The M433E1 High Explosive Dual Purpose (HEDP) round is meant to penetrate up to 2.5 inches of steel at a 0 degree angle and then inflict personnel casualties with the shrapnel produced from the high explosive shape charge. DODIC B546

Characteristics: Height: Weight: Color/Markings: Muzzle Velocity: Casualty Radius: Range: Fuze: Fuze Type: Arming Distance: Filler:

4.05 inches 0.507 pounds Olive drab with a gold ogive and white markings 250 fps 20 feet casualty 450 yards M550E1 PIBD (Armed from rotation) 45 feet RDX

Weapon: M203 and M79 Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A13-6-7

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Nomenclature: XM576

Name: 40mm Multiple Projectile

Capability: Suppress/incapacitate traditional and nontraditional combatants. Description: XM576 fires 20 lead pellets for effective close range enemy engagement. This is an antipersonnel or breaching round. DODIC B534

Characteristics: Height: Weight: Color/Markings: Muzzle Velocity: Casualty Radius: Range: Fuze: Fuze Type: Arming Distance: Filler:

2.5 inches 0.268 pounds Aluminum cartridge case with white markings 885 fps Impact 50 yards None N/A N/A 20 pellets of 20 grains each

Weapon: M203 and M79 Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A13-6-7

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Nomenclature: M583

Name: 40mm White Star Parachute

Capability: Illuminate the battlefield or provide bright signal. Description: The M583 provides an effective illumination and signaling cartridge for support of ground troops. It launches a candle that descends on a parachute - it gives off about 70,000 candlepower for at least 35 seconds. DODIC B535

Characteristics: Height: Weight: Color/Markings: Muzzle Velocity: Casualty Radius: Range: Fuze: Fuze Type: Arming Distance: Filler:

5.3 inches 0.469 pounds White projectile and ogive 250 fps None Burst Height - 700 feet Delay charge 5 second delay N/A Illumination candle

Weapon: M203 and M79 Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A13-6-7

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Nomenclature: M585

Name: 40mm White Star Cluster

Capability: Mark targets or signal friendly forces. Description: The M585 has the same exterior as the M583 but it contains five white star pellet assemblies that free fall as individual stars upon ejection. The pellet assemblies provide 55,000 candlepower for seven seconds. DODIC B536

Characteristics: Height: Weight: Color/Markings: Muzzle Velocity: Casualty Radius: Range: Fuze: Fuze Type: Arming Distance: Filler:

5.3 inches 0.449 pounds White projectile and ogive 250 fps None Burst Height - 700 feet Delay charge 5 second delay N/A Illumination pellet assemblies

Weapon: M203 and M79 Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A13-6-7

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Nomenclature: XM651E1

Name: 40mm Riot Control Agent

Capability: Subdue and control riots and mobs and temporarily incapacitate traditional and nontraditional combatants. Description: The XM651E1 is a riot/crowd control, CS (tear gas) agent grenade. DODIC B567

Characteristics: Height: Weight: Color/Markings: Muzzle Velocity: Casualty Radius: Range: Fuze: Fuze Type: Arming Distance: Filler:

4.5 inches 0.625 pounds Gray aluminum with a green casing and black markings 250 fps Dense white cloud - round burns for about 25 seconds 450 yards XM581E1 Point Detonating and Delay 98 feet CS pyrotechnic mixture

Weapon: M203 and M79 Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A13-6-7

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Nomenclature: M674

Name: 40mm Riot Control Agent

Capability: Subdue and control riots and mobs and temporarily incapacitate traditional and nontraditional combatants. Description: The M674 grenade can be fired from M79, AN-M8 pistol, or by hand. It contains CS (tear gas) as the crowd/riot control agent. DODIC B537

Characteristics: Height: Weight: Color/Markings: Muzzle Velocity: Casualty Radius: Range: Fuze: Fuze Type: Arming Distance: Filler:

8.8 inches 0.75 pounds Has a red identification band by the barrel and a brown band next to the red one 100 fps Varied - dense white cloud Short Point initiating and delay 3 stage burning delay/point initiating N/A CS pyrotechnic mixture

Weapon: M79. AN-M8 pistol, or by hand Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A13-6-7

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Nomenclature: XM675

Name: 40mm Red Smoke

Capability: Provides smoke for screening friendly forces from enemy observation or as a signal to mark locations or helicopter landing sites. Description: The Red Smoke cartridge is identical to M674 except the markings on the exterior, the assembly contains red smoke and not CS agent, and there is a two stage delay instead of three. This cartridge has a brown identification band instead of the red. DODIC B538

Characteristics: Height: Weight: Color/Markings: Muzzle Velocity: Casualty Radius: Range: Fuze: Fuze Type: Arming Distance: Filler:

8.8 inches 0.75 pounds Has a brown identification band by the barrel 100 fps None, only emits dense red cloud Short Point initiating and delay 2 stage burning delay/point initiating N/A Red pyrotechnic smoke mixture

Weapon: M79. AN-M8 pistol, or by hand Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A13-6-7

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Nomenclature: M715

Name: 40mm Green Smoke

Capability: Provides smoke for screening friendly forces from enemy observation or as a signal to mark locations or helicopter landing sites. Description: The M715 emits a dense cloud of green smoke for signaling and screening purposes. DODIC B508.

Characteristics: Height: Weight: Color/Markings: Muzzle Velocity: Casualty Radius: Range: Fuze: Fuze Type: Arming Distance: Filler:

3.91 inches 0.49 pounds Tip of projectile is colored green 250 fps None 450 yards M733 Impact and delay 50 to 150 feet Pyrotechnic smoke mixture

Weapon: M203 and M79 Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A13-6-7

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Nomenclature: M716

Name: 40mm Yellow Smoke

Capability: Provides smoke for screening friendly forces from enemy observation or as a signal to mark locations or helicopter landing sites. Description: The M715 emits a dense cloud of yellow smoke for signaling and screening purposes. DODIC B509

Characteristics: Height: Weight: Color/Markings: Muzzle Velocity: Casualty Radius: Range: Fuze: Fuze Type: Arming Distance: Filler:

3.91 inches 0.49 pounds Tip of projectile is colored yellow 250 fps None 450 yards M733 Impact and delay 50 to 150 feet Pyrotechnic smoke mixture

Weapon: M203 and M79 Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A13-6-7

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Nomenclature: M781

Name: 40mm Target Practice

Capability: 40mm training round. Description: Target practice round has a frangible plastic ogive and contains a signal dye. When the projectile hits a solid target, it produces a yellow-orange cloud that simulates an explosion. DODIC B519

Characteristics: Height: Weight: Color/Markings: Muzzle Velocity: Casualty Radius: Range: Fuze: Fuze Type: Arming Distance: Filler:

3.9 inches 0.452 pounds Projectile is blue 250 fps None 450 yards None N/A N/A Signal dye

Weapon: M203 and M79 Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A13-6-7

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Nomenclature: M918

Name: 40mm Target Practice Linked

Capability: 40mm training round. Description: This target practice round is for use in the MK19 launcher. It simulates the appearance and ballistics of the M430. When it impacts the target it produces a flash, smoke, and a loud report. DODIC B584

Characteristics: Height: Weight: Color/Markings: Muzzle Velocity: Casualty Radius: Range: Fuze: Fuze Type: Arming Distance: Filler:

4.42 inches 0.75 pounds Blue ogive and body with a brown stripe 780 fps None 1600 yards Effective M550 PIBD (Armed from rotation) 60 feet minimum Flash charge

Weapon: MK19 Grenade Machine Gun Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A13-6-7

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Nomenclature: XM1006

Name: 40mm Sponge Grenade

Capability: Non-lethal ability to subdue to temporarily incapacitate a traditional and nontraditional combatant. Description: The sponge grenade is a non-lethal weapon meant to incapacitate an individual. The projectile has a foam rubber nose and a high-density plastic body. DODIC BA06

Characteristics: Height: Weight: Color/Markings: Muzzle Velocity: Casualty Radius: Range: Fuze: Fuze Type: Arming Distance: Filler:

3.95 inches 0.15 pounds Light green tip with black body and white markings and casing. 260 fps Impact Short None N/A N/A Solid rubber and plastic projectile

Weapon: M203 and M79 Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A13-6-7

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Nomenclature: M1029

Name: 40mm Non-Lethal Crowd Dispersal

Capability: Non-lethal ability to temporarily incapacitate traditional and nontraditional combatants. Description: The M1029 is used to incapacitate personnel non-lethally. It contains 48 0.48 caliber rubber balls that inflict a stunning blow to a combatant’s body. DODIC BA13

Characteristics: Height: Weight: Color/Markings: Muzzle Velocity: Casualty Radius: Range: Fuze: Fuze Type: Arming Distance: Filler:

4.8 inches 2.5 pounds Green band on end 260 fps 10 feet at 100 feet range 35 to 100 feet None N/A N/A 48 rubber balls

Weapon: M203 and M79 Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A13-6-7

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Nomenclature: XM1057

Name: 40mm Non-Lethal Crowd Dispersal

Capability: Non-lethal ability to temporarily incapacitate traditional and nontraditional combatants. Description: This round is the same as the M1029; only it is linked and used in the MK19 launcher for rapid fire.

Characteristics: Height: Weight: Color/Markings: Muzzle Velocity: Casualty Radius: Range: Fuze: Fuze Type: Arming Distance: Filler:

4.8 inches 2.5 pounds Green band on end 260 fps 10 feet at 100 feet range 35 to 100 feet None N/A N/A 48 rubber balls

Weapon: MK19 Grenade Machine Gun Management/Engineering: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A13-6-7

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CHAPTER SEVENTEEN 1 June 2009

MEDIUM and LARGE CALIBER MUNITIONS

FOR OFFICIAL USE ONLY

INTENTIONALLY LEFT BLANK

Nomenclature: PELE

Name: 20mm PELE KE

Capability: 20mm PELE (Penetrator with Enhanced Lateral Efficiency) KE (Kinetic Energy) projectile converts forward momentum into lateral fragmentation effect and/or penetration upon impact with a suitably hard target without the utilization of explosive material. Description: The 20mm PELE Round uses the same case, primer, and propellant as the PGU-27series cartridge. It has a black non-explosive projectile. Upon impact with a suitably hard target, the aluminum nose cap is crushed and the internal plastic core is compressed creating a very high internal pressure within the projectile. The resultant pressure increases until catastrophic failure of the steel body occurs which in turn creates a lateral velocity of the projectile body fragments as the projectile enters the target, causing damage. No explosive means are used in the fragmentation of the projectile. Characteristics: Caliber: 20mm Length: Total Weight: Total Projectile Explosive Fuze:

6.6 in. 0.56 lb. 0.23 lb. None None

Muzzle velocity: 3400 fps (nominal) Weapon: Designed for the M61 Gun System Platforms: F-15, F-16, F/A-18, F-22A Contractor / Status / Improvements / Special Equipment: Contractor - Alliant Tech (ATK) Status Testing Management: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A13-4-7

PELE

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Nomenclature: PGU-27 Series

Name: 20mm Target Practice (TP) (20x102mm NATO)

Capability: Target Practice (TP) cartridge designed for training. It can also be used as a kinetic energy combat round to limit collateral damage potential. Description: The PGU-27 Series Target Practice (TP) cartridge uses a hollow steel projectile body with an aluminum nose plug. It is ballistically matched to PGU-28 Series cartridge. Upon impact with a target, the projectile transfers kinetic energy to the target. There is no incendiary or explosive effect. Characteristics: Caliber: 20x102mm Length: Total 6.6 in. Weight: Total 0.56 lb. Projectile 0.23 lb. Explosive None Fuze: None Muzzle velocity: 3400 fps (nominal) Weapon: Designed for the M61Gun System Platforms: F-15, F-16, F/A-18, F-22A Contractor / Status / Improvements / Special Equipment: Contractor - Alliant Tech (ATK) Status - Production Management: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A13-4-7

PGU-27/B and PGU-27A/B Target Practice Cartridge

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Nomenclature: PGU-28 Series

Name: 20mm (SAPHEI) (20x102mm NATO)

Capability: Damage/destroy moving and stationary light armored vehicles and aircraft and suppress personnel targets. Description: The PGU-28 Semi-Armor Piercing High Explosive Incendiary (SAPHEI) projectile is machined from 15B27 steel bar stock and then hardened to improve performance against lightly armored targets such as APCs and armored helicopters. It functions on impact, but is not fuzed. The projectile consists of two incendiary compounds, High Explosive (HE), zirconium pellet, copper rotating band, aluminum nose, and a support disk. The nose ignites the more energetic body incendiary, which in turn, initiates the Composition A4 HE. The burning of the pyrotechnic material produces a delay, allowing the projectile to penetrate into the target before detonation. The HE reaction splinters the hardened steel body of the projectile and ignites the zirconium pellet providing a long, persistent spark for improved capability to start fires. Characteristics: Caliber: 20x102mm Length: Total 6.6 in. Weight: Total 0.56 lb. Projectile 0.23 lb. Explosive 0.0228 lb. Fuze: None Muzzle velocity: 3410 ft/s (nominal) Weapon: Designed for the M61 Gun System (also the M197-mm gun) Platforms: F-15, F-16, F/A-18, F-22A Contractor / Status / Improvements / Special Equipment: Contractor Status Management: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A13-4-7

Projectile

Propellant Primer

Zirconium Pellet

Main Explosive

Body Incendiary

Incendiary

PGU-28

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Nomenclature: PGU-30 Series

Name: 20mm Target Practice Tracer (TPT)

Capability: 20mm traced training round. Description: The PGU-30 Series Target Practice Tracer (TPT) Round has a blue non-explosive projectile with red T markings. Upon impact with a target, the empty projectile enters the target, causing damage. There is a tracer compound for a tracer effect. Characteristics: Caliber: 20mm Length: Total 6.6 in. Weight: Total 0.56 lb. Projectile 0.23 lb. Explosive none Fuze: none Muzzle velocity: 3450 fps (nominal) Weapon: Designed for the M61 Gun System Platforms: F-15, F-16, F/A-18, F-22A Contractor / Status / Improvements / Special Equipment: Contractor - Alliant Tech (ATK) Status Inventory Management: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A13-4-7

PROPELLANT

CARTRIDGE CASE

PROJECTILE

TRACER PELLETS

NOSE PLUG

PGU-30

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Nomenclature: PGU-23/U

Name: 25mm Target Practice (TP) (25x137mm NATO)

Capability: Target Practice (TP) cartridge designed for training. It can also be used as a kinetic energy combat round to limit collateral damage potential. Description: The PGU-23/U Target Practice (TP) cartridge uses a hollow steel/aluminum projectile body. It is ballistically matched to PGU-25/U ammunition. Upon impact with a target, the projectile transfers kinetic energy to the target. There is no incendiary or explosive effect. Characteristics: Caliber: 20x102mm Length: Total 8.78 in. Weight: Total 1.09 lbs. Projectile 1.09 lbs. Explosive None Fuze: None Muzzle velocity: 3400 fps (nominal) Weapon: Designed for the GAU-12/U and GAU-22/A Gun Systems Platforms: AC-130/U F-35 AV-8/B Contractor / Status / Improvements / Special Equipment: Contractor - Alliant Tech (ATK) Status Inventory Management: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A13-16-7

PGU-23/U

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Nomenclature: PGU-25/U

Name: 25mm HEI (25x137mm NATO)

Capability: Damage/destroy light materiel targets and incapacitate/suppress personnel targets. Description: The PGU-25/U High Explosive Incendiary (HEI) cartridge consists of a forged steel projectile body loaded with aluminized RDX explosive, an M505 series fuze, a steel cartridge case, double base Nitro Cellulose propellant, and a percussion primer. Upon impact with a target, the M505 series point detonating fuze functions the explosive train within 60 microseconds providing fragmentation and incendiary effects. Characteristics: Caliber: 25mm Length: Round 8.78 in. Weight: Total 1.09 lbs. Projectile .4 lb. Explosive 30 grams PBXN-5 Fuze: M505A3 PD set SQ Cartridge Case Material: Steel Primer: M115 Muzzle Velocity: 3609 fps Weapon: Designed for the GAU-12/U gun Platforms: AV-8/B AC-130U Contractor / Status / Improvements / Special Equipment: Contractor - Alliant Tech (ATK) Status Inventory Management: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A13-16-7

PGU-25/U

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Nomenclature: PGU-13/B

Name: 30mm HEI (30x173mm NATO)

Capability: Damage/destroy light materiel targets and incapacitate/suppress personnel targets. Description: The PGU-13/B High Explosive Incendiary (HEI) cartridge consists of a forged steel projectile body loaded with aluminized RDX explosive, an M505 series fuze, an aluminum cartridge case, double base Nitro Cellulose propellant, and a percussion primer. Upon impact with a target, the M505 series point detonating fuze functions the explosive train within 60 microseconds providing fragmentation and incendiary effects. Characteristics: Caliber: 30mm Length: Round 11.5 in. Projectile 5.5 in. Weight: Total 1.50 lbs. Projectile .80 lb. Explosive 0.0916 / 0.1019 lb. Fuze: M505 series Cartridge Case Material: Aluminum Primer: M36A2 Percussion Muzzle velocity: 3346 fps Weapon: Designed primarily for GAU-8/A Gun System and the Navy Goalkeeper ship system Platforms: A-10, AC-130/U (clipped/linked) for MK44 Gun system Contractor / Status / Improvements / Special Equipment: Contractor Status Management: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A13-14-7

PGU-13/B

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Nomenclature: PGU-14A/B

Name: 30mm API (30x173mm NATO)

Capability: Destroy moving or stationary tanks, armored personnel carriers and other armored targets. Description: The PGU-14A/B Armor Piercing Incendiary (API) - Kinetic energy projectile is used against armored targets. The PGU-14A/B API Armor Piercing Incendiary round has a lightweight body which contains a sub-caliber high density penetrator of Depleted Uranium (DU). In addition to its penetrating capability DU is a natural pyrophoric material which enhances the incendiary effects. This round is effective against tanks and personnel carriers. The projectile is made up of four parts: an aluminum body or pusher, glass-reinforced nylon rotating band, DU rod penetrator, and aluminum windshield. The projectile has no fuze; its penetration depends on the shape of the penetrator, KE of the round, and grazing angle at impact. Characteristics: Caliber: 30mm Length: Round 11.5 in. Projectile 5.5 in. Weight: Total 1.60 lbs. Projectile .94 lb. Fuze: None Cartridge Case Material: Aluminum Primer: M36A2 Percussion Muzzle velocity: 3323 fps Weapon: Designed primarily for GAU-8/A Gun System Platforms: A/OA-10A Contractor / Status / Improvements / Special Equipment: Contractor Status Management: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A13-14-7

PGU-14A/B

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Nomenclature: PGU-15/B

Name: 30mm Target Practice (TP) (30x173mm NATO)

Capability: The Target Practice (TP) cartridge is designed for training. It can also be used as a kinetic energy combat round to limit collateral damage potential. Description: The PGU-15/B Target Practice (TP) uses a hollow steel/aluminum projectile body. It is ballistically matched to PGU-13/B ammunition. Upon impact with a target, the projectile transfers kinetic energy to the target. There is no incendiary or explosive effect. Characteristics: Caliber: 30mm Length: Round 11.5 in. Weight: Total 1.50 lbs. Projectile .83 lb. Fuze: None Cartridge Case Material: Aluminum Primer: M36A2 Percussion Muzzle velocity: 3350 fps Weapon: Designed primarily for GAU-8/A Gun System Platforms: A/OA-10A Contractor / Status / Improvements / Special Equipment: Contractor Status Management: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A13-14-7

PGU-15/B

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Nomenclature: PGU-9C/B

Name: 40mm HEI-P (L-60 NATO)

Capability: Damage/destroy light materiel targets and incapacitate/suppress personnel targets. It can also be used for target spotting/marking. Description: The 40-mm PGU-9C/B High Explosive Incendiary-Plugged (HEI-P) (Zirconium) cartridge consists of a steel case, propellant charge, an approximately 1.9 pound steel projectile body, zirconium liner, Composition A6 explosive charge and FMU-154 /B fuze. It was specifically developed for the AC-130 to increase fire-starting capability while maintaining adequate fragmentation for use against personnel. Each projectile will produce approximately 1,000 fragments with an average weight of 0.5 grams. Characteristics: Caliber: 40mm Length: Round 17.6 in. Projectile 7.2 in. Cartridge 12.2 in. Diameter: 1.6 in. Weight: Total 6.50 lbs. Projectile 1.9 lbs. Cartridge 4.6 lbs. Explosive 0.22 lb. Fuze: FMU-154/B and FMU-154A/B Cartridge Case Material: Steel or brass Weapon: Used with M2A1 (modified) 40mm automatic gun Platform: AC-130 Contractor / Status / Improvements / Special Equipment: Contractor Status Management: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A13-11-7

PGU-9C/B

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Nomenclature: PGU-43/B

Name: 105mm Training Practice (TP)

Capability: PGU-43/B Practice cartridge is designed to enhance safety in the training environment, and still provide an impact signature that can be seen on the gunship sensors. It can also be used as a kinetic energy combat round to limit collateral damage potential. Upon impact with a target, the projectile transfers kinetic and chemical energy to the target. Description: The 105mm inert PGU-43/B Practice cartridge with Live Supplementary Charge was modified from the semi-fixed to fixed configuration for use on the AC-130 Gunship. The PGU-43/B Practice cartridge is similar to the inert M1 Cartridge, except the inert PGU-43/B consists of a CYU-1/B brass cartridge case. The PGU-43/B is the inert target practice version which utilizes the less expensive M739A1 fuze. Characteristics: NSN Caliber: Length:

1315-01-472-1854 105mm Round Projectile Diameter Weight: Total Projectile Fuze: Case/Prop Explosive Fuze: M739A1 Cartridge Case Material: Brass

DODAC: CA22 31.07 in. 15.3 in. 4.13 in. 45.0 lbs. 32.4 lbs. 1.5 lbs. 6.0 lb. 0.3 lb.

Weapon System: 105mm (MOD) M137 Howitzer Platform: AC-130H, AC-130U Contractor / Status / Improvements / Special Equipment: Contractor - LAP - GD-OTS (Canada) Status Production Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A13-13-7 - 105mm Airborne Artillery Ammunition

105mm PGU-43/B TP

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Nomenclature: PGU-44/B

Name: 105mm High Explosive (HE) (105mm NATO Artillery)

Capability: It is used for conventional fire support for Harassment and Interdiction (H&I), fragmentation, mining, and blast effect. It can damage/destroy light-medium materiel targets and incapacitate/suppress personnel targets and breach structures and obstacles. Description: Used in the Air Force Special Operation Command (AFSOC) AC130 Gun Ships, the 105MM PGU-44/B is a fixed round. It consists of the refurbished/modified Army M1 Projectile assembly crimped on the CYU-1/B brass cartridge case at the loading to allow for safety and handling concerns. The PGU-44/B is fuzed with an FMU-153/B PD/Delay fuze. The contractor is required to inspect, x-ray projectile, replace prop charge, rework as necessary and crimp acceptable M1(Army) semi-fixed rounds to become the PGU-44/B. The PGU-44/B program uses the CYU-1B brass cartridge case, the M28A2 primer, and the M67 prop charge. Characteristics: NSN Type Caliber: Length -

1315-01-515-6269 DODAC: CA34 HE 105mm Round 31.07 in. Projectile 15.3 in. Diameter 4.13 in. Weight Total 46.0 lbs. Projectile 32.4 lbs. Fuze: 3.233 lbs. Case/Prop 6.0 lbs. Explosive: 5.0 lbs. Body Material Forged Steel Color Black with yellow markings Explosive 4.8 lbs. TNT; 5 lbs. Comp B Maximum Propelling Charge Compatibility M67 (Zone 7) Maximum Range 11.5 Km Fuze FMU-153/B Cartridge Case Material Brass Weapon System: 105mm (MOD) M137 Howitzer Contractor / Status / Improvements / Special Equipment: Contractor - LAP - GD-OTS (Canada) Status Inventory (USAF) Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A13-13-7 - 105mm Airborne Artillery Ammunition

105mm PGU-44/B HE (USAF)

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Nomenclature: PGU-45/B

Name: 105mm HE/HF (105mm NATO Artillery)

Capability: Incapacitate/suppress personnel targets and damage/destroy light material targets. Description: The 105mm High Explosive/High Fragmentation (HE/HF) PGU-45/B cartridge consists of a forged HF-1 steel projectile, specifically heat treated to produce multiple fragments appropriately sized to incapacitate personnel targets. The round was modified from semi-fixed to fixed configuration for use on the AC-130 Gunship. The projectile contains approximately five pounds of Comp B explosive fill, a CYU-1/B brass cartridge case, M67 propellant charge, M28 Primer & Flash Tube, and a radar proximity FMU-160/B fuze. Each projectile will produce approximately 13,000 fragments upon detonation. The FMU-160/B fuze is factory set for a 15 foot above ground level height of burst. The FMU-160/B does not employ a selectable Point Detonating (PD) feature, but will function in the PD mode if the proximity mode fails. Characteristics: NSN: 1315-01-514-8595 Caliber: 105mm Length: Round 31.07 in. Projectile 15.3 in. Diameter 4.13 in. Weight: Total 45.0 lbs. Projectile 32.4 lbs. Fuze 1.5 lbs. Case/Prop 6.0 lbs. Explosive 5.0 lbs. Fuze: FMU-160/B Cartridge Case Material: Brass

DODAC: CA33

Weapon System: 105mm HE/HF (MOD)/M137 Howitzer Platform: AC-130H, AC-130U Contractor / Status / Improvements / Special Equipment: Contractor Status - Production Management: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A13-13-7 - 105mm Airborne Artillery Ammunition Primer, Percussion FMU-160/B

Comp B CYU-1/B Charge, Propelling

PGU-45/B

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Nomenclature: FMU-160/B

Name: Proximity Fuze

Capability: Used with 105mm PGU-45B for 15 foot Height of Burst (HOB). Description: The FMU-160/B Fuze is an RF Proximity Fuze with a Point Detonating (PD) backup. Designed specifically for use on the AC-130 Gunship, the fuze is factory set to provide a 15-foot height of burst to optimize the lethality of the 105mm High Fragmentation (HF) PGU-45B Cartridge. There are no switches or manual settings for the fuze. Its shape conforms to MIL-STD -333 Short Intrusion Fuzes except for slightly deeper wrench slots. Wrench slot depth is the same as the M557 Fuze so that the current fuze wrenches and PA-71 Storage Tube C-washers (Stop, Packing, Hardened, drawing 9243287 -1) are compatible with the FMU-160/B. The fuze consists of a radome, sleeve, MK41 Safe & Arm (S&A) Assembly, lead block assembly, reserve energizer (battery) and electronics assembly. Characteristics: Weight: 1.8 pounds Weapon System: 105mm (MOD) M137 Howitzer Platform: AC-130H, AC-130U Contractor / Status / Improvements / Special Equipment: Contractor - KDI Status - Inventory Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A13-13-7 - 105mm Airborne Artillery Ammunition

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Nomenclature: FMU-153/B

Name: Fuze Point Detonating (PD)

Capability: Used with 105mm HE M1 (MOD) for detonation with target on impact. Description: The FMU-153 PD (HIP) Fuze is threaded onto the front of a steel projectile uses an MK49 MOD 2 Safe and Arm (S&A) mechanism for inbore and close aboard safety. The Fuze is designed with a hardened improved body so that the projectile will penetrate upon impact. An aluminum head is threaded onto the front of the fuze. Part of the head is a flat aluminum rain shield that protects the firing pin. The hardened body, located behind the head, is made of a stress proof material, and consists of the MK25 stab detonator, MK29 relay detonator, and MK50 relay detonator in the S&A. The arming sequence begins after firing when the projectile is subjected to both setback and spin simultaneously. The NO ARM spin rate is 1000 ROM; and 25-30 rotations completed for arming. Characteristics: Weight: 3.233 pounds Weapon System: 105mm (MOD) M137 Howitzer Platform: AC-130H, AC-130U Contractor / Status / Improvements / Special Equipment: Contractor Status Management: 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A13-13-7 - 105mm Airborne Artillery Ammunition

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Nomenclature: M739A1

Name: Fuze Point Detonating (PD)/Delay

Capability: Used with 105mm PGU-45B for detonation with target on impact. Description: The M739 series Fuzes are the latest improved version of selective impact fuzes. The Fuze body is a one-piece design of solid aluminum and has a standard 2-inch threaded base to match the projectile nose and fuze cavity. The firing pin and detonator assembly is located below the rain insensitive sleeve and provides the super quick action on impact. The firing pin is held in position by a firing pin support which prevents initiation of the M99 Stab Detonator until impact. The M739A1 fuze contains an Impact Delay Module (IDM) assembly instead of the M1 Delay Plunger Assembly. Characteristics: Weight: 1.43 pounds Weapon System: 105mm (MOD) M137 Howitzer Platform: AC-130H, AC-130U Contractor / Status / Improvements / Special Equipment: Contractor Status Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A13-13-7 - 105mm Airborne Artillery Ammunition

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CHAPTER EIGHTEEN 1 June 2009

AIRCRAFT ROCKET SYSTEMS 2.75-INCH AND 5.0-INCH

FOR OFFICIAL USE ONLY

INTENTIONALLY LEFT BLANK

Nomenclature: MK 66

Name: 2.75-inch Rocket Motor

Capability: Attack soft fragment sensitive targets, troops, POL, radars, and aircraft in the open. Description: The 2.75 inch Folding Fin Aerial Rocket (FFAR) system was designed by the U.S. Navy after World War II to replace the 5 inch rocket system. It fills a variety of roles against a wide spectrum of targets. The MK 66 2.75 inch rocket motor was designed to provide a common 2.75-inch motor for helicopters and high performance aircraft. The motor tube is impact extruded from aluminum stock and has an integral forward bulkhead. Fins are spring-activated to open and lock on launch. The MK 66 Mod 4 motor is an improvement on the MK66 and is triservice compatible. Changes include a new E3 filtering system located under the contact band, a new initiator, a new igniter, and a new stabilizing rod and attachment assembly. The new ignition mechanism reduces variations in ignition delay time. The bare MK 66 Mod 4 motor is considered Hazards and Electromagnetic Radiation to Ordnance (HERO) safe without special precautions. The MK 66 Mod 4 motor is also considered safe in Electrostatic Discharge (ESD) environments. Lighter weight launchers have replaced the older models while allowing more rockets to be carried. Selectable and programmable fuze options are now available through rocket management and control systems from various aircraft cockpits. Multiple types of warheads provide a solution to many tactical situations within the battle area. To better depict the varied capabilities within the large selection of warheads available, an additional identification, or name, is now associated with the 2.75 inch rocket weapon system, Hydra 70. The word Hydra refers to the nine-headed serpent of Greek mythology, the 70 indicates the number of millimeters when converted from 2.75 inches. Characteristics: Air Force CRD Weapons Code: R21AA ROCKET 2.75 HE HEAVY W/MK66 R41AA ROCKET 2.75 ILLUM W/MK66 R41BA ROCKET 2.75 IR ILLUM W/MK66 Z75TB ROCKET 2.75 SIGNATURE PRACTICE

Z75TA R31AA Z75PA SZTCA

DODIC/NALC HA03 HA03 HA07 HA07

Pack Mk 1 Mod 0 Mk 706 Mod 0 Mk 1 Mod 0 Mk 706 Mod 0

Warhead/Fuze N/A N/A N/A N/A

Motor Mk66 Mod 2 Mk66 Mod 2 Mk66 Mod 4 Mk66 Mod 4

ROCKET 2.75 TRAINING ROCKET 2.75 WP W/MK66 ROCKET, DUMMY 2.75 STAMP FAC ROCKETS Qty 4 4 4 4

Class Air launched Rocket Dimensions: Length (in.) - 41.7 (without warhead) Diameter (in.) - 2.75 Weight (lbs.) - 13.6 Speed 1,000 m/s Range 10,000 meters

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User Navy Navy Navy Navy

Propellant - NOSIH AA2 - Type - Extruded Double Base, Ethylcellulose Inhibited, Cartridge Loaded - Weight - 7 lbs. - Configuration - 8 point internal burning star Performance at 77o F: Burn Time 1.05 - 1.10 sec. Average Thrust 1300 -1370 lbs. Impulse 1500 lb./sec. Motor Burnout: Range 1300 ft (397 m) Velocity 2425 fps Launch: Spin rate 10rps Exit velocity 148 fps Range - maximum at QE 43o w/MPSM warhead 11,407 yd (10,426 m) Color White with Brown Band and Black Lettering Carriage Options: Aircraft: A-10 F-16A-D AH-1W and AH-1Z Super Cobra UH-1N and UH-1Y Huey AV-8B F/A-18 AH-6 Little Bird AH-64A Apache AH-64D Apache Longbow OH-58D Kiowa Warrior UH-1N MH-60 Defense Armored Penetrator (DAP) Armed Reconnaissance Helicopter (ARH)

Launcher/Rack: LAU-68A/A, LAU-68B/A, LAU-131/A LAU-68A/A, LAU-68B/A, LAU-131/A LAU-68D/A, LAU-61C/A LAU-68D/A, LAU-61C/A LAU-68D/A, LAU-61C/A LAU-68D/A, LAU-61C/A M260, M261 M260, M261 M260, M261 M260, M261 M260, M261 M260, M261 M260

The 2.75-Inch Rocket Systems Includes the Following Items: Unitary Warheads - M274 Training Warhead, Smoke Signature - M151 HE (10 lb.) Warhead with M423 Point Detonating (PD) Fuze - M229 HE (17 lb.) Warhead with M423 PD Fuze - M278 IR Illumination Warhead with M442 Motor Burn Out (MBO) Fuze - M257 Illuminating Warhead with M442 MBO Fuze - WTU-1/B Training Warhead - M156 Smoke, White Phosphorous Warhead with M427 PD Fuze

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Cargo Warheads - M267 MPSM Training Warhead, Smoke Signature with M439 RS Fuze - M261 MPSM HE Warhead with M439 RS Fuze - M255A1 Flechette Warhead with M439 RS Fuze - M264 Red Phosphorous Smoke Screening Warhead with M439 RS Fuze Rocket Motors - Mk 66 Rocket Motor, Mod 1, 2, 3 and 4 - Mk 4/40 Rocket Motor (No longer produced) 2.75-Inch Rocket Launchers - M260 7 Tube Light Weight Launcher (Army) - M261 19 Tube Light Weight Launcher (Army) - LAU 68 D/A 7 Tube Launcher (Navy) - LAU 61 C/A 19 Tube Launcher (Navy) - LAU 68 A/A, LAU 68 B/A and LAU 131 A - 7 Tube Launcher (Air Force) Contractor / Status / Improvements / Special Equipment: Contractor General Dynamics Status Inventory Improvements Insensitive Munitions Special Equipment - N/A Management/Engineering: 506 CBSS/GBLA, Hill AFB, UT Joint Attack Munition Systems Project Office, Redstone Arsenal, AL Technical Order: 11A11-24-7

MK 66 Rocket Motor

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Hydra - 70 Payloads

Navy/Marine Corps 2.75-Inch Rocket System 1. 2. 3, 4. 5. 6. 7. 8. 9.

LAU-68/D/A Rocket Launcher (7 round) MK III Rocket Launcher Tester LAU-61C/A Rocket Launcher (19 round) MK 66 Rocket Motor WTU-1/B Training/M151 High Explosive Warhead M257 Illumination Warhead MK 67 Red Phosphorous (smoke) Warhead M156 White Phosphorous (smoke) Warhead M156 White Phosphorous (smoke) Warhead

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Nomenclature: M423/M427

Name: Point Detonating (PD) Fuze

Description: The M423 and M427 PD fuzes are an oblique sensitive, point-detonating, super-quick fuze used as a common component with the M151 warhead. The safety and arming device forward of the booster housing contains an unbalanced rotor. Upon acceleration of the rocket at firing, a weight setback occurs in the unbalance rotor assembly that houses the primer and detonator. This set back places the fuze into an armed condition when the rocket has traveled approximately 43 to 92 meters from the launcher. Externally the M427 PD fuze is identical to the M423 fuze. The M427 differs from the M423 in that its internal construction is designed to produce the longer arming time and arming distance required for launch from fixed-wing aircraft. Characteristics: Fuze: Model Type Weight Length (total) Explosive Train: Primer Detonator Lead Booster Explosive weight Arming Distance: M423 M427 Color: Body Markings -

M423/M427 Mechanical, Point Detonating 0.75 lbs. 4.0 in. Stab M104 M85 RDX RDX 8.4g 46.9 - 101 yards (43 - 92 meters) 220 - 396 yards (200 - 360 meters) Green Yellow

Management/Engineering: Joint Attack Munition Systems Project Office, Redstone Arsenal, AL

M423/M427 Point Detonating (PD) Fuze

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Nomenclature: M439 RC

Name: Variable Time Delay, Remotely Settable Fuze

Description: This electronic time fuze is a base mounted, electronic variable time delay fuze utilizing a resistance capacitance delay circuit. It is a remote set airburst fuze providing a variable range from 500 to 7,200 meters. The fuze is remotely set and charged in the cockpit through an umbilical assembly that is run through the warhead and connected externally to the rocket launcher. The safe and arming (S&A) mechanism prevents the fuze from being charged if it is in the partially armed or fully armed position. The fuze does not have an internal battery; instead the remote fuze setter in the aircraft supplies energy at the time of fuze setting. The energy stored in the capacitor will operate the electronic timer and fire the M84 electronic detonator. The charging cycle takes place approximately 50 milliseconds prior to rocket motor firing. The fuze begins timing at first motion of the rocket and will function at the prescribed time. Note: If the fuze is set and the motor fails to ignite, it may be loaded into another tube and fired. The fuze may be set a second time; however, it will function longer than set time and should not be used for accurate measurements. For accuracy, 10 days should elapse before resetting. If the fuze has been charged, fired, and duds, it will take approximately 45 days for the charge to decay so that the fuze is safe. Characteristics: Fuze: Model Type Detonator Weight Length Arming Distance Delay -

M439 Electronic, Resistance-Capacitance Time Delay M84 0.4 lbs. 2.77 in. 105.6 to 138.6 yd (96 to 126 meters) 0 to 25 seconds

Management/Engineering: Joint Attack Munition Systems Project Office, Redstone Arsenal, AL

M439 RC, Variable Time Delay Remotely Settable Fuze

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Nomenclature: M442

Name: Fuze

Description: This fuze is used with the M257 illumination and M278 IR illumination warheads. The fuze mechanically arms at rocket motor burnout at which time a pre-set nine second pyrotechnic delay is initiated. After the delay, the warhead airburst functions, deploying the illumination candle. Characteristics: Fuze: Model M442 Type Motor Burn Out Stab Primer PA515 Weight 0.72 lbs. Length3.88 in. Delay 8-10 seconds, pyrotechnic Management/Engineering: Joint Attack Munition Systems Project Office, Redstone Arsenal, AL

M442 Fuze

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Nomenclature: M151

Name: HE Warhead

Capability: Attack troops, materiel and lightly armored and wheeled vehicles. Description: The M151 HE Warhead is a 10-pound high explosive anti-personnel, anti-materiel warhead and is traditionally referred to as the 10-Pounder. The bursting radius is 10 meters; however, high velocity fragments can produce a lethality radius in excess of 50 meters. The nose section is constructed of malleable cast iron that is treaded to receive the fuze. The base section is constructed of steel or cast iron and is threaded so that it can be attached to the rocket motor. The base section and rocket motor are welded together. Total weight of the loaded, unfuzed warhead is 8.7 pounds, of which 2.3 pounds is Composition B4. The M151 can use M423/M427 point detonating or M433 Resistance Capacitance fuzes. Characteristics: DODIC/NALC Warhead/Fuze H583 M151 HE/M423 PD HA12 M151 HE/M423 PD H583 M151 HE/M423 PD HA12 M151 HE/M423 PD H163 M151 HE/M423 PD H583 M151 HE/M423 PD H842 M151 HE/M427 PD H843 M151 HE/M423 PD Warhead Fuze Weight (fuzed) Length (w/o fuze) Body material Filler Weight Color -

Motor Mk66 Mod 3 Mk66 Mod 4 Mk66 Mod 3 Mk66 Mod 4 Mk66 Mod 1 Mk66 Mod 3 N/A N/A

Pack Fastpack Fastpack Wood Wood Wood Wood Wood Wood

Qty 48 48 4 4 4 4 4 4

High Explosive M423, M427, or M433 9.3 lbs. 12.9 in. Pearlitic or ferritic malleable iron Comp B4 2.3 lbs. (1.04 kg) Body Olive drab with Yellow Markings

Management/Engineering: Joint Attack Munition Systems Project Office, Redstone Arsenal, AL

M151 HE Warhead

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User Army Army Army Army SOF SOF Navy/USAF Navy

Nomenclature: WTU-1/B

Name: Training Warhead

Capability: Training round. Description: The WTU-1/B provides a ballistic match for the M151 HE warhead. The WTU-1/B is utilized by the Navy and Air Force for training. The WTU-1/B weighs 9.4 pounds. Characteristics: DODIC HA23 H663 H663 Warhead Weight Length Body material Color -

Warhead/Fuze Motor WTU-1/B Practice N/A WTU-1/B Practice N/A WTU-1/B Practice N/A 2.75 inch Practice 9.4 lbs. 16.04 ins. Iron Blue with White markings

Pack Wood Wood Wood

Qty 4 12 48

Management/Engineering: Joint Attack Munition Systems Project Office, Redstone Arsenal, AL

WTU-1/B Practice Warhead

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User Navy Navy USAF

Nomenclature: M274

Name: Smoke Signature Training Warhead

Capability: Training Warhead. Description: The M274 smoke signature training warhead provides a ballistic match for the M151 HE warhead. The casing is a modified WTU-1/B with vent holes. A modified M423 fuze mechanism is integral to the warhead. A cylindrical cartridge assembly in the forward section of the casing contains 40 grams of potassium perchlorate and aluminum powder that provides a “flash, bang and smoke” signature. The M274 weighs 9.3 pounds. Characteristics: DODIC Warhead/Fuze Motor Pack Qty User H975 M274 Sig Prac Mk66 Mod 3 Fastpack 48 Army HA13 M274 Sig Prac Mk66 Mod 4 Fastpack 48 Army H975 M274 Sig Prac Mk66 Mod 3 Wood 4 Army HA13 M274 Sig Prac Mk66 Mod 4 Wood 4 Army Warhead Safe and Arm (S&A) Device Primer Detonator Weight Length Body material Filler Weight Color -

Smoke signature, training M423 M104 M85 9.3 lbs. 19.04 ins. Iron Potassium Perchlorate/Aluminum Powder 39.5 gr. Blue with White markings and Brown band

Management/Engineering: Joint Attack Munition Systems Project Office, Redstone Arsenal, AL

M274 Training (Smoke) Warhead

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Nomenclature: M229

Name: HE Warhead

Capability: Attack troops, materiel, and lightly armored and wheeled vehicles. Description: The M229 HE warhead is currently in inventory with SOF. An elongated version of the M151, it is commonly referred to as the 17-Pounder. The M229 has a burst radius of 15+ meters with a lethality radius of approximately 75 meters. The filler consists of 4.8 pounds of Composition B4 and can use M423 or M433 fuzes. Its unfuzed weight is 26.4 pounds. Characteristics: DODIC Warhead/Fuze H642 M229 HE/M423 PD HA09 M229 HE/M423 PD Warhead Fuze Weight (fuzed) Length (w/o fuze) Body material Filler Weight Color -

Motor Mk66 Mod 2 Mk66 Mod 4

Pack Wood Wood

Qty 4 4

High explosive M423 and M433 17.0 lbs. 23.03 in. Pearlitic or ferric malleable iron Comp B4 4.8 lbs. (2.18 kg) Olive drab with Yellow Markings

Management/Engineering: Joint Attack Munition Systems Project Office, Redstone Arsenal, AL

M229 HE Warhead

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User SOF SOF

Nomenclature: M257

Name: Illumination Warhead

Capability: Battlefield target illumination. Description: The M257 warhead is designed for battlefield target illumination. The flare warhead is assembled to the rocket motor in the field. The flare and rocket can be launched from either rotary-wing or fixed-wing aircraft. The M257 provides 1M foot candles for 3 minutes and will illuminate approximately 1 square mile. The M257 warhead uses the M442 motor burnout fuze. This fuze functions at a preset range to deploy the candle at approximately 3500 m from launch with the Mk40 motor and 3.5 km from launch with the Mk66 motor. Characteristics: DODIC Warhead/Fuze H183 M257 Ill Flare/M442 HA18 M257 Ill Flare/M442 H812 M257 Ill Flare/M442 H812 M257 Ill Flare/M442 H813 M257 Ill Flare/M442

Motor Mk66 Mod 3 Mk66 Mod 4 N/A N/A N/A

Pack Wood Wood PA92 PA92 PA92

Qty 6 6 4 4 4

Warhead Illumination Flare Fuze M442 Motor Burn Out Weight 11.0 lbs. Length 31.5 in. Body material - Aluminum Filler Magnesium Sodium Nitrate Weight - 5.44 lbs. (2.47 kg) Color Olive drab with White Markings Management/Engineering: Joint Attack Munition Systems Project Office, Redstone Arsenal, AL

M257 Illumination Warhead

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User Army Army Navy USAF Navy

Nomenclature: M278

Name: Infrared (IR) Illumination Warhead

Capability: Battlefield target illumination. Description: The M278 IR illumination warhead is designed for battlefield target illumination in conjunction with infrared (IR) goggles. The warhead is assembled to the Mk66 rocket motor in the field. The M278 provides an average near IR light output of 250 watts/steradian and less than one K-candle power of visible light. The IR flare will provide IR light for 3 minutes. Time to candle ignition from launch is 13.5 seconds Characteristics: DODIC Warhead/Fuze H183 M257 Ill Flare/M442 H154 M278 IR Flare/M442 HA10 M278 IR Flare/M442 HA06 M278 IR Flare/M442 HA06 M278 IR Flare/M442

Motor Mk66 Mod 3 Mk66 Mod 2 Mk66 Mod 4 N/A N/A

Pack Wood Wood Wood PA92 Wood

Qty 6 3 3 4 6

Warhead IR Flare Fuze M442 Motor Burn Out Weight 11.0 lbs. Length 31.64 ins. Body material - Aluminum Filler DQL-152 (proprietary right) Weight 1980 g. Color Black with White Markings Management/Engineering: Joint Attack Munition Systems Project Office, Redstone Arsenal, AL

M278 IR Illumination Warhead

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User Army SOF SOF/Army Navy USAF

Nomenclature: M261

Name: HE Multi-Purpose Sub-munition (MPSM)

Capability: Attack troops, materiel, and lightly armored and wheeled vehicles. Description: The MPSM HE warhead provides improved lethal effectiveness against area targets such as light armor, wheeled vehicles, materiel, and personnel. It has a plastic nose cone assembly, an aluminum warhead case, an integral fuze, an expulsion charge, and nine M73 sub-munitions. The primary warhead fuze (M439) is remotely set with the ARCS, MFD or RMS to provide range (time of flight) from 500 meters to approximately 7000 meters. On the AH-1 the RMS is programmable only from 700 meters to 6900 meters. Initial forward motion of the rocket at firing initiates fuze timing. At fuze time at a point before and above the target, depending on the launch angle and range, the expulsion charge is initiated. The MPSMs are separated by ejection, and arming occurs when the Ram Air Decelerator (RAD) deploys. The RAD virtually stops forward velocity and stabilizes the decent of the SM. An M230 omni-directional fuze with an M55 detonator is used on each SM and is designed to function regardless of impact angle Each SM has a steel body that has a 3.2-ounce shaped charge of Composition B for armor penetration in excess of four inches of Rolled Homogeneous Steel (RHA). The SM is internally scored to optimize fragments against personnel and materiel. Upon detonation, the shaped charge penetrates in line with its axis and the SM body explodes into high velocity fragments (approximately 195 at 10 grains each up to 5,000 feet per second) to defeat soft targets. The fuzed weight of the M261 is 13.6 pounds. Characteristics: DODIC Warhead/Fuze Motor Pack Qty User H165 M261 MPSM HE/M439 Mk66 Mod 3 Fastpack 48 Army HA14 M261 MPSM HE/M439 Mk66 Mod 4 Fastpack 48 Army H165 M261 MPSM HE/M439 Mk66 Mod 3 Wood 4 Army HA14 M261 MPSM HE/M439 Mk66 Mod 4 Wood 4 Army Warhead Cargo, High Explosive Fuze M439 Remote Set Weight (fuzed) - 13.5 lbs. Length 26.86 ins. Body material - Aluminum Filler 9 ea. M73 HE multi-purpose sub-munitions (MPSM) Color Olive Drab with Yellow Markings and yellow band

The M-73 HE multi-purpose sub-munition consists of a full caliber, cylindrical tapered steel casing, pres-cored internally for controlled fragmentation, a RAD device for arming, orientation and stabilization, a truncated shaped charge liner, wave shaper and the M230 omni-directional o fuze with explosive train. The kill mechanism is a truncated sub-caliber, 44 included angle, shaped charge copper liner 33.02mm (1.3 in.) high. The sub-munition detonation is initiated by the M230 fuze that is armed by the action of the RAD on ejection from the warhead.

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Payload nine each Model M73 HE Multi-purpose sub-munitions (MPSM) Detonator - M55 Weight Each M73 MPSM - 1.2 lbs. Total Weight of 9 M73 - 10.8 lbs. Filler Comp B Each 0.2 lbs. Total of 9 M73 - 1.8 lbs. Management/Engineering: Joint Attack Munition Systems Project Office, Redstone Arsenal, AL

M261 HE MPSM Warhead

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Nomenclature: M267

Name: Multi-Purpose Sub-munition (MPSM) Smoke Signature (Training)

Capability: Training Warhead. Description: The M267 MPSM training warhead operationally, physically, and ballistically matches the M261 HE warhead. Three M75 practice MPSMs and six inert SM load simulators take the place of nine HE sub-munitions in the M261 warhead. Like the M274, the practice MPSMs contain pyrotechnic powder that provides a “flash, bang and smoke” signature. Each of the three practice MPSMs contains approximately 14 grams (0.6 ounces) of pyrotechnic powder. An M231 fuze with an M55 detonator is used with the practice MPSMs. Characteristics: DODIC Warhead/Fuze H974 M267 MPSM Prac/M439 HA17 M267 MPSM Prac/M439 H974 M267 MPSM Prac/M439 HA17 M267 MPSM Prac/M439

Motor Mk66 Mod 3 Mk66 Mod 4 Mk66 Mod 3 Mk66 Mod 4

Pack Fastpack Fastpack Wood Wood

Qty 48 48 4 4

User Army Army Army Army

Warhead Cargo, Smoke Signature, Training Fuze M439 Remote Set Weight (Fuzed) - 3.6 lbs. Length 26.86 in. Body Material - Aluminum Filler 3 M75 Sub-Munitions and 6 Inert Simulators Color Blue with White Markings and Brown Band The M75 Sub-Munition (SM) consists of a steel body with a smoke signature flash charge. The body has the identical outside configuration as the M73 HE sub-munition. However, the wall is thicker and is machined out so the finished sub-munition with smoke capsule has the same weight and center of gravity as the loaded HE sub-munition. The smoke/flash charge consists of 14 grams of a mixture of potassium perchlorate and aluminum powder. The M55 detonator in the M231 Omni-directional fuze ignites the charge. The M231 fuze is identical to the M230 fuze except there is no explosive lead, no booster pellet, and no wave shaper. The smoke capsule is located directly below the fire hole of the fuze. Payload 3 M75 Practice SM Detonator - M55 Weight Each - 1.2 lbs. Total (9 (3 M75 SM w/6 inert simulators)) - 10.8 lbs. Filler Aluminum Powder & Potassium Perchlorate Each 0.04 lbs. (14 g) Total (3 M75 SM) - 0.12 lbs. (42 g)

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Management/Engineering: Joint Attack Munition Systems Project Office, Redstone Arsenal, AL

M267 MPSM Training Warhead

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Nomenclature: M255A1

Name: Flechette Warhead

Capability: Attack enemy personnel. Description: The M255A1 flechette warhead is primarily for antipersonnel operations. This warhead contains 1,179 sixty-grain hardened steel flechettes and uses the M439 Remote Set fuze. A full material release has been issued for use by Army Aviation units effective July 2006. Characteristics: DODIC Warhead/Fuze H462 M255A1 Flechette/M439 HA11 M255A1 Flechette/M439

Motor Mk66 Mod 2 Mk66 Mod 4

Pack Wood Wood

Qty 4 4

User SOF SOF/Army

Warhead Flechette Fuze M439 RS Weight (fuzed) - 13.7 lbs. Length 26.92 in. Body Material - Aluminum Filler 1,179 ea. 60 grain hardened steel flechettes Color Olive Drab with White Markings and Band of White Diamonds Management/Engineering: Joint Attack Munition Systems Project Office, Redstone Arsenal, AL

M255A1 Flechette Warhead

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Nomenclature: M264

Name: Smoke, Red Phosphorous

Capability: Provide Battlefield Smoke Screen for Friendly Forces. Description: The M264 is designed to provide longer standoff range and integration with the range settable M439 RS fuze. The warhead consists of a plastic nose cone, aluminum warhead case; a remote set primary fuze with an umbilical cable, an expulsion charge, and 72 wedges of Red Phosphorous (RP). The RP is more stable and has improved performance as a screening agent during hot temperature conditions. When deployed the screen effect from 14 rockets will establish a concentration of smoke across a 300 to 400 meter front for 5 minutes. Full screening will be accomplished within 60 seconds after warhead initiation. Characteristics: DODIC Warhead/Fuze H184 M264 RP Smoke/M439 HA15 M264 RP Smoke/M439

Motor Mk66 Mod 3 Mk66 Mod 4

Pack Fastpack Fastpack

Qty 4 4

Warhead Cargo, Smoke Generating Fuze M439 RS Weight (fuzed) - 8.5 lbs. Length 26.92 in. Body Material - Aluminum Filler 72 Red Phosphorous Pellets Weight - 5 lbs. (approximately) Color Light Green with Black Markings and one Brown Band Management/Engineering: Joint Attack Munition Systems Project Office, Redstone Arsenal, AL

M264 Red Phosphorous Warhead

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User Army Army

Nomenclature: M156

Name: White Phosphorous (WP)

Capability: Mark Targets and set targets on fire. Description: The M156 White Phosphorous (WP) warhead consists of a steel body, a base, and an adapter, brazed together. The base is an extruded steel cup threaded for attachment to the rocket motor. The steel adapter, at the forward end of the warhead, is threaded to receive the fuze and also serves to retain the burster charge tube. The M156 WP warhead is primarily used for target marking and incendiary purposes. It ballistically matches the M151 and is of similar construction. Filler for the M156 is 2.2 pounds of white phosphorous. A burster tube, with a charge of 85 grams of Composition B, extends into white phosphorus charge. A lead-in explosive in the fuze, consisting of a 97 mg pellet of RDX, ignites the booster pellet, also in the fuze. The booster pellet, in turn, detonates the burster charge. On detonation, the high explosive ruptures the warhead, dispersing the white phosphorous, generating a white smoke cloud. It provides a smoke marking signal for approximately 2 minutes depending upon wind conditions. The M156 can be used effectively for target marking in open dry terrain and in jungle terrain. The approximate weight of the fuzed warhead is 9.7 pounds. The M156 WP warhead uses M423 and M427 point detonating fuzes. Characteristics: DODIC Warhead/Fuze H519 M156 WP Smoke/M423 H855 M156 WP Smoke/M427

Motor Mk40 N/A

Pack Wood Wood

Qty 4 4

User Army USAF

Management/Engineering: Joint Attack Munition Systems Project Office, Redstone Arsenal, AL

M156 Smoke, White Phosphorous

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Nomenclature: Mk 146 Mod 0

Name: HE Frag Warhead

Capability: Attack troops, materiel and lightly armored and wheeled vehicles. Description: The Mk 149 Mod 0 is a HE-Frag warhead will be in inventory with Navy/Marine Corps. The warhead is an extended-length M151 warhead that contains insensitive explosives and a venting system that have been shown to significantly improve its insensitive munitions response. The Mk 146 Mod 0 has a burst radius of 15+ meters with a lethality radius of approximately 75 meters. The filler consists of 4.8 pounds of PBXN-110 and uses the Mk 436 Mod 0 Fuze. Characteristics: DODIC Warhead/Fuze HA33 MK 146 Mod 0/Mk 436 Mod 0

Motor Mk 66 Series

Pack PA-92

Qty 4

Warhead High explosive Frag Fuze Mk 436 Mod 0 Weight (fuzed) - 16.6 lbs. Length (w/Mk 436 Mod 0 Fuze) - 26.02 in. Body material - Pearlitic or ferric malleable iron Filler PBXN-110 Weight - 4.3 lbs. Color Olive drab with Yellow Markings Management/Engineering: Joint Attack Munition Systems Project Office, Redstone Arsenal, AL

Mk 146 Mod 0 HE Fragmentation Warhead

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User Navy/MC

Nomenclature: WDU-4A/A

Name: Flechette Warhead

Capability: Attack enemy personnel or lightly armored targets. Description: The WDU-4A/A flechette warhead is used against personnel and lightly armored target operations. This warhead contains hardened steel flechettes and uses the Model M113A Self contained Fuzing Mechanism. A small propellant charge in the warhead expels the flechettes after motor burn out. Target damage is caused by impact of high velocity flechettes. Characteristics: DODIC Warhead/Fuze HY71 WDU-4A/A Warhead Fuze Weight Length Body Material Filler Color -

Motor Mk66 Series

Pack Metal

Qty 6

User Navy/Marine Corps

Flechette Model M113 9.30 lbs. 26.02 in. Aluminum 2,220 ea. 20 grain hardened steel flechettes Olive Drab with White Markings

Management/Engineering: Joint Attack Munition Systems Project Office, Redstone Arsenal, AL

WEIGHT SHEAR PIN (1 OF 3)

FLECHETTE

CASE

PUSHER PLATE

WDU-4A/A Flechette Warhead Configuration

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MODEL 113A FUZE

Nomenclature: MK 71

Name: Zuni Rocket

Capability: Attack soft fragment sensitive targets, troops, POL, radars, and aircraft in the open as well as armored vehicles and bunkers. The MK 71 is also used to mark ground targets. Description: The unguided Zuni Folding Fin Aerial Rocket (FFAR) was designed by the US Navy for air-tosurface and air-to-air applications. It can be fired from fixed-wing and rotary-winged aircraft. The steel nozzle expansion cone contains flutes that cause the rocket to spin during burn, thus stabilizing it at all launch velocities. The MK 71 Mods 1 and 2 rocket motors are used in all configurations of the Zuni FFAR, where as the type of fuze and warhead combination is determined by mission requirement. MK 71 rocket motors consist of the following principle parts: motor tube, igniter, MK 88 Mod 0 propellant grain, stabilizing rod, and nozzle and fin assembly. In addition, an electromagnetic radiation barrier and shielding band are used as safety features. The primary difference between the MK 71 Mod 1 and MK 71 Mod 2 rocket motors is that the MK 71 Mod 1 is classified as ESD and HERO susceptible; whereas, the MK 71 Mod 2 is certified as ESD and HERO safe due to a new ignition circuit. Characteristics: DODIC/NALC Warhead/Fuze

Motor

Pack

Qty

User

H567

N/A

MK 71 Mod 1

LAU-10 D/A

4

Navy

H580

N/A

MK 71 Mod 1

LAU-10 C/A

4

Navy

J271

N/A

MK 71 Mod 1 MK 38 Mod 0

1

Navy

HA44

N/A

MK 71 Mod 2 MK 38 Mod 0

1

Navy

Class Air launched rocket Dimensions: Length 76.76 in. (without warhead and fuze) Diameter 5.125 in. Weight: MK 71 Mod 1 - 79.50 lbs. MK 71 Mod 2 - 80.06 lbs. Spin Rate 60 rps Operational Temperature - 40 to 140 °F (-40 to 60 °C) Storage Temperature 65 to 165 °F (-53.8 to 73.9 °C) Propellant: NOSIH AA-6 Type Extruded Double Base, Ethylcellulose Inhibited, Cartridge Loaded Configuration 8 point internal burning star Weight 44.81 lbs. Performance at 77 ° F: Burn time 1.7 - 1.8 sec Average Thrust 5400 - 5600 lbs. Impulse 9662 lbs.-sec Motor Burnout (with MK 6 Mod 7 Practice Warhead at QE 15°): Range 2477 - 2526 ft (755 - 770 m) Speed 2592 - 2723 ft/s (790 - 830 m/s)

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Range (with MK 6 Mod 7 Practice Warhead at QE 15°) - 30000 ft max Range (with WTU-11/B Practice Warhead at QE 42°) - 52000 ft Color - white with brown band and black lettering Carriage Options: Aircraft: F-18-C/D AV-8B AH-1W

Launcher: LAU-10C/A, LAU-10D/A LAU-10C/A, LAU-10D/A LAU-10C/A, LAU-10D/A

The 5.0-Inch Rocket System Includes the Following Items: Unitary Warheads MK 63 Mod 0 HE-FRAG warhead MK 32 Mod 0 AT/APERS warhead MK 24 Mod 0 HE GP warhead with MK 191 Mod 1 base-detonating fuze permanently installed MK 24 Mod 1 HE GP warhead MK 34 Mod 0 white phosphorus smoke warhead MK 34 Mod 2 red phosphorus smoke warhead MK 6 Mod 7 practice warhead MK 32 Mod 1 practice warhead WTU-11/B practice warhead Fuzes MK 188 Mod 0 point-detonating fuze MK 352 Mod 2 point-detonating fuze with BBU-15/B adapter FMU-90/B point-detonating fuze with BBU-15/B adapter MK 436 MOD 0 point-detonating fuze with BBU-15/B adapter Rocket Motors MK 71 Rocket Motor, Mods 1 and 2 5.0-Inch Rocket Launchers LAU-10 C/A - 4 tube launcher (Non Thermal Coated), (Shore base Use Only) LAU-10 D/A - 4 tube launcher (Thermal Coated), (Shipboard Use Only) Contractor / Status / Improvements / Special Equipment: Contractor – NSWCIHD Status – Inventory Improvement – Insensitive Munitions Special Equipment – N/A Management/Engineering: Direct and Time Sensitive Strike Program (PMA-242), NAVAIRSYSCOM, Patuxent River, MD Naval Surface Warfare Center, Indian Head Division, MD

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MK 71 Mod 1/2 Rocket Motor

LAU-10 Series Launcher

LAU-10 Series Launcher

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INTENTIONALLY LEFT BLANK

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CHAPTER NINETEEN 1 June 2009

ARMY ARTILLERY MUNITIONS

FOR OFFICIAL USE ONLY

INTENTIONALLY LEFT BLANK

Nomenclature: M198

Name: 155mm Towed Howitzer

Capability: Provide destructive, suppressive and protective indirect and direct field artillery fires in support of combined arms operations. Description: The M198 155mm towed howitzer is a medium artillery system that provides direct support fires on an interim basis to the Stryker Brigade Combat Teams and direct general support fires to light and special purpose forces (Airborne and Air Assault). The M198 provides significant improvements in lethality, range, reliability, availability emplacement and movement over older 155mm towed howitzers. Normally towed by a 5-ton truck, the M198 system can also be dropped by parachute or transported by CH-47 Chinook helicopter or C-130 aircraft. The carriage of the M198 has a retractable suspension system and a top carriage which can be rotated 180 degrees to decrease overall length for shipment or storage. The fire control equipment may be used by one or two crewmen for direct or indirect fire. The gunner on the left side controls the left and right (traversing) settings and the assistant gunner on the right side controls up and down (elevation) settings. Characteristics: Length 40.7 ft (in tow): 36.2 ft (firing) Width 9.2 ft (in tow) Height 9.5 ft (in tow) Weight 15,700 lbs. Crew 10 Range 22,400 m standard: 30,000 m rocket-assisted Max. Rate of Fire 4 rounds per minute for first 2 minutes Sustained Rate of Fire - 2 rounds per minute Ammunition HE, ICM, CPHD, HC, DPCIM, ILLUM, WP, RAAMS Fires all current NATO 155 mm artillery ammunitions, but not the newer extended range ammo. Contractor / Status / Improvements / Special Equipment: Contractor - Rock Island Arsenal Status Production Management: Technical Order:

M198 155 MM Towed Howitzer

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Nomenclature: M777A1, A2

Name: 155mm Lightweight Towed Howitzer

Capability: Provide destructive, suppressive and protective indirect and direct field artillery fires in support of combined arms operations. Description: The Lightweight 155mm Howitzer (M777A1) is the general support artillery for the Army’s light forces. The use of titanium in its major structures makes it 7,000 pounds lighter than its predecessor (the M198) with no sacrifice in range, stability, accuracy, or durability. Two M777A1’s can be transported by a C-130, and it can be dropped by parachute. The M777A1’s lighter weight, smaller footprint, and lower profile increase strategic deployability, tactical mobility, and survivability. The automatic primer feeding mechanism, loader-assist, digital fire control, and other improvements enhance reliability and give light artillery a semi-autonomous capability found only in self-propelled howitzers. The M777A1 is jointly managed, with the Marine Corps having led the development of the howitzer and the Army having led the development of Towed Artillery Digitization (TAD), the digital fire control system for the M777A1. Software updates and the Platform Integration Kit (PIK) hardware will give the M777A2 the capability to fire the Excalibur precision guided munition. Characteristics: Length 30.4 ft (in tow): 33.5 ft (firing) Width 9.1 ft (in tow) Height 7.4 ft (in tow) Weight 7,000 lbs. Crew 7 Range 24,700 m standard: 30,000 m rocket-assisted Max. Rate of Fire 4 to 8 rounds per minute for first 2 minutes Sustained Rate of Fire - 2 rounds per minute Emplacement time 3 min or less Displacement time 2 min or less Ammunition HE, ICM, CPHD, HC, DPCIM, ILLUM, WP, RAAMS Fires all current NATO 155 mm artillery ammunitions, but not the newer extended range ammo. Contractor / Status / Improvements / Special Equipment: Contractor - Rock Island Arsenal Status Production Management: Technical Order:

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M177A1 Lightweight 155mm Howitzer with Digital Fire Control

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Nomenclature: M109A6

Name: 155mm Paladin Self Propelled (SP) Howitzer

Capability: Provide destructive, suppressive and protective indirect and direct field artillery fires in support of combined arms operations. Description: The M109A6 is an armored, full tracked howitzer carrying 37 complete conventional rounds and two Copperhead projectiles. It is operated by a crew of four and features improvements in the areas of survivability; reliability, availability, and maintainability (RAM); responsiveness; and terminal effects. It is designed with a new turret structure that facilitates integration of the various turret improvements and vulnerability reduction measures. It improves overall crew compartment layout and space. The M109A6 is the most technologically advanced cannon in the Army inventory. This weapon has a 4 man crew, and weights approximately 62,000 lbs./32 tons, and has a cruising range of 186 miles, Max speed is 38 MPH, It has a fuel capacity of 133 gals. The Paladin can operate independently, from on the move, it can receive a fire mission, compute firing data, select and take up its firing position, automatically unlock and point its cannon, fire and move out - all with no external technical assistance. Firing the first round from the move in under 60 seconds, a "shoot and scoot" capability protects the crew from counterbattery fire. The M109A6 Paladin is capable of firing up to four rounds per minute to ranges of 30 kilometers. The Paladin features increased survivability characteristics such as day/night operability, NBC protection with climate control and secure voice and digital communications. The crew remains in the vehicle throughout the mission. Characteristics: Length 30 ft Width 10.3 ft Height 10.7 ft Weight (approx.) 56,400 lbs. empty; 63,615 lbs. combat loaded Crew 4 (accompanying M992 FAASV-5) Cruise Range 300 Kilometers Fuel Capacity 133 gallons Max Speed Highway - 38 mph; Cross country - 19 mph Action Time 45 seconds from stop Range 22,400 m standard; 30,000 m rocket-assisted; min range 4,000 m Max. Rate of Fire 4 rounds per minute for first 3 minutes Sustained Rate of Fire - 1 rounds per minute (depending on thermal warning device) Ammunition Fires all current NATO 155 mm artillery ammunitions, but not the newer extended range ammo. Contractor / Status / Improvements / Special Equipment: Contractor Status Production Management: Technical Order:

19-4

FOUO

M109A6 Paladin SP Howitzer

M109A6 Paladin with M992A2 Field Artillery Ammunition

19-5

FOUO

Nomenclature: M107

Name: 155mm HE Round

Capability: The M107 is the Army’s conventional standard high explosive projectile for all 155mm Howitzers and was originally used in Harassment and Interdiction (H&I) roles. Other principal uses are fragmentation, mining, and blast effect. Currently, it is primarily used in the training role. Description: The M107 projectile is a hollow steel shell filled with high explosive (HE) fill. Earlier models contained an explosive charge of either TNT or Composition-B. There is also a supplementary charge which has 0.36 lb. of TNT contained in an aluminum liner in the fuze cavity. A swaged gilding metal rotating band encircles the shell casing near the base and is protected for shipment by a grommet before loading. A specially designed threaded lifting plug closes the cavity at the nose of the projectile to prevent damage during handling and stowage. The projectiles are loaded with a deep intrusion cavity (4.99 inches max) and a shallow cavity (2.3 inches max). The deep intrusion permits use of proximity fuzes M514, M728, and M782. When all other fuzes are employed, a supplementary charge is used to continue the fuze imitation through to the explosive charge. The shallow cavity projectile will employ all fuzes except the deep intrusion proximity fuzes. Based upon propellant type the range of the projectile is from 2,700 m - 18,100m. Characteristics: DODIC Type Weight Body Material Color Explosive Maximum Propelling Charge Compatibility Maximum Range -

D544 (HE DC) D571 (HE NC) HE 95 lbs. Forged Steel Olive drab with yellow markings TNT - 14.6 lbs., COMP B - 15.4 lbs. M119A2, M232 (Zone 7) 18 km

Contractor / Status / Improvements / Special Equipment: Contractor - DZI Kansas KAAP (LAP) for USMC; GD-OTS - Scranton (Metal Parts) Status Inventory, Army and USMC Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM-43-0001-28

M107 155mm High Explosive (HE) Round

19-6

FOUO

Nomenclature: M549A1

Name: 155mm Rocket Assisted Projectile (RAP)

Capability: The Rocket Assisted Projectile (RAP) was designed to extend the range and improve effectiveness of the 155mm Howitzer. It is used for fragmentation and blast effect against personnel and material. Description: The M549A1 projectile has two distinctive pre-assembled components – the high explosive warhead and the rocket motor. The warhead is fabricated from high fragmentation steel for increased effectiveness and contains TNT. The motor body has a hollow boattail base and a recessed nozzle on it central spin axis. The rocket motor is made from a hi8gh strength steel alloy and contains 6.5 lbs. of solid rocket propellant. The rocket motor provides extended range through functioning of the rocket motor. For all current 155mm artillery systems, the M549A1 can be fired either “Rocket On’ or “Rocket Off.” For the “Rocket On” mode, the cap is removed prior to chambering the projectile. This exposes the pyrotechnic delay to propelling charge gases within the gun tube. The delay is ignited and burns for several seconds before igniting the rocket motor for its short in-flight burn of about three seconds. For use with the Crusader system, the cap was replaced with a blow-through seal. The M549A1 is only used in the “Rocket On” mode. The M549A1 is only used at maximum range with M4A2 (Zone 7), M119A1/M119A2 and M203/M203A1 propelling charges. A special protective energy absorbing lifting plug is used in place of a fuze for handing. PD and proximity fuzing are normally used when firing this projectile. Characteristics: DODIC Type Weight Body Material Color Filler Maximum Propelling Charge Compatibility Maximum Range -

D579 HE, rocket assisted 96 lbs. High fragmentation steel Olive drab with yellow markings TNT – 15 lbs M203A1 (Zone 8) 30 km

Contractor / Status / Improvements / Special Equipment: Contractor Status Inventory Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM-43-0001-28

M549A1 Rocket Assisted Projectile (RAP)

19-7

FOUO

Nomenclature: M712

Name: 155mm HE, Guided, Cannon Launched, Copperhead

Capability: The M712 Copperhead is a laser guided, indirect fired, cannon launched projectile which provides the Field Artillery with the ability to engage both stationary and moving hard point targets such as tanks, armored personnel carriers, bridges and bunkers, with a high degree of first round kill probability. Description: Copperhead is a terminally guided system launched from conventional Howitzers into a ballistic trajectory. During light, the target is illuminated by a forward observer with a laser designator. On board signal processing continuously refines the terminal trajectory and provides guidance to the control surfaces, causing the round to home in on the target. Copperhead consists of three sections: the forward section contains the guidance; the second is the warhead, and the aft section is the stabilization and control. The configuration is aerodynamically controlled by cruciform in-line wings and tail fins that provide roll stabilization and lateral maneuverability sufficient to provide an impact footprint capable of defeating maneuvering armored targets. The guidance section consists of the seeker and electronic assemblies which are housed within the nose dome and steel housing. The payload section includes a high explosive shaped charge warhead in a steel structure and fuze module. The fuze module houses the dual channel Safing and Arming Mechanism and the firing circuit train. The stabilization and control section includes the deployable aero-dynamic surfaces and associated actuator mechanisms. Tail fins are attached to the hubs of the control actuator and retained within the housing by a latch mechanism. The fin locks are released by launched acceleration and the fins are deployed by centrifugal force immediately after the projectile leaves the gun barrel and locked in place. Characteristics: DODIC D510 Type HEAT Weight 138.4 lbs. Body Material Forged steel Color Black with yellow markings Filler Composition B, shaped charge Maximum Propelling Charge Compatibility M119A2 (Zone 7) Maximum Range 6.1 km Contractor / Status / Improvements / Special Equipment: Contractor Status Inventory Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM-43-0001-28

M712 155mm Projectile, HE, Guided, Cannon Launched, Copperhead

19-8

FOUO

Nomenclature: M804A1

Name: 155mm Practice Round

Capability: The M804 Practice round is used in place of HE M107 projectile for 155mm Howitzer crew and forward observed training in indirect fire. Crew and forward observer training can be conducted without the blast and fragmentation effects of the M107 projectile. Description: The M804A1 Practice round is a heavy wall, hollow core forged or cast steel shell and does not contain an explosive filler. It is similar in weight and external configuration of the M107 service round. The projectile body includes four smoke vent holes forward of the rotating band in the bourrelet area. These holes will provide a quick escape route for the smoke produced by the small smoke canister. It produces a visible signature upon projectile impact. This projectile uses standard M107 firing table data. Characteristics: DODIC NSN Type Weight Body Material Color Explosive Maximum Propelling Charge Compatibility Maximum Range -

D513 1320-01-097-4872 Practice 95 lbs. Forged steel Blue with white markings Spotting smoke M119A2 (Zone 7) 18.1 km

Contractor / Status / Improvements / Special Equipment: Contractor - Crain AAA Status Inventory Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM-43-0001-28

M804 155mm Training Round

19-9

FOUO

Nomenclature: M898

Name: 155mm SADARM

Capability: SADARM (Sense and Destroy Armor) is a "smart" artillery submunition designed for precision engagement of self-propelled howitzers as well as other lightly armored vehicles. Additional capability is to effectively interdict mobile armor and suppress armored air defenses. Description: The projectile is fired from any 155mm Howitzer using either an M577A1 or M762A1 fuze. Upon fuze time out, two submunitions are simultaneously expelled from the projectile. These submunitions separate via a Belleville spring device and are slowed by attached drag devices. A pyrotechnic time delay unit ignites the thermal battery which powers up the submunition as well a deploying a Ram Air Inflated Decelerator (RAID). The RAID despins the submunition and orients it directly downward. The multi-mode sensor then determines the altitude above the ground. This sensor consists of active and passive millimeter wave radars as well as an infrared detector. At the proper altitude above the ground the sensor fires an electrical initiated squib. This squib known as the Electric Band Cutter (EBC) detaches the RADI and deploys a Vortex Ring Parachute (VRP). The VRP imparts spin to the submunition and allows it to hang at the proper angle for a collapsing spiral search pattern. If a target is detected within the search, the submunition fires a tantalum alloy Explosively Formed Penetrator (EFP) to defeat it. If no target is detected, the submunition self-destructs. The item is currently in low rate production. Characteristics: DODIC Type Weight Body Material Color Explosive Maximum Propelling Charge Compatibility Maximum Range -

D061 HE submunition, base ejection 102.4 lbs. with fuze Forged steel Black with yellow markings LX-14 - 3.3 lbs. per submunition M203A1 (Zone 8) 22.56 km

Contractor / Status / Improvements / Special Equipment: Contractor Status Inventory Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM-43-0001-28

M898 155mm SADARM

19-10

FOUO

Nomenclature: M483A1

Name: 155mm Dual Purpose Improved Conventional Munition (DPICM)

Capability: The projectile is used to deliver cargo of sub missile dual purpose armor defeating and antipersonnel grenades. Description: The M483A1 Dual Purpose Improved Conventional Munition (DPICM) projectile contains 88 dual-purpose grenades, each capable of penetrating in excess of 2-1/2 inches of homogeneous armor and fragmentation for incapacitating personnel. The M42 grenade (64 each) is embossed on the inside wall surface to provide controlled fragmentation effects. The M-46 grenade (24 each) has a stronger unembossed body which is able to withstand the greater load seen at the rear of the shell due to setback upon firing. The M577A1 Mechanical Time Fuze or the M762A1 Electronic Time Fuze are used in the projectile fuze functioning, and the expelling charge expels the grenades from the aft end of the projectile. The projectile spin disperses the grenades in a circular pattern. Upon expulsion from the projectile, the nylon ribbon stabilizer, attached to the arming screw is each grenade, deploys and orients the grenade. Arming of the grenade occurs during the cycle and on impact. Functioning of the grenade occurs. A shaped-charge jet is directed downward to penetrate armor plate while the grenade body bursts into a large number of small fragments to provide the anti-personnel effects. The grenades themselves provide the projectiles' dual capability. However, a third effect can be achieved by replacing the original expelling charge with a spotting charge designed to detonate the entire projectile as if it were a bulk-loaded HE item. This projectile is shipped with a fusible lifting plug which protects the item during shipping, handling and storage. Characteristics: DODIC Type Weight Body Material Color Filler Maximum Propelling Charge Compatibility Maximum Range -

D563 HE, dual purpose submunition 102.6 lbs. Forged steel Olive drab with yellow diamonds & markings M42/M46 submunitions M119A2 (Zone 7) 17.5 km

Contractor / Status / Improvements / Special Equipment: Contractor Status Inventory Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM-43-0001-28

M483A1 155mm DPICM

19-11

FOUO

Nomenclature: M692/M731

Name: Area Denial Artillery Munition (ADAM)

Capability: The Area Denial Artillery Munitions (ADAM) is used for rapid, remote emplacement of point or tactical minefields used to restrict personnel movement. ADAM should not be planned on hard surface roads or airfields as the mines will shatter or break when hitting asphalt or concrete. Description: ADAM is an antipersonnel (AP) mine activated by deployed trip lines. There are 36 wedgeshaped mines contained in the 155-mm projectile which are fuzed with the M577A1 and M762ET series Time Fuzes. The fuze action ignites the expulsion charge (M10 propellant) contained in a cup in the ogive section, ejecting the 36 mines from the base of the projectile over a large area nearly circular area. Minefield density can be selectively determined by altering the number of rounds applied. There are currently three densities: low, medium, and high. The mines are expelled from the projectile (approximately 600 meters) over the designated target. Shortly after ground impact, up to seven trip line sensors are released out to a maximum length of 20 feet. After a short time delay to allow the mines to return to rest, the electronics are enabled, causing the mine to completely arm. Disturbance of a tripline or disturbance of the mine itself triggers an electronic firing circuit. At a position 2-8 feet above the ground, the kill mechanism, which is a spheroid embossed with a fragmentation pattern detonates. The ADAM mine has lethality out to 15 feet. Self-destruct times are 4 hours for short self-destruct (M731) and 48 hours for long self-destruct (M692). If not triggered by one of the trip lines, the mines will detonate at a predesignated self-destruct interval or if the battery reaches a level that impairs their proper functioning. When the mine detonates, a small charge propels the kill mechanism upward and then the kill mechanism detonates to optimize its effect against personnel. Characteristics: DODIC Type Weight Body Material Color Filler Maximum Propelling Charge Compatibility Maximum Range -

D501 (M692); D502 (M731) HE projectile with submunition AP mines 102.5 lbs. Forged steel Olive drab with yellow triangle & markings 36 anti-personnel mines M119A2 (Zone 7) 17.5 km

Contractor / Status / Improvements / Special Equipment: Contractor Status Inventory Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM-43-0001-28

Projectile, HE, 155mm: M692 ADAM-L

19-12

M731 ADAM-S

FOUO

Nomenclature: M718, M718A1/ M741, M741A1

Name: 155mm Remote Anti Armor Mine System (RAAMS)

Capability: The 155mm M718, M718A1/M741, M741A1 Remote Anti-Armor Mine System (RAAMS) projectiles are used to deliver anti-tank mines in front of enemy armored forces to deny/delay access to a particular area for a specific time period. Description: This series of projectiles contains a payload of nine anti-tank mines stacked one on each other and are ejected during projectile flight by an expulsion charge activated by the M577A1 and M762 ET series Time Fuzes. The mines are armed soon after ground impact, and upon sensing the proximity of tanks or other armor, the mines initiate. If the mines are not initiated during their intended life span, a circuit is activated causing the mines to self-destruct. A percentage of mines in each projectile have anti-disturbance mechanisms to discourage attempts at mine field clearing. The mines are cylindrical in shape measuring five inches in diameter. The fuze action ignites the expulsion charge and gasses, acting against the pusher plate, eject the anti-armor mines from the base of the shell over the selected area. On ejection, set forward force and projectile spin action enables the safe and arming device of the mine to activate. Upon sensing the target and localizing the firing in the vehicles most vulnerable area, the mine fuze firing train is initiated and the main charge then accelerates, at hypervelocity, the Miznay Szhardin (MS) Plate through the belly armor of the vehicle. The large number of fragments, produced beyond the armor, produce a high kill probability. Characteristics: DODIC D503 (M718), D515 (M718A1), D509 (M741), D514 (M741A1) Type HE, projectile with anti-tank mines Weight 103 lbs. Body Material Forged steel Color Olive drab with yellow markings Filler 9 anti-tank mines Maximum Propelling Charge Compatibility M119A2 (Zone 7) Maximum Range 17.5 km Contractor / Status / Improvements / Special Equipment: Contractor Status Inventory Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM-43-0001-28

Projectile, HE, 155mm: M718A1, M741A1

19-13

FOUO

Nomenclature: M795

Name: 155mm HE Round

Capability: The M795 is part of the M483A1 family of ballistically similar 155mm Howitzer ammunition. It is used for conventional fire support for Harassment and Interdiction (H&I), fragmentation, mining, and blast effect. It is also used as a registration round for M483A1 family of cargo munitions. It provides greater range and effectiveness than the M107, which cannot be fired at top zone with M203A1 (Zone 8) charge. Description: The M795 is a 155mm high fragmentation steel (HF1) body projectile filled with 23.8 pounds of TNT and weighing approximately 103 pounds with a gilding metal rotating band for compatibility with all current and future 155mm howitzers. The M795 projectile is employed against personnel, trucks, electronic surveillance and target acquisition devices, supply points, command and control and communications (C3) installations, and mechanized and armored forces. The projectile is compatible with standard and developmental point detonating, shallow intrusion type fuzes and current and developmental propelling charges. The projectile in its standard package is capable of being delivered by parachute and assault landing during the assault phase of airborne operations (AR70-39). Characteristics: DODIC Type Weight Length with fuze Body Material Color Explosive Maximum Propelling Charge Compatibility Maximum Range -

D529 HE, projectile with anti-tank mines 103 lbs. 33.2 ins. High fragmentation forged steel Olive drab with yellow markings TNT - 23.8 lbs. M203A1 (Zone 8) 22.5 km

Contractor / Status / Improvements / Special Equipment: Contractor - DZI Kansas KAAP (LAP) for USMC; GD-OTS - Scranton (Metal Parts) Status - Production/inventory Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM-43-0001-28

M795 155mm High Explosive Round

19-14

FOUO

Nomenclature: M864

Name: 155mm Extended Range (ER) DualPurpose Improved Conventional Munition (DPICM)

Capability: To provide a dual-purpose, improved conventional munition projectile capable of being fired to long ranges. Description: The all steel hollow projectile consists of a cylindrical projectile body with a forebody ogive and an aft base assembly containing a propellant grain. The shell body payload consists of a combination of 72 M42/M46 dual purpose grenades, a nose expulsion charge or selfregistration charge. Airburst functioning achieves payload ejection and dispersion of grenades for maximum terminal effects. Extended range is achieved by the base propellant gases filling the vacuum behind the projectile. The base propellant is ignited during firing from the weapon. Burning is sustained for about 30 seconds of flight time reducing base drag resulting in extended range. At a pre-determined point on the trajectory the pre-set time fuze functions in the expulsion charge and shears the base, expelling the grenade payload. The projectile spin disperses the grenades in circular pattern. A ribbon stabilizer deploys which retards the spin, orients the grenade, and arms it. On impact, detonation occurs with a shape charged jet directed toward the target and the body burst into a large number of small fragments to provide anti-personnel effects. This projectile is provided with a fusible lifting plug for storage, handling and shipping. Characteristics: DODIC Type Weight Body Material Color Explosive Maximum Propelling Charge Compatibility Maximum Range -

D864 HE, projectile with anti-tank mines 102.2 lbs. Steel Olive drab with yellow diamonds and markings A4, 30.5 grams per grenade M203A1 (Zone 8) 28.3 km

Contractor / Status / Improvements / Special Equipment: Contractor Status - Production/inventory Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM-43-0001-28

M864 155mm Extended Range DPICM

19-15

FOUO

Nomenclature: M864

Name: Recap Program

Capability: To provide a dual-purpose, improved conventional munition projectile capable of being fired to long ranges. Description: The objective of the M864 Recapitalization (Recap) Program is to begin fielding up to 322,000 “like new” M864A1 rounds utilizing grenade pyrotechnic Self Destruct Fuzes (p-SDFs) in late 2008. The Recap process involves downloading M42/M46 DPICM grenades, removing existing M223 impact-initiating grenade fuzes, attaching a qualified p-SDF, and final Load, Assemble and Pack (LAP) of the round. The M864A1 rounds will also include the application of an Extended Range Ordnance (ERO) obturator to extend gun tube life. The program conducted a study in FY04 to determine the feasibility of recapping the M864 projectile. The effort successfully evaluated the technical and programmatic risks associated with all recap processes. Consequently, a Pre-Production Engineering (PPE) effort (Phase I) was initiated in 4QFY05, followed by a Qualification effort (Phase II) in 1QFY07, for two p-SDF designs in the M864E2 in order to compete M864A1 Production and have multiple qualified SDF sources for other artillery delivered systems and potential FMS. The M864 consists of three major components: An ogive, containing an expulsion charge at the base of the fuze well; the warhead, a payload of seventy two M42/M46 DPICM grenades; and a solid propellant baseburn unit containing a composite propellant grain and igniter. The M864A1 will be delivered by the M198 Towed Howitzer, Paladin Self Propelled Howitzer and Joint Lightweight 155mm M777 Howitzer. The round is compatible with the M203A1 maximum charge and the Modular Artillery Charge System (MACS). This system supports the Legacy-toObjective transition path of the Transformation Campaign Plan (TCP). Characteristics: DODIC Type Weight Body Material Color Explosive Maximum Propelling Charge Compatibility Maximum Range -

D864 HE, projectile with anti-tank mines 102.2 lbs. Steel Olive drab with yellow diamonds and markings A4, 30.5 grams per grenade M203A1 (Zone 8) 28.3 km

Contractor / Status / Improvements / Special Equipment: Contractor - XM1062 p-SDF: Bulova, Lancaster, PA teamed w/ - DZI Lone Star, Texarkana, TX XM242 p-SDF: ATK, Plymouth, MN teamed w/ -Israel Military Industries (IMI), Israel - DZI Lone Star, Texarkana, TX Status Production/inventory Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM-43-0001-28

19-16

FOUO

Nomenclature: M110, M110A1, and M110A2

Name: 155mm White Phosphorus (WP)

Capability: Provide smoke for marking purposes and can be used to provide screening of mechanized or infantry maneuver. They also have a slight incendiary effect. Description: The projectile is essentially a hollow steel shell filled with white phosphorous. An explosive burster runs down the center of the entire length of the shell. The M110 and M110A1 models use a Tetrytol explosive burster while the M110A2 uses Composition B5 explosive burster. A PD fuze is normally used with these projectiles. The ballistics of these shells are the same as the HE M107 projectile. Characteristics: DODIC Type Weight Body Material Color Filler Maximum Propelling Charge Compatibility Maximum Range -

D550 Smoke, white phosphorus (WP) 98.5 lbs. Forged steel Light green with yellow band and light red markings Smoke, WP - 15.6 lbs. M119A2 (Zone 7) 18.1 km

Contractor / Status / Improvements / Special Equipment: Contractor - LAP - PBA; PMPTS - GDOTS, Scranton Operations; M54 Burster - Expal (Spain) Mecar (Belgium) Status Production/inventory Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM-43-0001-28

M110A1 155mm White Phosphorus (WP)

19-17

FOUO

Nomenclature: M825A1

Name: 155mm Smoke

Capability: Projectile produces smoke so obscure enemy vision or to screen mechanized and infantry maneuver forces. Description: The M825A1 is an improved artillery projectile witch produces a ground screening smoke 125150 meters wide for 5-10 minutes duration. The smoke screen is produced by burning multiple wedge-shaped pieces of felt which have been saturated with White Phosphorous (WP). The system consists principally of the projectile carrier (M483A1 Body) and the payload of 116 felt wedges WP. The projectile carrier consists of an M483A1 ogive and expulsion charge, a modified M483A1 all steel body, and a one-piece steel dome shaped base. The less expensive dome shaped base replaced an expensive toe-piece base and improved flight stability at high quadrant firings. On functioning, the M577A1/M762A1 ET fuze initiates the delay which provides ample time for the canister to clear the thin walled projectile body before the main charge functions. In less than 45 seconds, a dense and uniform smoke screen is created by the burning WP saturated felt wedges. This projectile is shipped with a fusible lifting plug which protects the item during shipping, handling and storage. Characteristics: DODIC Type Weight Body Material Color Filler Maximum Propelling Charge Compatibility Maximum Range -

D528 Smoke, WP 103 lbs. Thin walled steel Light green, yellow band, red markings White phosphorous M203A2 (Zone 8) 22.5 km

Contractor / Status / Improvements / Special Equipment: Contractor Status Production/inventory Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM-43-0001-28

M825A1 155mm Smoke

19-18

FOUO

Nomenclature: M485A2

Name: 155mm Illumination

Capability: The M485A2 projectile is used to provide battlefield illumination at night or other conditions of reduced visibility. It replaces the M118A2 illuminating projectile. Description: This projectile is a hollow steel shell containing a canister with primary expelling charge. A candle assembly, parachute, delay and secondary expelling charge are loaded in the canister. In functioning, a double ejection system is used. The first ejection is caused by fuze functioning, expelling the canister and igniting the delay. The second functioning ejects and ignites the candle from the canister. The main parachute is also deployed. The drogue chute and fins on the canister reduce the spin and decelerate the canister. The main parachute is also deployed. The drogue chute and fins on the canister reduce the spin and decelerate the canister. The main parachute and candle assembly produces 1,000,000-candle power for 120 seconds. Characteristics: DODIC Type Weight Body Material Color Filler VL Illum Burn Time Maximum Propelling Charge Compatibility Maximum Range -

D505 Illumination 92 lbs. Forged steel Olive drab with white markings and one white band Illumination compound - 94 oz. 1,000,000 candle power 120 sec M119A2 (Zone 7) 17.5 km

Contractor / Status / Improvements / Special Equipment: Contractor - Spin Brake Assembly awarded to Woodlawn Mfg for FY06; Candle production Crane AAA (CAAA); PMTPS - FY06 Projectile Metal Parts awarded to Red Lion Status Production/inventory Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM-43-0001-28

M485A2 155mm White Light Illuminating Projectile

19-19

FOUO

Nomenclature: XM982

Name: 155mm Guided, HE, ER-DPICM, EXCALIBUR

Capability: The XM982 is a Precision Guided Extended Range Artillery Projectile, also known as an Extended Range Dual Purpose Improved Conventional Munition (ER DPICM) projectile, is the Army’s fire and forget, smart munition. I provides the capability to attack all three key target sets, soft and armored vehicles, and reinforced bunkers, out to ranges exceeding current 155 mm family of artillery munitions. Description: The Excalibur (XM982) is a 155mm, Global Positioning System (GPS)-guided, fire-and-forget projectile under development as the Army’s next-generation cannon artillery precision munition. The target, platform location, and GPS-specific data are entered into the projectile’s mission computer through an enhanced portable inductive artillery fuze setter or automated system on the Future Combat Systems (FCS) Non-Line of Sight-Cannon (NLOS-C). Excalibur uses a jamresistant internal GPS receiver to update the inertial navigation system, providing precision guidance and dramatically improving accuracy regardless of range. Excalibur weighs 106 pounds, has three fuze options: height-of-burst, point-detonating, and delay/penetration; and is effective in all weather conditions and terrain. The program is using an incremental approach to provide a combat capability to the Soldier as quickly as possible, and to deliver advanced capabilities and lower costs as technology matures. The initial variant (Block Ia-1) was fielded in 2007 to provide an urgently needed capability and is currently being used in the GWOT in both theaters. It includes a unitary high-explosive warhead capable of penetrating urban structures, but is also effective against point targets, personnel targets, such as dismounted infantry and weapon crews, and light materiel targets, including air defense rockets, radars, and wheeled vehicles. Block Ia-2 will provide increased range (up to 40 kilometers) and reliability improvements. The third variant (Block Ib) will maintain performance and capabilities while reducing unit cost. Excalibur is designed for fielding to the digitized Lightweight 155mm Howitzer, the 155mm M109A6 self-propelled howitzer (Paladin), the Future Force indirect fire weapon (FCS NLOS-C) and the Swedish Archer howitzer. Excalibur is an international cooperative program with Sweden, which contributes resources toward the development in accordance with an established project agreement and plans to join in procurement. Excalibur is fin-stabilized and canard controlled and utilizes a slipping obturator. Upon muzzle exit the fins are deployed from under the obturator. At apogee the canards are deployed which maximizes lift to provide glide capability to extended ranges allowing the projectile to glide to the target. At target approach, the projectile goes into a steep descent and the cargo is expelled. The center dispenser bladder then forces the submunitions outward radially in a spoke-like pattern. The 64 M42/46 type submunitions contain a self-destruct fuze to minimize hazardous duds on the battlefield. Excalibur is a family of precision-guided, extended-range modular projectiles incorporating three unique payload capabilities divided into Block configurations. Block I consists of high-explosive, fragmenting, or penetrating unitary munitions to enhance traditional fire support operations with increased range, improved accuracy, and reduced collateral damage against personnel, light materiel, and structure targets. Block II consists of smart munitions to search, detect, acquire, and engage fleeting and short-dwell targets common to open-terrain battlefields. Block III

19-20

FOUO

consists of discriminating munitions to selectively identify and engage individual vehicular targets in urban environments by distinguishing specific target characteristics. Excalibur's precision capabilities are intended to be used by Future Combat System (FCS) Non-Line-ofSight (NLOS) Cannon units to provide close support to maneuver units in urban or complex terrain. Digitized lightweight 155mm howitzer systems will be used to develop and test Excalibur's capabilities before FCS NLOS Cannon is fielded. Characteristics: DODIC Type Weight Body Material Color Explosive Maximum Propelling Charge Compatibility Maximum Range -

DA39 HE, dual purpose submunition 106 lbs. Steel, plastic ogive (cyanate ester) Olive drab with yellow diamonds and markings 30 grams PAX2A explosive in each submunition 5 increments of MACS 37 km, 47 km (Crusader)

Contractor / Status / Improvements / Special Equipment: Contractor Status - Production/inventory Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM-43-0001-28

XM982 155mm Guided, HE, ER-DPICM, EXCALIBUR

19-21

FOUO

Nomenclature: M119A1/A2

Name: 105mm Towed Howitzer

Capability: Provide destructive, suppressive and protective indirect and direct field artillery fires in support of combined arms operations. Description: The M119A1/A2 105mm towed howitzer is a lightweight towed weapon that provide direct support fires to light, airborne and air assault forces. The prime mover for the M119 is the HMMWV. However, it can be dropped by parachute or airlifted with its basic load of ammunition by UH60 and CH47 helicopters of C130 aircraft. The M119A1 and the productimproved M119A2 provide significantly greater range and lethality then the M1021A1 and M102 howitzers. Based on the L118 British Light Gun, the M119 systems in U.S. units are modified with U.S. fire control (digital), increased low-temperature capability (from -25 F to -50 F), improved interchangeability of spare/repair parts, simplified tail light assembly, improved trail access cover and added brackets to incorporate a chronograph and battery computer system. Block 1 improved howitzers were predesignated as the M119A1. Additional Light Artillery System Improvement Program (LASIP) improvements in Block II were completed and those systems were designated as the M119A2. Characteristics: Length 20.75 ft Width 5.83 ft Height 7.25 ft Weight 4,100 lbs. Crew 7 Range 14,000 m standard: 19,500 m rocket-assisted Max. Rage of Fire 6 rounds per minute for first 2 minutes Sustained Rate of Fire - 3 rounds per minute for 30 minutes (sustained) Ammunition Fires all standard NATO 105 mm artillery ammunitions, including the M1 High Explosive, M314 Illuminating, M60/60A2 White Phosphorous (smoke), In addition, it fires the M913 and M760 extended range ammunitions. Contractor / Status / Improvements / Special Equipment: Contractor - Joint US/RO partnerships (Rock Island Arsenal, Watervilliet Arsenal, Seller Instruments, and Royal Ordinance, UK) Status Production Management: Technical Order:

M119A1/A2 105 MM Towed Howitzer

19-22

FOUO

Nomenclature: M102

Name: 105mm Towed Howitzer

Capability: Provide destructive, suppressive and protective indirect and direct field artillery fires in support of combined arms operations. Description: The M102 105mm towed howitzer is a lightweight towed weapon that provides direct support fires to light, airborne and air assault forces. It can be towed by a 2-ton truck or HMMWV, dropped by parachute or transported with it basic load of ammunition by UH60 or larger helicopter and C130 aircraft. It consists of the M137 Cannon, a one piece aluminum M31 Box Carriage which supports a ball screw type elevating mechanism, spring action equilibrators, a circular firing platform, wishbone shaped trails, a 360-degree rubber roller traversing mechanism, an M37 hydro pneumatic variable length recoil mechanism, a retractable suspension system and two wheels with individual hand brakes. The M102 Howitzer also comes equipped with a fire control system which includes the M1A2 Quadrant, M14A1 Quadrant, M113A1 Panoramic Telescope and the M114 Elbow Telescope. When emplaced, the howitzer’s high volume of fires compensates in large measure for the lower explosive weight or the projectile compared to the 155mm howitzers. The M102 has been replaced in the active Army by the M119A1105 towed howitzer. The M102 is still found in several Army National Guard units and the Air Force uses the same cannon and recoil system in the AC130 gunship. Characteristics: Length Width Height Weight Crew Range: Max. Rate of Fire Sustained Rate of Fire Ammunition -

17.1 ft 6.4 ft 5.2 ft 3,670 lbs. 8 11,500 m standard; 17,000 m rocket-assisted 10 rounds per minute for first 3 minutes 3 rounds per minute Fires all standard NATO 105 mm artillery ammunitions, but not the newer extended range ammo.

Contractor / Status / Improvements / Special Equipment: Contractor - Rock Island Arsenal Status Production Management: Technical Order:

19-23

FOUO

Nomenclature: M1

Name: 105mm High Explosive (HE)

Capability: It is used for conventional fire support for Harassment and Interdiction (H&I), fragmentation, mining, and blast effect. Description: The M1 is a semi-fixed 105mm Cartridge consisting of the M14B4 Cartridge Case, M28B2 Percussion Primer, M67 Propelling Charge, a fuze and a projectile containing a TNT or Comp B explosive fill with an aluminum fuze well liner and a supplementary charge. The M1 cartridge is compatible with the M557PD, M739PD, M582MT, M732VT, and the M767ETSQ fuzes. At the expected time, the preset nose fuze detonates the high explosive in the air or on ground impact. Characteristics: DODIC C445 Type HE Weight 39.92lbs. Body Material Forged Steel Color Olive Drab with yellow markings Explosive 4.8 lbs. TNT or 5 lbs. Comp B Maximum Propelling Charge Compatibility M67 (Zone 7) Maximum Range 11.5 Km Fuze M557PD, M739PD, M582MT, M732VT, and the M767ETSQ Cartridge Case Material - Brass Contractor / Status / Improvements / Special Equipment: Contractor - Recap - Blue Grass Army Depot/Hawthorne Army Depot/McAlester AAP; Primers - Lone Star AAP; Prop Charge - SNC; Cartridge Case - Valentec Status Inventory Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM-43-0001-28_R12

M105mm M1 HE

19-24

FOUO

Nomenclature: M60A2

Name: 105mm Smoke Cartridge

Capability: Smoke cartridges are used to build a smoke screen to provide cover for the maneuver unit from enemy observation and as spotting rounds mark location on the battlefield. Description: The M60A2 Smoke Cartridge is a semi-fixed round consisting of a M14 Cartridge Case, M28 Percussion Primer, M67 Propellant Charge, a fuze and a sealed projectile which contains the M53A1 Burster Assembly and a cast white phosphorous filler. Burning white phosphorous produces smoke and heat and can cause severe burns and coughing on contact. The M60A2 projectile can be fired with a point detonating or mechanical time fuze. Upon impacting the ground, the M739 PD Fuze detonates the M53A1 Burster Charge which, in turn, ruptures the projectile body and releases its cargo of white phosphorous. On contact with the atmosphere, white phosphorous spontaneously ignites emitting a dense white cloud of smoke and heat. The evolving smoke screen may serve as an artillery reference point or to temporarily obscure enemy visibility and observation. Characteristics: DODIC Type: Length w/fuze: Weight w/fuze: Body Material: ColorExplosiveFiller Max. Propellant Charge Maximum Range Fuze Cartridge Case Material-

C454 Smoke 31.1 in. 42.9 lbs. Forged Steel Light green, red markings and yellow band Comp B5 White Phosphorus (3.86 lbs.) M67 (Zone 7) 11.5 km M739A1 PD Fuze Brass

Contractor / Status / Improvements / Special Equipment: Contractor Status - Inventory Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM-43-0001-28_R12

M67 Propelling Charge M14B4 Cartridge Cass

M60A2 105mm Smoke Cartridge

19-25

FOUO

Nomenclature: M84A1

Name: 105mm Smoke Cartridge

Capability: Smoke cartridges are used to provide obscuration on the battlefield and to mark locations. Obscuration rounds are used to build a smoke screen to provide cover for the maneuver unit from enemy observation. Spotting rounds mark location on the battlefield. Description: The M84A1 is a semi-fixed smoke cartridge which is comprised of the M14 Cartridge Case, M28 Percussion Primer, M67 Propellant Charge, the time fuze and a projectile that contains a pinned base plug, a black powder expelling charge and three HC smoke canisters. Each metal canister contains a core igniter flash tube, a first fire mix and the HC smoke composition. When ignited, HC composition produces a caustic white smoke. As the round approaches the target area, the fuze ignites the black powder expelling charge which simultaneously ignites and expels the three HC canisters from the base of the carrier. The smoking canisters fall to the ground producing billowing clouds of smoke which last from 40-90 seconds. Characteristics: DODIC Type Weight with fuze Length with fuze Projectile Body Projectile Color Filler Max. Propellant Charge Maximum Range Fuze: Cartridge Case Material:

C442 (A1), C479 (B1) Smoke 44.96 lbs. 30.49 in. Forged Steel Light green with black markings HC (4.1 lbs. per canister) (3 canisters) M67,Zone 7 11.5 km Brass

Contractor / Status / Improvements / Special Equipment: Contractor Status - Inventory Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM-43-0001-28_R12

M84A1 105mm Smoke Cartridge

19-26

FOUO

Nomenclature: M314A3

Name: 105mm Illuminating Cartridge

Capability: The M314A3 projectile is used to provide battlefield illumination at night. It can also be used during reduced visibility conditions and for signaling. Description: The M314A3 is a semi-fixed illuminating cartridge which includes an M14 Cartridge Case, M28 Percussion Primer, M67 Prop Charge, a projectile which contains a pinned base plug, a black powder expelling charge, an illuminating canister with anti-rotational vanes, and a parachute assembly which is connected to the closed end of the canister. The canister contains an illuminating filler covered by a thin layer of first fire composition. Characteristics: DODIC Type Weight w/ fuze Length w/fuze Body Type Payload Max Propelling Charge Maximum Range VL Illumination Burn Time Fuze Cartridge Case Material -

C449 (w/Fuze), C542 (w/o Fuze) Illuminating 46.4 lbs. 31.17 in. Forged Steel Illuminant 2 lbs. M67 (Zone 7) 11.5 km 525,000 candle power 60 sec M582MT, M767ETSQ Brass

Weapon System: Platform: Contractor / Status / Improvements / Special Equipment: Contractor - GD - Canada Status Production/Inventory Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM-43-0001-28_R12

105mm M314A3 Illumination Cartridge

19-27

FOUO

Nomenclature: M444

Name: 105mm High Explosive (HE) Improved Conventional Munition (ICM)

Capability: Delivers an effective concentration of anti-personnel grenades against massing enemy ground forces. Description: The M444 ICM cartridge is a semi-fixed round which includes the M14 Cartridge Case, M28 Percussion Primer, M67 Propellant Charge, the M565 MT / M548 MTSQ Fuze and a projectile which contains a pinned base plug, an expulsion mechanism and eighteen M39 Grenades. A grenade consists of two moveable stabilizing vanes attached to a wedged shaped body which contains a firing and ejection charge mechanism, and a spherical steel bomblet. The M39 Grenade is an effective fragmenting bomblet used to incapacitate enemy personnel and in the prone or standing positions and in fox holes. After the round is fired it reaches a point where the fuze initiates the expelling charge forcing the M39 Grenades from the base of the carrier. In the air stream, the vanes deploy to stabilize the grenade’s orientation, slow the rate of descent and prime the ejection mechanism. On impact, the armed bomblet is ejected from the housing and is propelled upward 4 to 6 feet above the ground. At this height, the bomblet detonates producing blast and fragmentation in all directions. Characteristics: DODIC Type Weight w/fuze Length w/fuze Body Material Color Explosive Max. Propellant Charge Maximum Range Fuze Cartridge Case Material -

.

C462 Improved Conventional Munition (ICM) Approximately 42.0 lb. 31.04 in. Forged Steel Olive Drab with yellow markings 93 lbs. Comp A5 M67 (Zone 7) 11.5 Km M548 MTSQ Brass

Weapon System: 105mm M119A1/A2; M102 Contractor / Status / Improvements / Special Equipment: Contractor Status Inventory Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM-43-0001-28_R12

19-28

FOUO

Nomenclature: M760

Name: 105mm High Explosive (HE)

Capability: It is used for conventional fire support for Harassment and Interdiction (H&I), fragmentation, mining, and blast effect against targets beyond conventional 105mm range. It can damage/destroy light-medium materiel targets and incapacitate/suppress personnel targets and breach structures and obstacles. Description: The M760 is a semi-fixed cartridge composed of the M14 Case, M28 Percussion Primer, M200 Propellant Charge, M1 Projectile Body and a nose fuze. The projectile contains a TNT fill, an aluminum fuze well liner and a supplementary charge. The M760 can be fired with the M739A1 PD, the M582A1 MT, the M732A2 VT and the M767 ETSQ Fuze. Characteristics: DODIC Type Weight w/fuze Length w/fuze Body Material Color Explosive Max. Propellant Charge Maximum Range Fuze Cartridge Case Material -

C473 High Explosive Approximately 42 lbs. 31.1 in. Forged steel Olive Drab with yellow markings 4.8 lbs. TNTB M200, Zone 8 14 Km M739A1 PD, M582A1 MT, M732A2 VT, or M767 ETSQ Brass

Weapon System: 105mm M119A1/A2; M102 Contractor / Status / Improvements / Special Equipment: Contractor Status Inventory Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM-43-0001-28_R12

105mm M760 HE

19-29

FOUO

Nomenclature: M913

Name: 105mm High Explosive Rocket Assisted (HERA)

Capability: It is used for conventional fire support to destroy troops and light armor in the open. Description: The M913 is semi-fixed cartridge composed of the M14B4 Cartridge Case, M28 Percussion Primer, the M229 Propellant Charge, a nose fuze, and a rocket assisted projectile. The projectile warhead contains an explosive filler, an aluminum liner and a supplementary charge. The base of the warhead is threaded in tandem to a rocket motor which contains a rocket propellant grain (Elastomeric) and an ignition delay. The M913 Cartridge is compatible with the M739A1 PD, the M732A2 VT, the M582A1 MT, and the M767 ETSQ fuzes. As the projectile descends toward the intended target area, the preset nose fuze is timed to detonate the warhead in the air or on ground impact. The M913 provides greater range and lethal area coverage and is most effective against light armor and enemy troop concentrations. Characteristics: DODIC C546 Type High Explosive Rocket Assisted (HERA) Weight with fuze Approximately 42 lbs. Length with fuze 36.66 in. Projectile body High Fragmentation Steel Projectile Color Olive drab with yellow markings Explosive 5 lbs. TNT Rocket Propellant Elastomeric Maximum Propelling Charge Compatibility M229 (Zone 8) Maximum Range - 19.5 km Fuze M739A1 PD, M732A2 VT, M582A1 MT, M767 ETSQ Cartridge Case Material - Brass Contractor / Status / Improvements / Special Equipment: Contractor Status Production Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM-43-0001-28_R12

105mm M913 HERA

19-30

FOUO

Nomenclature: M915

Name: 105mm Dual Purpose Improved Conventional Munition (DPICM)

Capability: It is used for conventional fire support to destroy troops and light armor in the open. Description: The M915 cartridge provides dual-purpose improved conventional munition capability at extended ranges for 105mm howitzers and is most effective against light armor and enemy troop concentrations. The M915 can only be fired from the M119 howitzer system. The M915 consists of the M217E1 series Cartridge Case, M28 Percussion Primer, M200 Prop Charge, a nose fuze, and a projectile that contains an expulsion charge, forty-two Dual-Purpose M80 grenades with IM explosive fill, and a base plug. The M80 grenades, with the M234 SD Fuze, is a self destructing, fragmenting shaped charge munition designed to defeat 2.5 inches of armor and incapacitate enemy personnel. The M915 cartridge is fired with the M762A1 ET Fuze, M762 ET Fuze or the M577A1 MT Fuze. As the fired projectile approaches the target area, the preset M762A1 ET fuze initiates the expulsion charge expelling the base plug and grenades from the base of the carrier into the air. During free fall, the stabilizing ribbon on each grenade deploys. This action arms the M234 SD Fuze and also serves to control the free fall orientation of the submunition and spiral safety flag. On impact, the grenade detonates producing a hyper velocity armor piercing jet and numerous incapacitating metal fragments. The self-destruct capability of the M234 Fuze assures high probability of grenade functioning on impact thereby minimizing the threat of battlefield duds. Characteristics: DODIC Type Weight with fuze Length with fuze Projectile body Projectile Color Explosive Maximum Propelling Charge Compatibility Maximum Range Fuze Cartridge Case Material -

CA11 Dual Purpose Improved Conventional Munition 42.7 lbs. 36.67 in. High Alloy Steel Olive drab with yellow markings PDax-2A, Type II (17.2g/grenade) M200 (Zone 8) 14 km M762A1 ET, M762 ET, M577A1 MT Brass

Contractor / Status / Improvements / Special Equipment: Contractor - KDI/L3 Precision Products, Cincinnati, OH M234 SDF; Day and Zimmerman Inc, Texarkana, TX - Projectile LAP Status Production Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM-43-0001-28_R12

105mm M915 DPICM

19-31

FOUO

Nomenclature: M927

Name: 105mm High Explosive Rocket Assisted (HERA)

Capability: It is used for conventional fire support for Harassment and Interdiction (H&I), fragmentation, mining, and blast effect. Description: The M927 is semi-fixed cartridge composed of the M14B4 Cartridge Case, M28B2 Percussion Primer, M67 Propelling Charge, a nose fuze, and a rocket assisted projectile. The projectile warhead contains an explosive filler, an aluminum liner and a supplementary charge. The base of the warhead is threaded in tandem to a rocket motor which contains a rocket propellant grain (Elastomeric) and an ignition delay. The M927 Cartridge is compatible with the M739A1 PD, the M582A1 MT, the M732A2 VT and the M767 ETSQ fuzes. As the projectile descends toward the intended target area, the preset nose fuze is timed to detonate the warhead in the air or on ground impact. Characteristics: DODIC Type Weight w/fuze Length w/fuze Body Material Color Explosive Rocket Propellant Maximum Propelling Charge Compatibility Maximum Range Cartridge Case Material -

C544 HERA Approximately 40 lbs. 335.66 in. High Frag Steel Olive drab with yellow markings 5.8 lbs. TNT Elastomeric M67 (Zone 7) 15 km Brass

Contractor / Status / Improvements / Special Equipment: Contractor - No production Status Inventory Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM-43-0001-28_R12

105mm M927 High Explosive Rocket Assisted (HERA)

19-32

FOUO

Nomenclature: M546

Name: 105mm APERS-T

Capability: Destroy personnel in direct fire, muzzle action, and in a direct fire mission with a time setting other than muzzle action. Description: The M546 Anti-Personnel projectile with tracer (APERS-T) is an assembly of four pieces: base with sintered iron rotating band and M13 Tracer, connector, forward body and fuze adapter. Inside the base of the projectile is a base charge. Forward of the base charge are assembled the tiers of Flechettes, the centers of which form a flash tube. The fuze adapter is assembled forward of the first tier of Flechettes. The fuze adapter contains an M87 detonator, M7 relay, four radially oriented M86 detonators and a pyrotechnic composition smoke marker pellet. The M563 Fuze may be set for muzzle action, for functioning at a minimum of ½ second or in tenths of a second up to 100 seconds after firing. Characteristics: DODIC Type Weight with fuze Length with fuze Projectile body Projectile Color -

C513 APERS-T 34.15 lbs.. 36.66 in. Aluminum Steel Olive drab with yellow band, white markings and A row of white diamonds 8,000 - 8 grain flechettes, 9.14 lbs. XM121

Filler Propelling Charge Maximum Range - 19.5 km Fuze Tracer -

MT-M563-E1, E-2, -E3, E-4 M13, 1.7 grains igniter composition, 5.5 grains tracer composition

Cartridge Case Material - M14B4 Contractor / Status / Improvements / Special Equipment: Contractor Status Inventory Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM-43-0001-28

105mm M546 APERS-T

19-33

FOUO

Nomenclature: M557

Name: Fuze Point Detonating (PD)

Capability: A point detonating fuze with a selective superquick or 0.05 second delay impact for use in all artillery HE projectiles. Description: The M557 PD Fuze consists of fuze M48A3 assembled with the MN125A1 booster. The fuze PD head assembly contains a firing pin held in position by a pin support, which prevents initiation of detonator M24 until impact. The fuze body contains an M1 delay plunger assembly and an interruption assembly with a setting sleeve, which provides a means of setting the selecting PD Super Quick or delay functioning. The delay plunger includes a firing pin and delay element M2. The delay element includes primer M54, a black powder delay charge and relay M7. The M125A1 booster consists of a brass booster body, a delay mechanism and a booster charge. The M17 detonator is held in an unarmed position by centrifugal detents and a gear train mechanism, which provide for the delayed arming for approximately 200 feet depending upon the weapon and charge being fired. Characteristics: DODIC Type WeightLength -

N335 Point Detonating 2.15 lbs. 5.93 in.

Contractor / Status / Improvements / Special Equipment: Contractor Status Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A13-13-7 - 105mm Airborne Artillery Ammunition

19-34

FOUO

Nomenclature: M564, M565

Name: Fuze, Mechanical Time (MT) M565 and Mechanical Time Superquick (MTSQ) M564

Capability: A mechanical time fuze to detonate a variety of spin stabilized projectiles. Description: This fuze consists of a solid steel head threaded into a steel lower cap containing the timing movement , and a steel body containing a detonator. A safety adapter containing a relay and a detonator in addition to an interrupter assembly is threaded into the base of the fuze body. The timing movement is a spring-driven clockwork mechanism secured in the unarme3d position by setback pins and centrifugal detents. A time scale graduated from 0-100 seconds is inscribed on the notable lower cap, and a vernier scale to permit setting accuracy to .01 second appears on the body. The safety adapter interrupter mechanism is the base consists of two centrifugal weights which prevent alignment assembly and safety adaptor portion of the M564 fuze is mechanically the same as the M565 fuze. However, a loaded booster cup and point detonating elements are added for high explosive application, and the M564 has a super quick function. Characteristics: DODIC Fuze, MT: M565 Type Mechanical Time Weight2.03 lbs. Length 5.256 in. Projectile intrusion - 1.516 in.

N278 (M564) Fuze, MTSQ: M564 Mechanical Time and Super-quick 2.14 lbs. 5.966 in. 2.216 in.

Contractor / Status / Improvements / Special Equipment: Contractor Status Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: 11A13-13-7 - 105mm Airborne Artillery Ammunition

19-35

FOUO

Nomenclature: M577A1

Name: Fuze, Mechanical Time and Superquick (MTSQ)

Capability: A mechanical time fuze to operate on a variety of flash initiated artillery projectiles with improved reliability and timing accuracy. Description: The M557A1 fuze is composed of an aluminum ogive and a stainless steel body which contain two M55 Stab Detonators, a mild detonator fuze, crush element, timer assembly, a sleeve and trigger assembly, a safe separation device and a counter assembly. The fuze is manually set from the setting key with a fuze setter and the set time is read directly from the counter window in the ogive. The fuze can be set to function at some specific altitude above the target area or on impact (superquick setting). The setback and spin forces generated in a gun firing environment activate the timer when the fuze is in the set time mode. The safe separation device serves to safe arm the fuze. At two to four seconds prior to reaching the set time, the trigger assembly releases the rotor. This permits the detonators in the rotor to rotate in line with the firing plate. When set time is reached, the firing plate strikes the M55 Stab Detonators which ignite the mild detonating fuze. This produces a hot flash through the lead which initiates the expelling charge and the subsequent aerial expulsion of the payload from the projectile. Characteristics: DODIC Type WeightLength Projectile intrusion Manual Time Setting Fully Armed Rotation -

Setback -

N285 Mechanical Time and Super-quick 1.4 lbs. 5.28 in. 1.516 in. 2 to 200 seconds or PD 2 to 4 seconds before set time Non-Armed - 1,000 rpm Armed - 1,800 rpm Non-Armed - 300 Gs Armed - 600 Gs

Contractor / Status / Improvements / Special Equipment: Contractor Status Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: 11A13-13-7 - 105mm Airborne Artillery Ammunition

19-36

FOUO

Nomenclature: M582A1

Name: Fuze, Mechanical Time Superquick (MTSQ)

Capability: A safe, reliable and accurate mechanical time (MT) fuze for use in all artillery systems. Description: The M577A1 Fuze becomes the M582A1 Fuze when assembled with a loaded booster for high explosive application. The fuze contains a detached lever escapement timer, and modular counter, trigger and safe separation device assemblies. The time set or impact function option is made by turning the setting key, located at the nose of the fuze, with a fuze setter or any screwdriver-like tool. The setting is viewed through a plastic window in the ogive and may be changed any number of times. The timer and trigger modules are held safe by setback and spin locks. The safe separation device (SSD) is linked to the trigger module to provide overhead safety and is also held by spin detents. When the timer reaches two to four seconds before set time, it causes the safe separation device to be released, thus arming the fuze. When the fuze is set for impact function, the SSD is released on launch from the weapon. The centrifugally driven SSD arms at a constant number of turns of the shell and provides a variable safe distance depending on the caliber of the weapon. The M577A1/M582A1 Fuze, for impact functioning features a rear inertial actuated device in lieu of a frontal pressure actuated device (M577/M582). Upon experiencing a velocity change, the rear safe separation device slides forward and stabs the detonator on the firing p9in with sufficient energy to initiate the round. Characteristics: DODIC -

N286 Fuze, MTSQ: M577A1 Type Mechanical Time Weight1.39 lbs. Projectile intrusion - 1.057 in. max Arming Method Setback and spin Fully Armed 2-4 sec. before set time Rotations Non-Arm 16.7 rps Arm 30 rps Setback Non-Arm 300 GS Arm 600 Gs Time Set 2-200 sec.

Fuze, MTSQ: M582A1 Mechanical Time and Super-quick 1.49 lbs. 2.059 in. max Setback and spin 2-4 sec. before set time Non-Arm 16.7 rps Arm 30 rps Non-Arm 300 Gs Arm 600 Gs 2-200 sec.

Contractor / Status / Improvements / Special Equipment: Contractor Status Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: 11A13-13-7 - 105mm Airborne Artillery Ammunition

19-37

FOUO

Nomenclature: M728

Name: Proximity Fuze

Capability: Developed to replace the M513 and M514 proximity fuzes and provide improved functioning reliability. Description: The M728 is a long intrusion proximity fuze which contains a radio continuous wave transmitter/detector, antennas, a clockwork timing mechanism, a power supply, a PD element, and a booster charge. A plastic nose cone fixed to a rotatable setting ring is inscribed with a single index line. The shoulder of the metal sleeve is inscribed with graduated set time markings and a PD line. When fired in the proximity mode, setback forces activate the timing mechanism, initiate the power supply and arm the PD element. Three seconds prior to set time, the proximity element becomes armed and radio transmission begins. The transmitted radio waves travel to the target and are reflected back to the fuze. The interaction between the transmitted and the reflected waves produces a Doppler signal. When the signal reaches a certain amplitude, an electronic switch triggers the explosive train detonating the warhead at an optimum distance from the target. If the proximity element fails to function, the PD element detonates the projectile on impact. Characteristics: DODIC Type WeightOverall Length Projectile intrusion Manual Time Setting Arming Method -

Proximity Approximately 2.19 lbs. 8.6 in. 4.86 in. 5-100 seconds and PD Setback

Contractor / Status / Improvements / Special Equipment: Contractor Status Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: 11A13-13-7 - 105mm Airborne Artillery Ammunition

19-38

FOUO

Nomenclature: M732 Series

Name: Proximity Fuze

Capability: Used with 105mm ammunition for approximately 7 meter Height of Burst (HOB). Description: The M732 series Proximity Fuze can be set for either proximity, airburst, or to function upon impact (PD mode). The proximity section detonates the round at approximately 7 meters above the target (depending upon target background reflectivity and electromagnetic interference). The Fuze well intrusion is 2.2 inches. It has a plastic nose cone crimped to an aluminum collar, index mark for setting time, and is labeled TURN. The fuze sleeve is marked with PD and two second increments in the range of 4 - 156 seconds inclusive. The fuze is shipped with index mark aligned with the PD mark on the sleeve. Characteristics: DODIC Weight Projectile Intrusion Manual Time Setting Arming Method Rotation Setback Delayed Proximity Arming Settings -

N464 1.75 lbs. 2.21 in. 5 to 100 seconds and PD Setback and Spin Non-arm 1,000 rpm All-arm 2,500 rpm Non-arm 800 Gs All-arm 1,300 Bs From 5-10 seconds to 150 seconds

Contractor / Status / Improvements / Special Equipment: Contractor Status Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A13-13-7 - 105mm Airborne Artillery Ammunition

19-39

FOUO

Nomenclature: M732A2 Series

Name: Proximity Fuze

Capability: Used with 105mm ammunition for approximately 7 meter Height of Burst (HOB). Description: The M732A2 is a redesign of the basic M732. The M732 was not able to keep pace with the ballistic environment. Setting it also required a wrench type setting tool, and a significant amount of force. Even with the large setting force, some lots of M732 fuzes have experience3d low reliability due to inbore resetting caused by the spin Environment. Improvements include: changing the analog timer to digital, uses a frequency modulated signal which is less susceptible to counter-measures, improved hand setting capability, modernized electronics and interconnections, and an improved Safe and Arming Mechanism. Characteristics: DODIC Weight Projectile Intrusion Manual Time Setting Arming Method Rotation Setback -

N291 1.75 obs. 2.21 in. 5 to 100 seconds and PD Setback and Spin Non-arm 1,000 rpm All-arm 2,500 rpm Non-arm 800 Gs All-arm 1,300 Bs

Contractor / Status / Improvements / Special Equipment: Contractor Status Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A13-13-7 - 105mm Airborne Artillery Ammunition

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Nomenclature: M739

Name: Fuze Point Detonating (PD)/Delay

Capability: Provides Superquick (SQ) or 50-millisecond delay impact functioning for all standard HE Artillery. Description: The M739 series Fuze has a one-piece solid aluminum body and five modular sub-assemblies: (1) Crossbar and Holder Assembly, (2) Firing Pin and Detonator Assembly, (3) Setting Sleeve Assembly, (4) M1 Delay Plunger and (5) the Safe and Arming (S&A) Assembly. The crossbar and holder assembly is a rain insensitive sleeve that allows firing in heavy rain or foliage with reduced probability of downrange premature functioning. Characteristics: DODIC Weight Projectile Intrusion Arming Metho9d Rotation -

C340 1.5 lbs. 2.21 In. max Setback and Spin Non-arm 1,100 rpm All-arm 1,700 rpm

Contractor / Status / Improvements / Special Equipment: Contractor Status Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A13-13-7 - 105mm Airborne Artillery Ammunition

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Nomenclature: M739A1

Name: Fuze Point Detonating (PD)/Delay

Capability: Provides Superquick (SQ) or 50-millisecond delay impact functioning for all standard HE Artillery. Description: The M739A1 Fuze is a product Improved Version of the M739 Fuze. It uses a mechanical delay called the Impact Delay Mode (IDM) in place of the Pyrotechnic M1 Delay. It has a onepiece solid aluminum body and five modular sub-assemblies: (1) Crossbar and Holder Assembly, (2) Firing Pin and Detonator Assembly, (3) Setting Sleeve Assembly, (4) Impact Delay Module (IDM) and (%) the Safe and Arming (S&A) Assembly. The crossbar and holder assembly is a rain insensitive sleeve that allows firing in heavy rain or foliage with reduced probability of downrange premature functioning. Characteristics: DODIC Weight -

N340 1.43 pounds

Contractor / Status / Improvements / Special Equipment: Contractor Status Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ 506 CBSS/GBLB, Hill AFB, UT Technical Order: 11A13-13-7 - 105mm Airborne Artillery Ammunition

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Nomenclature: M762A1/M767A1

Name: Electronic Time Fuze Artillery

Capability: The M762A1/M767A1 is an electronic fuze used that is autosettable for use with spin stabilized 105mm and 155mm artillery projectiles. Description: The M762A1/M767A1 is an electronic fuze used with spin stabilized 105mm and 155mm artillery projectiles. The M762A1 is used with the cargo carrying projectiles. The M767A1 is similar to the M762A1; however, a booster cup is attached to its base end to provide compatibility with the bursting and fragmentation projectiles. Also the M762A1 and the M767A1 each have their own unique inductive setting ID code. Both fuzes can be set to function in the time mode or impact mode. The M762A1/M767A1 can be set manually without the need of a tool or set remotely via an inductive link with an inductive autosetter. These setting features support an increase in the rate of fire. The M762A1/M767A1 will also further reduce the potential for fuze setting mistakes due to human errors. Characteristics: DODIC Weight Projectile Intrusion Arming Method Rotation Setback Maximum Ballistic Levels Reliability -

N289 (M762), NA17 (M762A1), N290 (M767) 1.1 lbs. (M762 and M762A1) 1.2 lb. (M767 and M767A1) 1.51 in. (M762 and M762A1) 2.21 in. (M767 and M767A1) Setback, Spin, and Piston Actuator Imitation Non-arm 900 rpm All-arm 2,100 rpm Non-arm 800 Gs All-arm 1,000 Gs 30,000 rpm; 30,000 Gs 99%

Contractor / Status / Improvements / Special Equipment: Contractor - L3-BTFP, Lancaster, PA Status Inventory Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM-43-0001-28_R12

M762A1/M767A1 Electronic Time Fuze Artillery

19-43

FOUO

Nomenclature: M782

Name: Multi Option Fuze Artillery (MOFA)

Capability: The M762 Multi Option Fuze Artillery (MOFA) provides proximity, precision time, delay and impact functions in a single fuze. Description: The M782 MOFA fuze is compatible with all current bulk filled bursting projectiles fired in the 105mm (M102 and M119 cannon systems); and 155mm cannon systems (Paladin, and the M198). The MOFA provides proximity, precision time, delay and impact functions in a single fuze, and the inductive fuze set feature optimizes MOFA for use with automated ammunition handling equipment. It has improved Electronic Counter Measure (ECM) capability, Rapid Inductive Set Capability and provides Improved Combat Effectiveness Characteristics: DODIC Type Weight Projectile Intrusion Arming Method Rotation -

NA09 Multi Option 1.94 lbs. 2.21 in. max Setback and Spin Non-arm 1,100rpm All-arm 1,700 rpm

Contractor / Status / Improvements / Special Equipment: Contractor - L3-KDI, Cincinnati, OH; ATK, ABL,WV Status Inventory Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM-43-0001-28_R12

M782 Multi Option Fuze Artillery (MOFA)

19-44

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Nomenclature: MK399 MOD 1

Name: Point Detonating (PD)/Delay Fuze

Capability: The MK399 MOD1 is a point detonating and delay fuze for use in concrete and masonry structures, light armored vehicles and maritime crafts. Description: This MK399 MOD 1 is the Army's Military Operations in Urban Terrain (MOUT) fuze for 105mm, 155mm and for the US Air Force AC-130 gunships. It is a dual setting PD or Delay Set with a screwdriver or M18 setter. MK 399 MOD 1 has a hardened steel penetrator body. This fuze functions reliably after penetration in the delay mode, penetrating concrete and masonry structures, light-armored vehicles and maritime craft. It has a safe and arm with a dual environment safety lock capable of withstanding 30,000 g setback and 30,000 RPM spin. The Delay Mode functions within .004 - .009 seconds. Characteristics: DODIC Type Weight Projectile Intrusion Arming Method Rotation -

N659 Multi Option

Contractor / Status / Improvements / Special Equipment: Contractor - L3-Communications, Lancaster, PA Status Inventory Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM-43-0001-28_R12

MK399 MOD1 Point Detonating (PD)/Delay Fuze

19-45

FOUO

INTENTIONALLY LEFT BLANK

19-46

FOUO

CHAPTER TWENTY 1 June 2009

ARMY MORTAR MUNITIONS

FOR OFFICIAL USE ONLY

INTENTIONALLY LEFT BLANK

Nomenclature: M120/M121

Name: 120mm Mortar

Capability: Provide heavy weapon, high-angle organic indirect fire support to the maneuver unit commander. Destroy personnel and materiel targets out to over 7,000 meters and as close as 166 meters with a killing radius of 70 meters. Description: The M120/121 120mm Mortar is a conventional smoothbore, muzzle-loaded, crew-served, high angle-of fire mortar system that provides increased range, lethality and safety compared to the M30 4.2 Inch Mortar it replaced in mechanized infantry, motorized, armored, and cavalry units. It is employed in towed (M120) and carrier-mounted (M121) versions and in the Stryker Brigade Combat Team mortar carrier. The M120, like all other U.S. mortars, fires a family of enhanced fin-stabilized, U.S.-produced ammunition from a smooth bore. Horseshoe-shaped cheese charges are used to propel the round from the tube. Depending on the distance to the target and the hang time desired, one to four charges are used. Although heavy mortars require trucks or tracked mortar carriers to move them, they are still much lighter than field artillery pieces. They outrange light and medium mortars, and their explosive power is much greater. The M120 towed Mortar System is transported on a trailer towed by the M998 High Mobility Multi-Wheeled Vehicle (HMMWV) and consists of the following components: Characteristics: M298 Cannon Assembly M191 (Bipod) M9 Baseplate M67 sight unit M1101 Trailer Maximum Rate of Fire Sustained Rate of Fire Cartridge Weight Bursting Radius

110 lbs. 68 lbs. 136 lbs. 2.25 lbs. 1460 lbs. 16 rounds/min (first minute) 4 rounds/min indefinitely 13.65 kg (30lbs.) 70 meters

Contractor / Status / Improvements / Special Equipment: Contractor - Various Contractors Status Production Management: PEO AMMO & PM-Mortars; Picatinny Arsenal, NJ Technical Order: TM 9-1015-250-10

M120 Mortar Ground Mounted

M121 Mortar in M113A3

20-1

FOUO

Nomenclature: M934A1

Name: 120mm High Explosive (HE) Cartridge

Capability: Destroy personnel, and light materiel targets. Description: The M934A1 120mm High Explosive cartridge with the M734A1 Multi-Option Fuze (MOF) is designed for use with the M120, 120mm Towed Mortar System and the M121, Carrier Mortar System. It is used against personnel and materiel providing both fragmentation and blast effects. It consists of a Steel Shell Body with Composition B fill, a plastic split-ring Obturator, and an aluminum M31 Fin Assembly. The propulsion system utilizes the M1020 Ignition Cartridge and four horseshoe-shaped, water-resistant M234 Propelling Charges. Characteristics: Range Maximum Rate of Fire Sustained Rate of Fire Cartridge Weight Cartridge Length Fuze Explosive Reliability Probable Error -

Maximum: 7,200m Minimum: 200m 15 rounds/min (first minute) 6 rounds/min 30.17 lbs. 27.99 in. M734A1 MOF Composition B 97% at 90% confidence Range: 1.5% Deflection: 1.0%

Contractor / Status / Improvements / Special Equipment: Contractor - GD-OTS Canada (formerly SNC TEC) for Load, Assemble and Pack (LAP) L3/KDI, Cincinnati, OH for M734A1 MOF Status Production/Deployment Management: PEO AMMO & PM-CAS; Picatinny Arsenal, NJ Technical Order: TM-43-0001-28

Comp B HE Fill

M1020 Ignition Cartridge

M734A1 MO Fuze

M31 Fin

Obturating Ring

M234 Prop Charge

20-2

FOUO

Nomenclature: M934A2

Name: 120mm HE Insensitive Munition (IM) Cartridge

Capability: Destroy personnel, bunker and light materiel targets. Description: The 120mm M934A2 High Explosive Insensitive Munition cartridge with the M734A1 MultiOption Fuze (MOF) is designed for use with the M120, 120mm Towed Mortar System and the M121, Carrier Mortar System. It will provide enhanced-insensitive munitions (IM) performance against unplanned external thermal and shock stimuli such as Fast and Slow Cook-Off, Sympathetic Detonation, and Bullet/Fragment Impact. It will be used against personnel, bunkers and materiel providing both fragmentation and blast effects. Characteristics: Range -

Maximum: 7,200m Minimum: 300m Probable Error Range: 1.5% Deflection: 1.0% Effectiveness 50% Improvement over 4.2” M329A1 HE Reliability 0.97 at 80% Confidence IM Performance Targets (Threshold / Objective): - Fast & Slow Cook-Off: Type V / Type IV - Sympathetic Detonation: Type III / Type II - Bullet Impact: Type V / Type IV - Fragment Impact: Type V / Type IV Maintains interfaces with standard M1020/M234 Propulsion System, M734A1 MOF, and M31 Fin Assembly. Fuze M734A1 MOF will utilize IM-enhanced PBXN-5 Booster and interfaces with M1064 Carrier ammunition storage racks Incorporate PA174 Monopack and new pallet configuration Contractor / Status / Improvements / Special Equipment: Contractor - L3/KDI, Cincinnati, OH for M734A1 MOF: GD-OTS, Scranton, PA for Shell Bodies Status The program is on hold until Common Mortar IM explosive solution is implemented. Management: PEO AMMO & PM-CAS; Picatinny Arsenal, NJ Technical Order: TM-43-0001-28

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FOUO

Nomenclature: M933A1

Name: 120mm High Explosive (HE) Cartridge

Capability: Destroy personnel, bunker and light materiel targets. Description: The M933A1 120mm High Explosive (HE) cartridge with the M783 Point Detonating/Delay (PD/DLY) Fuze is designed for use with the M120, 120mm Towed Mortar System and the M121, Carrier Mortar System. It is used against personnel, bunker and light materiel targets. It consists of a Steel Shell Body with Composition B fill, a plastic split-ring Obturator, and the aluminum M31 Fin Assembly. The propulsion system utilizes the M1020 Ignition Cartridge and four horseshoe-shaped, water-resistant M234 Propelling Charges. The M933A1 is similar to the M934A1 HE cartridge, except the M934A1 uses the M734A1 Multi-Option Fuze (MOF) for Mortars. Characteristics: Range Maximum Rate of Fire Sustained Rate of Fire Cartridge Weight Cartridge Length Explosive Fuze Reliability Probable Error -

Maximum: 7,200m Minimum: 200m 16 rounds/min (first minute) 4 rounds/min 30.2 lbs. 27.99 in. Composition B M783 PD/DLY 97% at 90% confidence Range: 1.5% Deflection: 1.0%

Contractor / Status / Improvements / Special Equipment: Contractor - GDOTS Canada, LAP; Pocal Industries, Scranton, PA for M1020 Ign. Ctg.; L3/KDI, Cincinnati, OH for M783 PD/DLY Fuze; GD-OTS Scranton, PA for Shell Bodies Status Production/Training/Development Management: PEO AMMO & PM-CAS; Picatinny Arsenal, NJ Technical Order: TM-43-0001-28

M783 PD Fuze Comp B HE Fill

M1020 Ignition Cartridge

Obturating Ring

M31 Fin

M234 Prop Charge

20-4

FOUO

Nomenclature: M929

Name: 120mm White Phosphorus (WP) Smoke Cartridge

Capability: The M929 is designed for screening, obscuration, and spotting missions. Description: The M929 provides smoke obscuration and spotting for area targets. The cartridge is filled with 5 lbs. of WP. When the fuze functions, it detonates the burster, which disperses the felt pads which are soaked with WP. The smoke obscuration is generated by a spontaneous reaction between the WP and oxygen. Two configurations are in inventory: M929 with M734A1 MultiOption (MO) Fuze and XM929 with M745 point detonating (PD) fuze. Characteristics: Range -

Maximum: 7,200m Minimum: 200m Maximum Rate of Fire 16 rounds/min (first minute) Sustained Rate of Fire - 4 rounds/min Cartridge Weight 30 lbs. Cartridge Length 28 in. Fill 5 lbs. White Phosphorous (WP) Fuze M734A1 MO or M745 PD Fuze Burn Time Approximately 6.5 Minutes Reliability 97% at 80% confidence level Probable Error in Range (PEr) at max range - 2 .0 % Required - PEr 1.0% Required Ballistically similar to the M934A1 HE, M930/M983 Illums and M931 FRP Effectiveness Provides twice the obscuration effectiveness of the 4.2” M328A1 WP cartridge Contractor / Status / Improvements / Special Equipment: Contractors - PM CAS System Integration; Pine Bluff Arsenal, Arkansas for Load, Assemble and Pack Status Production/Deployment Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM-43-0001-28 M234 Propelling Charges

White Phosphorus Felt

M734A1 MOFM (M929) M745 PD Fuze (XM929)

M31 Fin Ignition Cartridge*

Obturator Ring

M86 Burster

Fuze Booster (Comp B)

(Comp B)

20-5

FOUO

Nomenclature: M930

Name: 120mm Visible Light (VL) Illuminating Cartridge

Capability: Used as signaling and to illuminate target areas to facilitate adjustment of fire and allow infantry to engage enemy equipment and Personnel. Description: The M930 cartridge is a fin stabilized, mortar cartridge that consists of a M776 Mechanical Time Superquick (MTSQ) fuze, a steel 2-piece shell body that contains the payload (parachute and canister), and a fin assembly that contains the ignition cartridge and propelling charges. The payload is base ejected and upon ignition produces visible light illumination. This visible light illumination allows for monitoring of enemy activities and adjustment of fire at greater observation distances during night operations. It also provides a means for day/night signaling. It is particularly useful in combined operations with allies who may not have night vision devices (NVDs). This round illuminates to the full range of the M934A1 high explosive round, which allows adjustment of fire at any distance out to the maximum range, and provides a significant increase in illumination intensity and effectiveness over the 4.2-inch cartridge that it replaces. The M930 is fired from the M120 Towed and M121 Carrier-Mounted mortar systems. Characteristics: Range Maximum Rate of Fire Sustained Rate of Fire Cartridge Weight Cartridge Length Fuze VL Illumination Burn Time Reliability Probable Error -

Maximum: 6,675m Minimum: 200m 16 rounds/min (first minute) 4 rounds/min 30.6 lbs. 27.8 in. M776 MTSQ Fuze 1.0M candela 50 to 60 seconds 95% at point estimate Range: 2% Deflection: 1%

Contractor / Status / Improvements / Special Equipment: Contractors - PM CAS System Integration; Pine Bluff Arsenal, Arkansas for LAP Status Production/Deployment Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM-43-0001-28 Front Body Expelling Chg Assembly

M776 MTSQ Fuze

Canister Loading Assembly

M234 Propelling Charges Rear Body M1020 Ignition Cartridge

Parachute Assembly

20-6

M31 Fin Assembly

FOUO

Nomenclature: M983

Name: 120mm Infrared (IR) Illuminating Cartridge

Capability: Used to illuminate target areas to facilitate adjustment of fire and allow infantry with night vision devices to engage enemy equipment and Personnel. Description: The M983 cartridge is a fin stabilized, mortar cartridge that consists of a M776 Mechanical Time Superquick (MTSQ) fuze, a steel 2-piece shell body that contains the payload (parachute and canister), and a fin assembly that contains the ignition cartridge and propelling charges. The payload is base ejected and upon ignition produces infrared (IR) illumination. This infrared light illumination allows for monitoring of enemy activities and adjustment of fire at greater observation distances during night operations. The advantage of the infrared over conventional illumination is that there is minimal visible light. This reduces the possibility of exposing forward friendly troop positions while also allowing covert adjustment of fire at greater observation distances through use of passive Night Vision Devices (NVDs). This round illuminates to the full range of the M934A1 high explosive round, which allows adjustment of fire at any distance out to the maximum range. The M983 cartridge is ballistically similar to the M930 visible light illuminating cartridge, except for the chemical composition of the illuminating material, and provides a field of view equal or greater to that of the M930 visible light cartridge. The M983 is fired from the M120 Towed and M121 Carrier-Mounted mortar systems. Characteristics: Range Maximum Rate of Fire Sustained Rate of Fire Burn Time IR Illumination Cartridge Weight Cartridge Length Fuze -

Maximum: 6,675m Minimum: 200m 16 rounds/min (first minute) 4 rounds/min 50 to 60 seconds 75 watts/steradian 30.6 lbs. Probable Error - Range: 2% 27.8 in. Deflection: 1% M776 MTSQ Fuze Reliability - 95% at 90% confidence level

Contractor / Status / Improvements / Special Equipment: Contractors - PM CAS System Integration; Pine Bluff Arsenal, Arkansas for LAP Status Production/Deployment Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM-43-0001-28 Expelling Chg Assembly

M776 MTSQ Fuze

Front Body

Rear Body

M234 Propelling Charges

Canister Loading Assembly

20-7

Parachute Assembly

M1020 Ignition Cartridge

M31 Fin Assembly

FOUO

Nomenclature: M931

Name: 120mm Full Range Practice Cartridge (FRPC)

Capability: FRPCs are used when training crews and indirect fire teams (less expensive than service ammunition) or when the use of service ammunition is restricted. The M931 is a training round that can be used when firing M120 and M121 mortars. Description: This Cartridge is a full-range practice cartridge for use in the 120mm, M120 and M121 Battalion Mortar Systems. It provides realistic training for 120mm Mortar crews at reduced costs. The M931 is ballistically similar to the M934A1 HE cartridge. It will match the M934A1 in size and, shape. The M931 FRPC is equipped with M781 PD Practice Fuze, a facsimile of the M734A1 Multi-Option Fuze (MOF). The M781 PD Fuze produces a flash, bang and smoke signature that provides audio/visual feedback to the mortar crew and forward observer. The M931 FRPC will not exceed 75% of the unit production cost of the M934A1 Cartridge. Characteristics: Range Maximum Rate of Fire Sustained Rate of Fire Cartridge Weight Cartridge Length Fuze Probable Error Reliability -

Maximum: 7,200m Minimum: 200m 15 rounds/min (first minute) 6 rounds/min 30.82 lbs. 27.99 in. M781 PD Fuze Range: 1.5% Deflection: 1% 97% at 80% confidence level

Contractor / Status / Improvements / Special Equipment: Contractors - GD-OTS, Canada for Load, Assemble and Pack; Pocal Industries, Scranton, PA for Practice Fuze; GD-OTS Scranton, PA for Shell Bodies Status Production/Training/Deployment Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM-43-0001-28 Fuze Adapter M31 Fin

Shell Body

M781 PD FUZE

M1020 Ignition CTG

Center Vent Tube

M233 Prop Charges

20-8

FOUO

Nomenclature: M224

Name: 60mm Mortar

Capability: Provide short -range indirect fire support to airborne, air assault, light infantry, mountain and special operations forces. Description: The M224 60mm mortar is a muzzle-loaded, smooth-bore high-angle weapon used for close-in support of ground troops. It can be fired in the conventional mode or handheld mode. It can be drop-fired or trigger-fired. The M224 provides air assault, airborne, ranger, and light infantry rifle companies with an effective, efficient, and flexible weapon. The inherent limitations of a light mortar (short-range and small-explosive charge) can be minimized by careful planning and a thorough knowledge of its capabilities. The mortar can be fired accurately with or without a fire direction center. The short minimum range of the M224 makes the mortar well suited for close protective fires against an assaulting enemy, for block-to-block fighting in cities, and combat over close terrain with restricted visibility. The M224 can be employed in several different configurations. The lightest weighs about 18 pounds; the heaviest weighs about 46.5 pounds. Each round weighs about 4 pounds. Characteristics: Length -

Weight Crew Max. Range Min. Range Rate of Fire -

Ammunition -

M225 Cannon Assembly (14.4 lbs.) M8 Auxiliary Baseplate (3.6 lbs.) M170 Bipod Assembly (15.2 lbs.) M7 Baseplate (14.4 lbs.) 47 lbs. (conventional); 18 lbs. (handheld) 3 3,490 m (conventional); 1,340 m (handheld) 70 m (conventional); 75 m (handheld) (dependent on ammunition round fired) Max: 18-30 per rounds minute for 1 to 4 min Sustained: 8 to 20 rounds per minute indefinitely High-explosive/multi-option fuze, high- explosive point detonating fuze, white phosphorous/smoke, and illumination 40 in

Contractor / Status / Improvements / Special Equipment: Contractor - Multiple Status Production Management: PEO AMMO & PM-Mortars; Picatinny Arsenal, NJ Technical Order: TM 9-1010-223-10 M242 60mm Mortar, Hand Held

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Nomenclature: M720A1

Name: 60mm High Explosive (HE) Cartridge

Capability: Provide medium weapon, high-angle organic indirect fire support to the maneuver unit commander. Destroy personnel and materiel targets out to over 3,489m and as close as 70 meters with a killing radius of 30 meters. Description: The M720A1 60mm High Explosive cartridge with Multi-Option Fuze is designed for use with the M224 lightweight company mortar system in all light infantry battalions including Airborne, Air Assault and Ranger. It is used against personnel and materiel providing both fragmentation and blast effects. The M720A1 incorporates several new design features which improves the response to unplanned stimuli over the previous M720. This was achieved through a system level approach during its redesign. Upgrades from the previous version include a new explosive fill (PAX-21), fuze, shell body, fuze adapter and propellant charge. Characteristics: Range Maximum Rate of Fire Sustained Rate of Fire Cartridge Weight Cartridge Length Body Color Explosive Fuze Reliability -

Maximum: 3,489m Minimum: 70m 30 rounds/min for 4 min 20 rounds/min 3.7 lbs. 14.84 in. Alloy Steel Olive Drag 0.79 PAX-21 M734A1 MO Fuze 98%

Contractor / Status / Improvements / Special Equipment: Contractors - Day & Zimmermann Inc., Kansas AAP for LAP; Medico Industries, Wilkes Barre, PA for Shell Bodies; L3/KDI, Cincinnati, OH for M734A1 fuze; GDOTS-Canada, awarded LAP contract for FY06 & future buys Status Production/Deployment Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM 9-1010-223-10 PBX-N5 Booster PAX-21 HE Fill

M734A1 MO Fuze

M235 Prop Charge

Fuze M27 Fin HF-1 Body M702 Ignition Cartridge

20-10

FOUO

Nomenclature: M768 Name: 60 mm High Explosive (HE) Cartridge Capability: Provide medium weapon, high-angle organic indirect fire support to the maneuver unit commander. Destroy personnel and materiel targets out to over 3,400m and as close as 70 meters with a killing radius of 30 meters. Description: The 60mm Mortar High Explosive/Point Detonating/Delay (HE/PD/DLY) cartridges are designed for use with the M224 lightweight company mortar system (LWCMS) in all light infantry battalions including Airborne, Air Assault and Ranger. It will use the new M738 dual safety, point detonating/delay fuze, tail assembly, and high fragmentation steel projectile body. This round will be used primarily in training because it is significantly less expensive than the M720A1, the preferred warfighting round. However, the M768 will be lethal and can be used in combat. Characteristics: Range Maximum Rate of Fire Sustained Rate of Fire Cartridge Weight Cartridge Length Body Color Explosive Fuze -

Maximum: 3,489m Minimum: 70m 30 rounds/min (first minute) 20 rounds/min 3.59 lbs. Reliability - 98% 14.84 in. Probable Error - Range: 1.5% of mean range Alloy Steel - Deflection: 1% of mean range Olive Drab 0.79 lb PAX-21 M783 PD Fuze

Contractor / Status / Improvements / Special Equipment: Contractors - Day & Zimmermann Inc., Kansas AAP for LAP; Medico Industries, Wilkes Barre, PA for Shell Bodies; L3/KDI, Cincinnati, OH for M734A1 fuze; GDOTS-Canada, awarded LAP contract for FY06 & future buys Status Production/Deployment Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM 9-1010-223-10 PBX-N5 M768 w/M783 Booster P PAX-21 HE Fill M235 Prop Charge e M27 Fin n

20-11

Fuze Adapter HF-1 Body M702 Ignition Cartridge

FOUO

Nomenclature: M888 Name: 60mm High Explosive (HE) Cartridge Capability: Provide medium weapon, high-angle organic indirect fire support to the maneuver unit commander. Destroy personnel and materiel targets out to over 3,400m and as close as 70 meters with a killing radius of 30 meters. Description: The M888 has the same body and propulsion system as the M720 HE/MO but uses the M935 Point Detonating Fuze. It is 14.7 inches in length and weighs 3.9 pounds. The M935 PD Fuze is a modification of the M567 Fuze and provides reversible selection between superquick and delay modes. The fuze contains a safety wire. The cartridge was last loaded, assembled and packed at Milan Army Ammunition Plant. The M888 was developed by ARDEC, and type classified in Mar 1983. The Joint Munitions Command manages the M888, which is purchased only by the US Marine Corps. Characteristics: Range Maximum Rate of Fire Sustained Rate of Fire Cartridge Weight Cartridge Length Body Color Explosive Fuze Reliability Probable Error -

Maximum: 3,490m Minimum: 70m 30 rounds/min for 4 min 20 rounds/min 3.75 lbs. 14.738 in. Alloy Steel Olive Drab w/yellow markings 0.79 lb. PAX-21 M935 PD Fuze 88% at 90% confidence level C.L. Range: 75 meters max at charge 4

Contractor / Status / Improvements / Special Equipment: Contractors - GDOTS-Canada awarded FY06 LAP contract FY08 and future buys on Milan Facility Use Contract. Status Production/Deployment Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM 9-1010-223-10

M702 Ignition Cartridge

M27 Fin

Obturating Ring

M935 PD Fuze

M204 Propellant Charge

20-12

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Nomenclature: M722A1

Name: 60mm White Phosphorus (WP) Smoke Cartridge

Capability: The M772A1 is designed for screening and obscuration missions. Description: The M722A1 60mm Smoke cartridge is designed for use with the M224, 60mm Mortar System as a spotting/marking round. The steel projectile is bulk loaded with white phosphorous. When the fuze functions, it detonates the M85 burster, which ruptures the projectile and disperses the white phosphorus. The M722A1 replaced the M745 mechanical point-detonating fuze with the reliable, safe, and cost effective electronic M783 Point Detonating (PD) and Delay (DLY) fuze Characteristics: Range Maximum Rate of Fire Sustained Rate of Fire Cartridge Weight Cartridge Length Body Color Fill Fuze Reliability Probable Error -

Maximum: 3200m Minimum: 300m 30 rounds/min (first minute) 20 rounds/min 3.7 lbs. 14.84 in. Steel Light Green w/red marking and 1 yellow band Bulk-filled with WP M783 PD/DLY Fuze 98% @ 90% confidence level C.L. Range: 1.5% Deflection: 2.5 mils

Contractor / Status / Improvements / Special Equipment: Contractors - PM CAS System Integration Pine Bluff Arsenal, Arkansas for Load, Assemble and Pack Status Production/Deployment Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM 9-1010-223-10

M783 PD/DLY Fuze Obturating Ring M27 Fin M204 Prop Charge

M702 Ignition Cartridge

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FOUO

Nomenclature: M721

Name: 60mm Visible Light (VL) Illuminating Cartridge

Capability: Used to illuminate target areas to facilitate adjustment of fire and allow infantry to engage enemy equipment and Personnel. Description: The M721 cartridge is a fin stabilized, mortar cartridge that consists of a M776 Mechanical Time Superquick (MTSQ) fuze, a thin wall steel body tube and aluminum tail cone that contains the payload (parachute and canister), and a fin assembly that contains the ignition cartridge and propelling charges. The payload is base ejected and upon ignition produces visible light illumination. This visible light illumination allows for monitoring of enemy activities and adjustment of fire at greater observation distances during night operations. It also provides a means for day/night signaling. It is particularly useful in combined operations with allies who may not have night vision devices (NVDs). It Provides 325,000 candelas of Visible Light. The M721 is fired from the M224 Lightweight Mortar System and is ballistically similar to the 60mm M767 IR Illuminating cartridge. Characteristics: Range Maximum Rate of Fire Sustained Rate of Fire Burn Time VL Illumination Cartridge Weight Cartridge Length Color Fill Fuze Reliability Probable Error -

Maximum: 3,200m Minimum: 300m 30 rounds/min (first minute) 20 rounds/min 40 seconds 325,000 candela 3.79 lbs. 16.83 in. White w/black markings Bulk-filled with WP M776 MTSQ Fuze 95% @ 90% confidence level (CL) Range: 1.5% Deflection: 2.5 mils

Contractor / Status / Improvements / Special Equipment: Contractors - PM CAS System Integration; Pine Bluff Arsenal, Arkansas for LAP Status Production/Deployment Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM 9-1010-223-10 M27 Fin

M702 Ignition Cartridge

M204/M235 Propelling Charges

Canister Loading Assembly

Parachute Tail Cone Assembly Assembly

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M776 MTSQ Fuze

Body Tube Assembly

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Nomenclature: M767

Name: 60mm Infrared (IR) Illuminating Cartridge

Capability: Used to illuminate target areas to facilitate adjustment of fire and allow infantry with night vision devices to engage enemy equipment and Personnel. Description: The M767 cartridge is a fin stabilized, mortar cartridge that consists of a M776 Mechanical Time Superquick (MTSQ) fuze, a thin wall steel body tube and aluminum tail cone that contains the payload (parachute and canister), and a fin assembly that contains the ignition cartridge and propelling charges. The payload is base ejected and upon ignition produces infrared (IR) illumination. The advantage of the infrared over conventional illumination is that there is minimal visible light. This reduces the possibility of exposing forward friendly troop positions while also allowing covert adjustment of fire at greater observation distances through use of passive Night Vision Devices (NVD). The M721 is fired from the M224 Lightweight Mortar System and is ballistically similar to the M721 visible light illuminating cartridge, except for the chemical composition of the illuminating material. Characteristics: Range Maximum Rate of Fire Sustained Rate of Fire Burn Time IR Illumination Cartridge Weight Cartridge Length Fill Color Fuze Reliability -

Maximum: 3,489m Minimum: 300m 30 rounds/min (first minute) 20 rounds/min 40 seconds 75 watts/steradian 3.75 lbs. 16.85 in. Probable Error - Range: 1.5% Bulk-filled with WP - Deflection: 2.5 mils White w/black markings and 1 orange band M776 MTSQ Fuze 95% @ 90% confidence level C.L.

Contractor / Status / Improvements / Special Equipment: Contractors - PM CAS System Integration; Pine Bluff Arsenal, Arkansas for LAP Status Production/Deployment Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM 9-1010-223-10 M204/M235 Propelling Charges

Canister Loading Assembly

M776 MTSQ Fuze

M27 Fin

M702 Parachute Ignition Tail Cone Assembly Cartridge

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Body Tube Assembly

FOUO

Nomenclature: M769

Name: 60mm Full Range Practice Cartridge (FRPC)

Capability: The M769 is a low-cost, full range, practice round that will replace a percentage of the standard HE rounds used in 60mm mortar training. Description: The M769 60mm FRPC is designed for use with the M224 lightweight company mortar system (LWCMS) in all light infantry battalions including Airborne, Air Assault and Ranger. It consists of a M775 point detonating practice fuze, a steel body that approximates the shape of the 60mm HE service round; and a fin assembly, ignition cartridge and propelling charge that make up the propulsion system. The M769 has been designed to provide the user with realistic training at a fraction of the cost. It is identical in shape, size and weight to the M720/M720A1 HE cartridges. The flash, bang and smoke signature provided by the M775 fuze is channeled to exhaust holes in the rear of the cartridge through the use of a center vent tube. The signature allows the user to adjust fire as they would for the HE cartridge. Characteristics: Range Maximum Rate of Fire Sustained Rate of Fire Signature Cartridge Weight Cartridge Length Color Fuze Reliability Probable Error -

Maximum: 3,500m Minimum: 70m 30 rounds/min (first minute) 15 rounds/min Visible from 2000m 3.82 lbs. 14.88 in. Blue w/white markings M775 Practice Fuze 97% Range: 1.5% Deflection: 2.5 mils

Contractor / Status / Improvements / Special Equipment: Contractors - Medico industries, Wilkes Barre, PA, for Shell Bodies DZI, Camden, AR, awarded LAP contract for FY06S & future buys Status Production/Deployment Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM 9-1010-223-10 M775 Practice Fuze

M27 Fin Assembly

Center Vent Tube

M235 Propelling Charge

M702 Ignition Cartridge

M720 Projectile Body Obturator Ring

Exhaust Holes (4)

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Nomenclature: XM1061

Name: 60 mm Enhanced Fragmentation Mortar Cartridge

Capability: Provide medium weapon, high-angle organic indirect fire support to the maneuver unit commander. Destroy personnel and materiel targets out to over 3,400m and as close as 70 meters with a killing radius of 30 meters. Description: The XM1061 EF Evaluation Program is currently type classified and provides enhanced lethality and effectiveness as compared to the US M720 / M720A1 HE rounds. The XM1061 cartridges consist of a fuze, a fuze adapter, a HE container loaded with about 254 grams of PBXN-110 explosive. Characteristics: Range Maximum: 3,657m Minimum: 61m Maximum Rate of Fire 30 rounds/min (first minute) Sustained 15 rounds/min Cartridge Weight 4 lbs. Cartridge Length 16.95 in. Fill PBSN-110 Explosive Fuze M743A1 Reliability 98% Probable Error Range: 1.5% of mean range Deflection: 1% of mean range Contractor / Status / Improvements / Special Equipment: Contractors - ATK, Plymouth, MN Status Production Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM 9-1010-223-10

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Nomenclature: M252

Name: 81mm Mortar

Capability: Provide long-range indirect fire support to airborne, air assault and light infantry across the entire battalion front with sufficient range to engage targets out to the limit of the battalion zone of influence. Description: The M252 81mm medium weight mortar is an American smooth bore, muzzle-loading, high-angle-of-fire weapons used for long-range indirect fire support to light Infantry, air Assault, and airborne units across the entire front of a battalion of influence. In the US Army and US Marine Corps, it is normally deployed in the mortar platoon of an infantry battalion. The M252 is an adaptation of the standard British mm mortar.

Characteristics: Length Weight Crew Max. Range Min. Range Rate of Fire -

Ammunition -

50 in. (1.27m) 85.8 lbs. 3 5,608m 83m (dependent on ammunition round fired) Max: 25-30 per rounds minute for 2 min Sustained: 8 to 15 rounds per minute A variety of NATO-standard ammunition, including high-explosive, red phosphorous/smoke, and Illumination

Contractor / Status / Improvements / Special Equipment: Contractor - Multiple Status - Production Management: PEO AMMO & PM-Mortars; Picatinny Arsenal, NJ Technical Order: TM 9-1015-249-10

M252 81mm Mortar

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Nomenclature: M821A1/M889A1

Name: 81mm High Explosive (HE) Cartridge

Capability: Provide medium weapon, high-angle organic indirect fire support to the maneuver unit commander. Destroy personnel and light materiel targets out to over 5,850 meters and as close as 70 meters with a killing radius of 30 meters. Description: The 81mm M821A1 / M889A1 Cartridges consist of a fuze, a HF-1 steel projectile body loaded with approximately 2 lbs. of COMP B explosive, a plastic obturating ring, a M24 Fin (with canted blades), a M220 Propelling Charge (with 4 each horseshoe shaped increments), and a M299 Ignition Cartridge (with percussion primer). The cartridges are identical, except for the fuze. The M821A1 Cartridge is assembled with the M734 Multi-option (MO) Fuze, while the M889A1 Cartridge is assembled with the M935 Point Detonating (PD) Fuze. The M734 Fuze is capable of functioning proximity (PRX), near surface burst (NSB), impact (IMP) or delay (DLY). The M935 Fuze is capable of functioning superquick or with 0.05 second delay, on impact. Characteristics: Range Maximum Rate of Fire Sustained Rate of Fire Cartridge Weight Cartridge Length Fill Fuze Reliability Probable Error -

Maximum: 5,850m Minimum: 70m 30 rounds/min (first minute) 15 rounds/min 9.03 lbs. 19.6 in. 2 lbs. COMP B Explosive with a ball bearing matrix fragmentation body M734 MO Fuze (M821A1) or M935 PD Fuze (M889A1) 98% Range: < 1% at ranges >= 1,500m < 15 meters at ranges < 1,500m Deflection: < 15 meters

Contractor / Status / Improvements / Special Equipment: Contractors - New contract being procured Status Production/Deployment M889A1 only Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM 9-1015-249-10 Comp B Filler M220 Propelling Charges

M24 Fin

M734Multi-Option Fuze (M821A1) or M935 PD Fuze (M889A1)

M299 Ignition Cartridge

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Nomenclature: M821A2/M889A1E1

Name: 81mm High Explosive (HE) Cartridge

Capability: Provide medium weapon, high-angle organic indirect fire support to the maneuver unit commander. Destroy personnel and light materiel targets out to over 5,859 meters and as close as 70 meters with a killing radius of 30 meters. Description: The 81mm M821A2 / M889A1E1 Cartridges consist of a fuze, a HF-1 steel projectile body loaded with approximately 2 lbs. of COMP B explosive, a plastic obturating ring, a M24 Fin (with canted blades), a 4-increment M220 Propelling Charge, and a M299 Ignition Cartridge (with percussion primer). The cartridges are identical, except for the fuze. The M821A2 Cartridge is assembled with the M734A1 Multi-option (MO) Fuze, while the M889A1E1 Cartridge is assembled with the M783 Point Detonating / Delay (PD/DLY) Fuze. The M734A1 Fuze is capable of functioning proximity (60/81 PRX), impact (IMP) or delay (DLY). The M783 Fuze is capable of functioning on impact (IMP) or delay (DLY) and has simulated proximity mode setting (for training purposes). Characteristics: Range Maximum Rate of Fire Sustained Rate of Fire Cartridge Weight Cartridge Length Fill Fuze Reliability Probable Error -

Maximum: 5,859m Minimum: 70m 30 rounds/min (first minute) 15 rounds/min 9.42 lbs. 19.6 in. 2 lbs. COMP B M743A1 MO Fuze (M821A2) or M783 PD/DLY Fuze (889A1E1) 98% Range: < 1% at ranges >= 1,500m < 15 meters at ranges < 1,500m Deflection: < 15 meters

Contractor / Status / Improvements / Special Equipment: Contractors - New contract being procured Status Production/Deployment Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM 9-1015-249-10

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Nomenclature: M821A2E1/XM1058

Name: 81mm High Explosive (HE) Cartridge

Capability: Provide medium weapon, high-angle organic indirect fire support to the maneuver unit commander. Destroy personnel and light materiel targets out to over 5,900 meters and as close as 70 meters with a killing radius of 30 meters. Description: The 81mm M821A2E1 / XM1058 Cartridges consist of a fuze, a threaded plastic fuze adapter, a HF-1 steel projectile body loaded with approximately 2 lbs. of an IM explosive, a plastic obturator ring, a M24 Fin (with canted blades), a 4-increment M220 Propelling Charge, and a M299 Ignition Cartridge (with percussion primer). The cartridges are identical, except for the fuze. The M821A2E1 Cartridge is assembled with the M734A1 Multi-option (MO) Fuze, while the XM1058 Cartridge is assembled with the M783 Point Detonating / Delay (PD/DLY) Fuze. The M734A1 Fuze is capable of functioning proximity (60/81 PRX), impact (IMP) or delay (DLY). The M783 Fuze is capable of functioning on impact (IMP) or delay (DLY) and has simulated proximity mode setting (for training purposes). Characteristics: Range Maximum Rate of Fire Sustained Rate of Fire Cartridge Weight Cartridge Length Fill Fuze Reliability Probable Error -

Maximum: 5,859m Minimum: 70m 30 rounds/min (first minute) 15 rounds/min 9.42 lbs. 19.6 in. 2 lbs. IM Explosive M743A1 MO Fuze (M821A2E1) or M873 PD/DLY Fuze (XM1085) 98% Range: < 1% at ranges >= 1,500m < 15 meters at ranges < 1,500m Deflection: < 15 meters

Contractor / Status / Improvements / Special Equipment: Contractors - New contract being procured Status Production/Deployment Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM 9-1015-249-10

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Nomenclature: M819

Name: 81mm Red Phosphorous (RP) Cartridge

Capability: The M772A1 is designed for screening, marking, and obscuration missions. Description: The M819 Cartridge is a fin stabilized thin wall steel body tube containing 28 palletized red phosphorous (RP) wedges; it uses the M772 Mechanical Time Super Quick Fuze (MTSQ) fuze. After a set time delay, the RP wedges are ejected and dispersed on the target to quickly produce an obscuring smoke screen or marking round. A full screen can be developed with 3 rounds as opposed to 15 rounds with the M375 series WP cartridge. Provides 5 times the obscuration effectiveness of the 81mm M375 WP cartridge Characteristics: Range Maximum Rate of Fire Sustained Rate of Fire Cartridge Weight Cartridge Length Fill Fuze Reliability Probable Error -

Maximum: 5,859m Minimum: 70m 30 rounds/min (first minute) 15 rounds/min 10.37 lbs. 19.6 in. 28 pelletized red phosphorous (RP) wedges M772 MTSQ Fuze 98% at 90 % confidence level (CL) Range: < 1% at ranges >= 1,500m < 15 meters at ranges < 1,500m Deflection: < 15 meters

Contractor / Status / Improvements / Special Equipment: Contractors - PM CAS System Integration; Pine Bluff Arsenal, AK for Pellet Production and LAP Pocal, Scranton, PA for M752A1 Ignition Cartridge Status Production/Deployment Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM 9-1015-249-10 M772 Mechanical Time Super Quick Fuze

Projectile

RP Felt & Pellets

M218 Propelling Charge

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M28 Fin Assembly

M752A1 Ignition Cartridge

FOUO

Nomenclature: M853A1

Name: 81mm Visible Light (VL) Illuminating Cartridge

Capability: Used to illuminate target areas to facilitate adjustment of fire and allow infantry to engage enemy equipment and Personnel. Description: The M853A1 cartridge is a fin stabilized, mortar cartridge that consists of a M772 Mechanical Time Superquick (MTSQ) fuze, a thin wall aluminum body tube and aluminum tail cone that contains the payload (parachute and canister), and a fin assembly that contains the ignition cartridge and propelling charges. The payload is base ejected and upon ignition produces visible light illumination. This visible light illumination allows for monitoring of enemy activities and adjustment of fire at greater observation distances during night operations. It also provides a means for day/night signaling. It is particularly useful in combined operations with allies who may not have night vision devices (NVDs). This round illuminates to the full range of the HE round, which allows adjustment of fire at any distance out to the maximum range. The M853A1 is fired from the M252 Lightweight Mortar System and is ballistically similar to the 81mm M816 IR Illuminating cartridge. Characteristics: Range Maximum Rate of Fire Sustained Rate of Fire Cartridge Weight Cartridge Length Burn Time VL Illumination Fuze Reliability Probable Error -

Maximum: 4900m Minimum: 300m 30 rounds/min (first minute) 15 rounds/min 9.02 lbs. 25.5 in. 50 - 60 seconds 600,000 candela M772 MTSQ Fuze 95% at 90% confidence level Range: 1% Deflection: < 15 meters at all ranges

Contractor / Status / Improvements / Special Equipment: Contractors - PM CAS System Integration; Pine Bluff Arsenal, AK for LAP Status Production/Deployment Management: Joint Munitions Command Technical Order: TM 9-1015-249-10 M29 Fin

M219 Prop Charge

M752A1 Ignition Cartridge

VL Candle Assembly

Parachute Assembly

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M772 MTSQ Fuze

Body Tube Assembly

FOUO

Nomenclature: M816

Name: 81mm Infrared (IR) Illuminating Cartridge

Capability: Used to illuminate target areas to facilitate adjustment of fire and allow infantry with night vision devices to engage enemy equipment and Personnel. Description: The M816 cartridge is a fin stabilized, mortar cartridge that consists of a M772 Mechanical Time Superquick (MTSQ) fuze, a thin wall aluminum body tube and aluminum tail cone that contains the payload (parachute and canister), and a fin assembly that contains the ignition cartridge and propelling charges. The payload is base ejected and upon ignition produces infrared (IR) illumination. It is designed to provide infrared illumination which cannot be detected by the human eye. This reduces the possibility of exposing forward friendly troop positions while also allowing convert adjustment of fire at greater observation distances through use of passive night vision devices (NVD). This round illuminates to the full range of the HE round, which allows adjustment of fire at any distance out to the maximum range. The M816 cartridge is ballistically similar to the M853A1 visible light illuminating cartridge, except for the chemical composition of the illuminating material, and provides a field of view equal or greater to that of the M853A1 visible light cartridge. The M816 is fired from the M252 Improved Mortar System. Characteristics: Range Maximum Rate of Fire Sustained Rate of Fire Cartridge Weight Cartridge Length Burn Time IR Illumination Fuze Reliability Probable Error -

Maximum: 4,925m Minimum: 1025m 30 rounds/min (first minute) 15 rounds/min 9.25 lbs. 25.4 in. 60 seconds 50 watts/steradian M772 MTSQ Fuze 95% at 90% confidence level Range: 1% Deflection: <15 meters at all ranges

Contractor / Status / Improvements / Special Equipment: Contractors - PM CAS System Integration; Pine Bluff Arsenal, AK for LAP Status Production/Deployment Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM 9-1015-249-10

M29 Fin

M752A1 Ignition Cartridge

M219 Propelling Charges

Canister Loading Assembly

Tail Cone Assembly

Parachute Assembly

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M772 MTSQ Fuze

Body Tube Assembly

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Nomenclature: M879

Name: Full Range Practice (FRPC) Cartridge

Capability: The M769 is a low-cost, full range, practice round that will replace a percentage of the standard HE rounds used in 70mm mortar training. Description: The M879 Full Range Practice Cartridge (FRPC) is a US developed improved practice rounds for use in the M252, improved 81mm, Mortar System. The practice cartridge provides realistic training in place of the M821 A1/M889 A1 High Explosive (HE) Cartridges at a cost savings of $95M. The M751 Point Detonating Practice Fuze simulates the M734 fuze and can be set, for training purposes, to the required fuze functioning mode for the fire mission. The M751 fuze used on this round detonates upon impact and produces a flash, bang, and smoke signature which gives the forward observer the ability to adjust fire. The M879 cartridge consists of a HE steel body with an inert concrete payload. The M879 is a full range training round for the 81mm M252 Mortar System. It simulates the 81mm, M821A1/M889A1 High Explosive (HE). Characteristics: Maximum Range Minimum Range Maximum Rate of Fire Sustained Rate of Fire Signature Cartridge Weight Cartridge Length Reliability Effectiveness -

5,600m 70m 30 rounds/min (first minute) 15 rounds/min Visible from 2000m 8.98 lbs. 19.55 in. 97% at 80% confidence Level Visual effect to allow adjustment from a range of 2500m

Contractor / Status / Improvements / Special Equipment: Contractors - Currently not in production Status Production/Deployment Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM 9-1015-249-10 M24 Fin Assembly

M299 Ignition Cartridge

Inert Filled Projectile Body

M220 Propelling Charge

Obturator Ring

20-25

M751 Practice Fuze

M734 Simulated Fuze Cover

FOUO

Nomenclature: XM784/XM785

Name: Electronic Time (ET) Fuze

Capability: The XM784/XM785 will be used with the 60mm, 81mm, and 120mm Illuminating Cartridges and the 81mm smoke cartridge. They will maintain ballistic similitude with all cartridges. The XM784/XM785 ET fuze will replace the M776/M772 fuzes respectively. These fuzes will be developed to improve timing accuracy and provide fuze safety to current requirements per MIL-STD-1316. Description: The XM784/XM785 ET fuze is a Material Change program to replace the M776/M772 fuzes respectively. These fuzes will be developed to improve timing accuracy and provide fuze safety to current requirements per MIL-STD-1316. The XM784 will be compatible with fielded and current developmental US 60mm and 120mm M721, M767, M930, and M983 mortar cartridges. The XM785 will be compatible with fielded and current developmental US 81mm M853A1, M816, and M819 mortar cartridges. The ET Fuze is an ACAT III Materiel Change Program. PEO Ammunition is the MDA. Characteristics: Safety Per MIL-STD-1316 (Dual Environ Safety) Cartridge Compatibility 60 mm (M721 Illum & M767 IR Illum) 81 mm (M853A1 Illum, M816 IR Illum & M819 RP Smoke) 20 mm (M930 Illum, M983 IR Illum) Hand Settable and Self Illuminating Reliability 98% Set Time 5 - 99.9 Seconds (0.1 Sec Increments) Will not Degrade Cartridge Range 20 Year Shelf Life (Controlled Environment) Minimum Arming Distance 00 Meters Contractor / Status / Improvements / Special Equipment: Contractors - ATK, Plymouth, Minnesota Status Production (Materiel Change), ACAT: III Management: U.S. Army TACOM-ARDEC Picatinny Arsenal, NJ Technical Order: TM 9-1015-249-10

XM784

XM785

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CHAPTER TWENTYONE 1 June 2009

ARMY ROCKETS AND MISSILES

FOR OFFICIAL USE ONLY

INTENTIONALLY LEFT BLANK

Nomenclature: M270A1

Name: Multiple Launch Rocket System (MLRS)

Capability: Provides all-weather counterfire and suppression of time sensitive point and area targets located in either open or complex urban terrain. Targets include Counter Fire, High Payoff Targets, Enemy Air Defense, Logistics Sites, Command and Control Sites, light materiel, and personnel targets at ranges from 15 to 300+km. Description: The MLRS M270A1 is a highly maneuverable tracked rocket/missile launcher based on the M270 stretched Bradley chassis weapons platform. The M270A1 program used remanufactured M993 Carriers and M269 Launcher Loader Modules, and incorporated the Improved Fire Control System (IFCS) and the Improved Launcher Mechanical System (ILMS) modifications. The M270A1 fires all rockets and missiles in the current and future Multiple Launch Rocket System (MLRS) Family of Munitions to include GMLRS rockets and Army Tactical Missile System (ATACMS) missiles. The new versions of the GMLRS and ATACMS munitions are specifically fitted with unitary warheads that minimize collateral damage. The launcher carries two Launch Pod/Containers (LP/Cs), each consisting of six MLRS rockets or one ATACMS missile. This highly automated self-loading and self-aiming system contains a fire control computer that integrates the vehicle and rocket launching operations. Without leaving the cab, the crew of three (driver, gunner, and section chief) can fire up to twelve MLRS rockets in less than 60 seconds. The M270A1 reduces launcher Operation and Support costs by 31% and improves slew time responsiveness by 60%. The M270A1 is transportable by C-5 and C-17. A Modular Launcher Communications System (MLCS) development program is ongoing to provide long-range communications, situational awareness and sensor to effects capability to each platform. Characteristics: Length Width Height Weight (combat loaded) Vehicle Range Speed Crew Munitions Range -

22.5 ft 9.8 ft 8.5 ft 54,500 lbs. 300 miles 40+ mph 3 15 to 300 + km

Contractor / Status / Improvements / Special Equipment: Contractor Lockheed Martin Missiles and Fire Control, Dallas, TX (Launcher / Munitions) British Aerospace Systems (Vehicle) Status Fielded Management: U.S. Army AMCOM, PEO Missiles and Space, PM Precision Fires Rocket and Missile Systems, Redstone Arsenal, AL Field Manual (FM): FM 6-60 has been renamed the FM 3-09.60.

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M270A1 Multiple Launch Rocket System (MLRS)

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Nomenclature: M142

Name: High Mobility Artillery Rocket System (HIMARS)

Capability: Provides all-weather counterfire and suppression of time sensitive point and area targets located in either open or complex urban terrain. Targets include Counter Fire, High Payoff Targets, Enemy Air Defense, Logistics Sites, Command and Control Sites, light materiel, and personnel targets at ranges from 15 to 300+km. Description: HIMARS is an air transportable, wheeled, indirect fire, rocket/missile system that is capable of firing all rockets and missiles in the current and future Multiple Launch Rocket System (MLRS) Family of Munitions (MFOM). The HIMARS system is deployable (roll on/roll off fully combat loaded) by C-130 and larger aircraft. The M142 uses on-board technical fire control and GPSaugmented position/navigation systems that are comparable to the M270A1 launcher. The M142 holds one Launch Pod Container/Guided Missile Launch Assembly (LPC/GMLA) containing six Guided MLRS (GMLRS)/MLRS rockets or one Army Tactical Missile System (ATACMS) missile. The new versions of the GMLRS and ATACMS munitions are specifically fitted with unitary warheads that minimize collateral damage. The M142 firing and reload times are comparable to the M270A1 launcher. Deployed units utilize the Low Signature Armored Cab-HIMARS (LSAC-H) variant for armored crew protection. An Improved Crew Protection (ICP) Armored Cab has completed development and will be cut into production and procured for retrofit across the entire fleet. A Modular Launcher Communications System (MLCS) development program is ongoing to provide long-range communications, situational awareness and sensor to effects capability to each platform Characteristics: Length 25.8 ft Width 8.3 ft Height 8.8ft Weight (Combat Loaded) - 35,000 lbs. Vehicle Range 300 miles Speed 58+ mph Crew 3 Munitions Range 15 to 300 + km Contractor / Status / Improvements / Special Equipment: Contractor - Lockheed Martin Missiles and Fire Control, Dallas, TX (Launcher / Munitions) British Aerospace Systems (Vehicle) Status Fielded Management: U.S. Army AMCOM, PEO Missiles and Space, PM Precision Fires Rocket and Missile Systems, Redstone Arsenal, AL Field Manual (FM): FM3-09.60

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M142 HIMARS firing a GMLRS

M142 HIMARS firing an ATACMS Missile

M142 HIMARS ICP Cab

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Nomenclature: M30, XM31

Name: Guided Multiple Launch Rocket System (GMLRS)

Capability: The GMLRS rocket gives the tactical commander an immediate, all-weather deep fire capability necessary to engage time critical targets out to 70 kilometers with increased lethality and Global Positioning System (GPS) accuracy, while minimizing collateral damage. Description: The M30 GMLRS Dual Purpose Improved Conventional Munitions (DPICM) rocket is an extremely accurate area suppression weapon possessing a warhead consisting of 404 DPICM grenades. It is inertially guided with GPS aided updates and is fired from the M270A1 or HIMARS launchers. M30 GMLRS DPICM is employed against lightly armored, stationary targets such as towed artillery, air defense units, and communication sites. The XM31 GMLRS Unitary rocket is a modified version of the current GMLRS DPICM rocket. It contains a single, 196 pound high explosive pre-formed fragmentation warhead with a tri-mode fuze (proximity, point detonate and delay) effective against critical point targets located in restricted terrain to ranges of 70km. It is inertially guided with GPS aided updates and is fired from the M270A1 or HIMARS launchers. An Urgent Material Release (UMR) version of the (M31) Unitary rocket, with a dual mode fuze (point detonate and delay), was produced in limited quantities in response to an Urgent Need Statement (UNS) submitted by Multi-National Corps - Iraq (MNC-I) in October 2004. Characteristics: Rocket Diameter Rocket Length Rocket Reliability Ballistic Range(s) -

227mm 3,937 mm Threshold 92 percent; objective: 95 percent 10 to 70 + kilometers

GMLRS DPICM

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GMLRS Unitary Contractor: Contractor - Lockheed Martin Missiles and Fire Control Management: U.S. Army AMCOM, PEO Missiles and Space, PM Precision Fires Rocket and Missile Systems, Redstone Arsenal, Al. Field Manual (FM): FM 6-60 has been renamed the FM 3-09.60.

Guided Multiple Launch Rocket System (GMLRS)

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Nomenclature: M39, M39A1, M48, M57

Name: Army Tactical Missile System (ATACMS)

Capability: The ATACMS missile gives the land-component commander an immediate, all-weather deep fire capability necessary to engage time critical targets at long range with increased lethality and Global Positioning System (GPS) accuracy, while minimizing collateral damage. Description: The Army TACMS family of munitions is a fielded, ground-launched missile system consisting of surface-to-surface guided missiles with variants containing anti-personnel/anti-materiel (APAM) and unitary warheads. Army TACMS missiles are fired from the M270A1 Multiple Launch Rocket System (MLRS) and the High Mobility Artillery Rocket System (HIMARS) launchers. Army TACMS variants provide the all weather capability to engage targets with Global Positioning System (GPS) accuracy at ranges well beyond the capability of existing cannons and rockets, and during situations when air delivered munitions are not available. Operations include Joint Suppression of Enemy Air Defense, shaping and shielding fires. Targets include air defense systems, logistics elements, and command, control, and communications complexes. - Block I (BLK I) and Block IA (BLK IA) missiles have APAM warheads. BLK I has a range of 165 kilometers, and BLK IA has a range of 300 kilometers. - Quick Reaction Unitary (QRU) missiles have a Unitary 500 pound high-explosive warhead with a point-detonating fuze and a range of 270 kilometers. QRU missiles were produced to meet an Urgent Material Release (UMR) requirement for the Global War on Terror (GWOT). - Army TACMS 2000 Unitary (T2KU) missiles hardware configuration has much commonality with the QRU missiles, but also has an improved Navigation and Guidance capability featuring a SAASM based, all-in-view GPS receiver, an improved Control Actuator System (CAS) and Electronic Control Unit (EUC), and a more reliable, repeatable FMU-161 fuze. New Operational Flight Software (OFS) also allows a near vertical attack trajectory for urban target engagements. Characteristics:

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Contractor: Contractor - Lockheed Martin Missiles and Fire Control Management: U.S. Army AMCOM, PEO Missiles and Space, PM Precision Fires Rocket and Missile Systems, Redstone Arsenal, Al. Field Manual (FM): FM 6-60 has been renamed the FM 3-09.60.

ATACMS Launch

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CHAPTER TWENTYTWO 1 June 2009

TEST EQUIPMENT

FOR OFFICIAL USE ONLY

INTENTIONALLY LEFT BLANK

Nomenclature: AN/GYQ-79A TEST PROGRAM SET

Name: Common Munitions Builtin-Test Reprogramming Equipment (CMBRE)

Capability: The Common Munitions Built-in-Test Reprogramming Equipment (CMBRE) allows U.S. Air Force and Navy personnel to initiate munition BIT, record maintenance data, and reprogram munitions OFP software on numerous MIL-STD-1760 smart munitions and Non MIL-STD-1760 Smart munitions such as the Joint Direct Attack Munition, the Advanced Medium Range Air-toAir Missile as well as next-generation weapon systems such as the Small Diameter Bomb. Description: Advanced precision-guided munitions require complex processors that need high-speed reprogramming equipment. To meet the growing demand for sophisticated test equipment, the CMBRE Plus is equipped with a 100MHz Ethernet port, Windows XP and Extended Bit-Rate (EBR) capabilities. At the same time, the CMBRE Plus is capable of servicing the U.S. military's existing inventory of smart munitions. Consequently, the CMBRE Plus is capable of testing the weapons of today as well as those that will enter service in the future. AF and Navy safety certified for use in flight line, back shop, and carrier deck environments. Characteristics: Three box system: TEST ADAPTER UNIT (BOX 1) CONTROLLER UNIT (BOX 2) ACCESSORY KIT (BOX 3) Unpackaged per system LBS Box 1

inches ft weight

Box 2

ft Box 3

ft Total

H

Cubic Ft

18

13

1.8

1.5

1.1

18

17

15

1.5

1.4

1.3

18

18

18

1.5

1.5

1.5

3

2.7

45.85

inches weight

D 22

41.2

inches weight

L

3.4

36.15 123.2

9

Munitions Currently Supported: JDAM WCMD JSOW AMRAAM SDB AIM-9X PAVEWAY II & III DMLGB HTSF JASSM AGM-142 (FMS) AARGM

SLAM-ER JAGM MALD

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Ancillary Equipment ADU-891 (V)1/E Replaces the AIM-9X TTU-574/E for missile BIT check and reprogramming Replaces the AMRAAM MBTS and CFMRE for missile BIT check and reprogramming FMS Variants: ADU-891 (V)2/E - AIM-9X only ADU-891 (V)3/e - AMRAAM only W-23 Multiplex Cable Facilitates the simultaneous BIT check and reprogramming of up to four JDAM Contractor / Status / Improvements / Special Equipment: Contractor Alliant Techsystems (ATK ), Clearwater FL Status Production CMBRE IOC 1998 CMBRE Plus IOC 2007 Special Equipment ADU-890E supporting SDB Currently managed by 681 ARSS, Eglin AFB FL Management transition to 647 AESS, Wright-Patterson AFB in 2009 - Support Equipment None Management/Engineering: ASC/77 AESW/647 AESS, Wright-Patterson AFB OH Technical Order: AIR FORCE TO 33D7-3-372-11 NAVY (NAVAIR) NA 16-30GYQ-79-2

CMBRE PLUS SYSTEM

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Name: A-10A/C ARMAMENT TEST EQUIPMENT Capability and Description: A-10A/C Armament equipment (multiple items used at all levels of maintenance). #1- Armament Control System (ACS) Interface Test Set (A-10A only, Flight-line) The ACS interface test set is a portable test unit used to test and monitor cable interfaces of the A-10 armament control system. #2- Gun Test Set (A-10A/C, Back-shop) The Gun Test Set (commonly called a –138 tester) is a portable test set used to test and isolate failures to the line replaceable unit (LRU) on the A/A49E-6 30MM aircraft armament subsystem manufactured by General Electric. #3- Stray Voltage Adapter and Test Set (A-10A/C, Flight-line) The Stray Voltage Adapter and Test Set, also referred to as the “beer can” tester, is a portable test set that uses a voltage detector and cable adapters to insure the absence of stray voltage in aircraft armament circuitry in a de-energized state, the presence of DC weapons release voltage levels in an energized state, the presence of a voltage under load for firing electro explosive devices (EEDs), and adapter cable continuity. #4- Armament Circuit Pre-load Test Set (ACPTS) (A-10A/C, Flight-line) The ACPTS replaces the Stray Voltage Adapter and Test Set described above with a modern digital components. In addition, to duplicating the functionality of the “beer can” tester it provides a Y-cable to speed up testing times when checking select armament systems. #5- Aircraft Weapon Control Test Set (AN/ASM-184B) (A-10A only, Flight-line) The Aircraft Weapon Control Test Set AN/ASM-184B is a portable unit consisting of a case and removable cover that contain all components. The test set performs preflight and periodic checkout of the aircraft control, indicator circuits, and video monitor associated with the MAVERICK guided weapon. #6- Bomb Rack Test Set (A-10A/C, Back-shop) The MAU-12, MAU-40/A, MAU-50/A, BRU-44A/A Bomb Rack Test Set is used to perform the electrical tests on the MAU-12, MAU-40/A, MAU-50/A, and BRU-44A/A bomb racks. The test set is used in conjunction with a multimeter to measure resistance and continuity of bomb rack circuits. The proper sequence of operation of the solenoids in the various bomb racks are also checked by the test set. #7- Ejector Rack Test Set (A-10A/C, Back-shop) The MER/TER/BRU Test Set is a locally manufactured test set used to perform an electrical bench check of the MER/TER/BRU type ejector racks. The test set provides a comprehensive test of the following circuits: Rack Present (F-111), Safety Switch, Home, Fire and Step (bomb release), Fire and Step (rocket), CBU Empty, and other circuits. #8- Guided Missile Test Set (GMTS) (A-10A/C, Back-shop) The Maverick Guided Missile Test Set AN/DSM-157, PN 13A9710(-3,-4) is a microprocessorbased, portable guided missile test set (GMTS) used to test and fault isolate the LAU-88/A Launcher, the LAU-117 Launcher, and the AGM-65A/B/D/G Missile when they are removed from the aircraft. #9- Mk III Test Set (A-10A/C, Back-shop) The Rocket Launcher Tester MK III is a maintenance or shop-type test that is used with the 2.75-inch FFAR system (less rockets) and any other system utilizing the MK1 squib or similar device. The MK III tester is capable of testing the safety switch, grounds, adequate pulse width,

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power available (.90 amp nominal), ripple mode, and single mode. It also checks for opens, shorts and performs a self-check and battery-check. #10- Mark IV Test Set (A-10A/C, Back-shop) The Rocket Launcher Tester MK IV is a maintenance tester that is used with the 2.75-inch FFAR system (less rockets) and any other system utilizing the MK1 squib or similar device. The MK IV tester is capable of testing the safety switch, grounds, adequate pulse width, power available (.80 amp nominal), ripple mode, and single mode. It also checks for opens, shorts and performs a self-check, battery check, and stray current check. #11- Control Test Set (CTS) (A-10A/C, Back-shop/Depot) The Control Test Set (CTS) TS-4231/U performs automatic functional testing of Line Replaceable Units (LRUs) used in the Armament Control System (ACS) and the AIM-9 Missile Control System aboard the A-10 aircraft. Internal circuitry and software simulates these system‟s various inputs and outputs. #12- Missile Launch System Test Set (A-10A/C, Flight-line) The Missile Launch System Test Set (MLSTS) is a portable test set that provides flight line test capability for the AIM-9 missile control system aboard the A-10 aircraft. #13- Depot Test Set (DTS) (A-10A/C, Depot) The A10/AIM-9 Depot Test Set is used to perform automatic functional testing of Shop Replaceable Units (SRUs) from equipment used to operate and support the AIM-9 Missile Control System on A-10 aircraft. The various inputs and outputs of the units under test (UUT) are simulated by the internal circuitry and software. #14- Portable Automated Test Station (PATS) (A-10C, Flight-line) Under the Precision Engagement (PE)/Suite 3 program, the PATS was fielded to provide troubleshooting and maintenance capabilities to support PE configured A-10 aircraft. The PATS consists of portable, stand-alone hardware intended for flight line use. Characteristics: Item #1

Test Set

NSN

Tech Order

#2

Armament Control System (ACS) Interface Test Set Gun Test Set

#3

Stray Voltage Test Set

4920-01-121-3601

33D7-50-662-1

#4

4920-01-550-4494KU

33D7-50-662-11

4920-00-106-5335KU

33D5-12-187-1

#6

Armament Circuit Pre-load Test Set Aircraft Weapon Control Test Set AN/ASM184B Bomb Rack Test Set

4933-01-049-7584

33D5-53-1-111

#7

Ejector Rack Test Set

P/N 7533694-10

11B29-3-35-2

#8

Guided Missile Test Set

4935-01-335-5060JB

33D9-54-62-1

#9

MK III Test Set

4927-01-061-1850

33D5-57-3-1

#10

MK IV Test Set

4927-01-061-1851NM

33D5-57-4-1

#11

Control Test Set (CTS)

4920-01-234-4063FJ

33D5-12-229-1-1

#12

Missile Launch System Test Set (MLSTS)

4935-01-237-1804

33D5-20-31-1

#13

Depot Test Set (DTS)

4920ND-600-248F

33D9-38-66-3

#14

Portable Automated Test Station

6625-01-566-3302

1A-10C-2-40MS-1

#5

4920-01-092-4434

33D5-12-218-1

4920-01-066-2700

33D5-12-211-1

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Contractor / Status / Improvements / Special Equipment: Contractor Multiple Status In sustainment Fielding DatesLate 1960‟s - present Management/Engineering: Items #1-5: WR-ALC/742CBSG/566CBSS, Robins AFB GA Items #6: WR-ALC/642CBSG/580CBSS, Robins AFB GA Item #7: WR-ALC/782CBSG/575CBSS, Robins AFB GA Items #8: OO-ALC/784CBSG/507CBSS, Hill AFB GA Items #9-10: OO-ALC/784CBSG/506CBSS, Hill AFB GA Items #11-14: OO-ALC/748SCMG/416SCMS, Hill AFB GA

A-10 ARMAMENT TEST EQUIPMENT

#1) ACSInterface Test Set

#4) Armament Circuit Pre-load Test Set

#2) Gun Test Set

#5) AN/ASM-184B

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#3) Stray Volts Test Set

#6) Bomb Rack Test Set

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A-10 ARMAMENT TEST EQUIPMENT (Continued)

#6) Ejector Rack Test Set

#9) MK IV Test Set

#7) Guided Missile Test Set

#10) Control Test Set (CTS)

#12) Depot Test Set (DTS)

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#8) MK III Test Set

#11) Missile Launch System Test Set (MLSTS)

#13) Portable Automated Test Station (PATS)

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Name: B-52 Multi-User System Tester Next Generation (MUSTANG) Capability: The MUSTANG is a 180 Day Verification and Certification of Weapon Release System Readiness and post maintenance check prior to Uploading of Pylons, Launchers, Missiles, and Bombs. It is a flight line and back shop armament tester that replaced armament test sets including the Weapons Preload Tester (WPT), Ground Weapon Maintenance Tester (GWM-9) and the Off-Aircraft Pylon Tester (OAPT). The MUSTANG performs back-shop checkout and certification testing, aircraft certification tests, checkout and certification testing of the weapon station interface, checkout and fault isolation testing of the Line Replaceable Units (LRUs), functional check of the B-53 MIL STD 1760 weapon umbilicals, internal tests. The MUSTANG provides fault data collections and display, the controls and display required for operator interface, data to an external computer. Description: The MUSTANG system consists of three main items; the MUSTANG, the Operational Cable Set (OCS) and the Cable Tester (CT). The MUSTANG consists of a single box containing a Versa Module Eurocard (VME) backplane that holds eleven cards with three spare slots for growth. The OCS consists of approximately 45 interface cables used to attach the MUSTANG to different armament systems and subsystems on the B-52H aircraft. These cables are designed to be field reparable using standard cable repair procedures. The CT provides the means to functionally check the OCS cables to ensure they are serviceable. Characteristics: NSN: MUSTANG Test Set: 4920-01-548-4602 Cable Tester: 4920-01-548-5431 Test Head NSN: 4920-01-548-5432 Operation Cable Set NSN: Not stock listed P/N:

MUSTANG Test Set: P/N F659-32700-1 Cable Tester P/N: F659-32460-3 MUSTANG Test Head P/N: F659-32400-1 Operational Cable Set P/N: F659-32450

Application: B-52H Contractor / Status / Improvements / Special Equipment: Contractor Boeing Wichita (Frontier Electronics and Celtron are primary subs) Status MUSTANG was started in 1999 by the B-52 SPO at OC-ALC. Initial (Lot 1) 15 MUSTANGs/OCS and 5 Cable Testers deliveries began December 2006. Option 1 (Lot 2) was for additional 15 MUSTANGs/OCS and 5 Cable Testers. Lot 3 was for 8 MUSTANGs/OCSs and 11 Cable Testers. All deliveries were complete Feb 2009. Improvements - Ch. 2 to -1 and -4 allows the user additional opportunities for local repair vs. sending into the depot - procedures and fold out drawings have been added. Ch. 2 also added calibration procedures which is one of the drivers for new Operational Software. Management/Engineering: Management - 742 CBSG 566 CBSS/GBLD, Engineering - 742 CBSG/GBEA Technical Order: 33D5-30-9-1, 33D5-30-9-3, 33D5-30-9-4

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MUSTANG TEST SET

MUSTANG CABLE TESTER

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Name: F-15 ARMAMENT TEST EQUIPMENT Capability and Description: F-15 Armament Equipment (multiple items used at all levels of maintenance). Aircraft Weapons Control Test Set (T-169, Flight-line). The T-169 tester is used to checkout, on a single weapon station basis, the LAU-106 missile launcher, the centerline pylons, and inboard pylon, LAU-114 launcher, the LAU-128 launcher and the gun system, when they are interfaced by the associated aircraft wiring with the Programmable Armament Control Set (PACS) or Armament Control Set (ACS). Fielded: +71 each. Launcher Pylon Test Set (T-170, Back-shop). The T-170 tester is used in the weapons release shop to perform electrical continuity and fault isolation checks of the LAU-106 missile launcher, inboard pylon, launcher adapters, MAU-12 bomb rack, LAU-114 launcher and AMRRAM launcher. Fielded: +37 each. Weapons Firing Circuit Test Set (T-171, Flight-line). The T-171 tester is used to perform preload checks on aircraft prior to loading weapons. The test set is used to detect unacceptable levels of stray voltage. Fielded: +9 each. Stores Management Subsystem Test Set (T-197, Back-shop). The T-197 tester is used in the armament shop to perform electrical functional and fault isolation testing of the UU-59 inboard and SUU-60/73 centerline pylons; ADU-407/552/578 adapters; LAU-88, LAU -117, and LAU128 launchers; MAU-12, BRU-46, BRU-47 bomb racks; the electronic sequencer unit; power supply; encoder/decoder, and SUU-20 bomb dispenser. Fielded: +43 each. Stores Management System Test Set (T-198, Flight-line). The T-198 tester is used to checkout, on a single station basis, the inboard pylon, centerline pylon, LAU-117/LAU-88 launchers, ADU-578, ADU-407, ADU-552 adapters, CFT-4, and LAU-114/LAU-128 launchers when interfaced with the armament wiring and the PACS. Fielded: +60 each. Armament Circuits Preload Test Set (T-199, Flight-line). The T-199 tester is used to perform weapons system preload check on the aircraft to detect levels of stray voltage and to detect the presence of firing voltages. Fielded: +73 each. Aircraft Pod Interface Test Set (T-224, Flight-line). The T-224 tester provides checkout and fault isolation of the improved/AXQ-14 Data Link System of the Aircraft Weapons Delivery System. The test set shall interface the SUU-73/A Fuselage and Centerline Pylon Disconnects and Umbilical Cables through Interconnecting Cables. Fielded: +20 each.

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Characteristics: Item Test Set #1 Aircraft Weapons Control Test Set (T-169). #2 Launcher Pylon Test Set (T-170). #3 Weapons Firing Circuit Test Set (T-171). #4 Stores Management Subsystem Test Set (T-197). #5 Stores Management System Test Set (T-198). #6 Armament Circuits Preload Test Set (T-199). #7 Aircraft Pod Interface Test Set (T-224).

P/N A05G0504-X A05G0506--X

Tech Order 33D5-16-72-1/-4 33D5-30-4-1/-4

A05G0451-X

33D5-3-46-1/-4

A05G0516-XX

33D5-63-5-1/-4

A05G0514-1-XX

33D5-12-231-1/-4

A05G0515-X

33D5-3-50-1/-4

A05G0600-X

33D7-50-1981-1/-4

Contractor / Status / Improvements / Special Equipment: Contractor Boeing, St. Louis Status In sustainment, upgrades to improve capability Fielding DatesMSIP series tester – 1970s, T190 series testers – 1980s Management/Engineering: All items in above chart managed by WR-ALC/742CBSG/566CBSS, Robins AFB GA

F-15 ARMAMENT TEST EQUIPMENT

#1) T-169 Case 1 of 3

#2) T-170 Case 1 of 3

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#3) T-171 Case 1 of 1

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F-15 ARMAMENT EQUIPMENT (Continued)

#4) T-197 Case 1 of 5

#5) T-198 Case 1 of 4

#6) T-199 Case 1 of 2

#7) T-224 Case 1 of 2

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Name: CRUISE MISSILE AUTOMATIC TEST EQUIPMENT Capability and Description: Cruise Missile Automatic Test Systems (CM-ATS) (multiple items used at intermediate and depot levels of maintenance). The AN/GSM-263 Electronic System Test Set (ESTS) is a multi-bay Automated Test System designed to test and diagnose missiles and associated Carrier Aircraft Equipment (CAE) used to launch missiles. The ESTS operates under automated computer control to provide power, stimulus, switching, monitoring, and measurement of test signal flow to the Unit Under Test (UUT). Five different configurations of ESTS equipment currently exists: AN/GSM-263 ESTS „Base‟ Model. The first version of the ESTS was the ESTS Model GSM263. It was originally designed in the mid-70s, with the last tester delivered in 1984. This incarnation of the ESTS was designed to support SRAMs (AGM-69, removed from inventory in the 1990s), and ALCMs (AGM-86A and B). Fielded: 4 each AN/GSM-263A ESTS „A‟ Model. Most of the original ESTS base models were modified to the ESTS Model 263A. This modification added the capability to support testing of the B-1 CSRL (the 180-Inch Launcher). Fielded: 11 each AN/GSM-263G ESTS „G‟ Model. The difference between an „A‟ version and „G‟ version is the incorporation of the 1A24 Bus Extender in the main rack, which allows GPIB communications with an additional rack, known as the Remote Switching Control Assembly (RSCA). The RSCA is used for testing the Advanced Cruise Missile (ACM). Fielded: 20 each AN/GSM-263F ESTS „F‟ Model. Model GSM-263F is a base model modified to include a GPIB Bus Extender to allow connection of an RSCA for ACM testing. Only one ESTS 263F version is still fielded, and is located at Tinker, AFB. This tester is limited in that it cannot test CSRLs, but has the added capability of testing ACMs. AN/GSM-263C ESTS „C‟ Model. The GSM-263C was developed to provide specific test capability for B-2 weapon systems. It is a base model ESTS with several key modifications. The changes are provided to allow the ESTS to test the B-2 Rotary Launcher Assembly (RLA) and four of its LRUs. Fielded: 7 each The Missile Radar Altimeter Test Assembly (MRATA) is used in conjunction with the ESTS to accomplish testing of the installed missile radar altimeter (MRA) and common missile radar altimeter (CMRA) in an Air Launched Cruise Missile (ALCM) AGM-86B and Conventional Air Launched Cruise Missile (CALCM) AGM-86/C as well as the installed MRA in an Advanced Cruise Missile (ACM) AGM-129A. Three different configurations of MRATA equipment currently exists: MRATA -1007. The MRATA, P/N: 70D180840-1007, is the initial MRATA developed. It was later modified to the 70D180840-7003, 70R180840-1003, and then finally to the current 70R180840-1007 part number configuration. Fielded: 2 each MRATA -1017. MRATA serial numbers 0029 and beyond were part numbered 70D1808401009, and select quantities were converted to P/N 70D180840-1011 and then finally to the

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current 70D180840-1017 part number configuration. Both the MRATA -1007 and MRATA 1017 are functionally and physically equivalent but are carried under separate part and national stock numbers. Fielded: 14 each MRATA -1019. Select quantities of the original 70D180840-1009 part number of MRATA were later converted and were added capabilities to test the Advance Cruise Missile. The MRATA 1019 has added circuitry to test these functions along with MRATA -1017 functions. Fielded: 16 each For testing ACM, ALCM, and CALCM, an Air Data Test Set (ADTS) is used in conjunction with the ESTS and MRATA. ADTS. The Air Data Test Set (ADTS), also known as the AN/GSM-291, is a precise, stable, easy to use pressure control system designed to accurately simulate and measure the pneumatic pressures associated with a cruise missile in flight. The test set is capable of operator selectable units of measurement in terms of pressure (inches of mercury or millibars), altitude (feet or meters), and airspeed (knots or kilometers per hour). Fielded: 24 each Calibration/certification of the ESTS is accomplished using standard test equipment and a, Portable Automatic Test Equipment Calibrator (PATEC). There are two versions of the PATEC; one for the ESTS, and one for the ADTS. PATEC-ESTS. A PATEC is used for calibration verification of the ESTS. A calibration TPS is executed on the ESTS in conjunction with the PATEC, which is performed every 90 days. The operator is guided through instructions on the ESTS on the hookup and test using the PATEC. Fielded: 23 each PATEC-ADTS. ADTS is calibrated on an annual basis using the ADTS PATEC. The King Nutronics Pressure Measurement Standard (3719-7-1) will replace the Ruska Pressure Measurement Standard (DDR 6000) as needed through attrition. The unit is a high accuracy microprocessor-driven pressure calibrator designed to provide regulated static (PS) and total (PT) pressure/vacuum outputs to simulate altitudes and airspeeds (QC) in instruments. Characteristics: Item #1 #2 #3 #4 #5 #6 #7 #8 #9 #10

Test Set AN/GSM-263 ESTS „Base‟ Model AN/GSM-263 ESTS „A‟ Model AN/GSM-263 ESTS „G‟ Model AN/GSM-263 ESTS „F‟ Model AN/GSM-263 ESTS „C‟ Model MRATA -1007 MRATA -1017 MRATA -1019 ADTS PATEC-ESTS

#11

PATEC-ADTS

NSN 4920-01-113-3246KV 4920-01-136-5146KV 4920-01-356-9514KV 4920-01-357-5016KV 4920-01-265-4090KV 4935-01-105-6373KV 4935-01-166-7423KV 4935-01-277-4760KV 4920-01-106-3343KV 6625-01-110-4426RH 6685-01-115-0303KV 6685-01-512-6426KV

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Tech Order 33D9-61-71-1/-4 33D9-61-71-1/-4 33D9-61-71-1/-4 33D9-61-71-1/-4 33D9-61-71-21/-24 33D9-44-233-1/-4 33D9-44-233-1/-4 33D9-44-233-1/-4 33D9-61-71-1/-4 33D9-61-71-7-1 33D9-61-71-7-1

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Contractor / Status / Improvements / Special Equipment: Contractor Boeing, St. Louis Status In sustainment Fielding DatesDeveloped in mid 1970‟s; fielded 1981-1984

Management/Engineering: All items in above chart managed by WR-ALC/742CBSG/566CBSS, Robins AFB GA

CRUISE MISSILE AUTOMATIC TEST EQUIPMENT

AN/GSM-263 ESTS (#1- #5)

MRATA (#6 - #8)

ADTS (#9)

Not Shown: PATEC-ESTS and PATEC-ADTS (items # 10 - #11)

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Nomenclature: TTU-584/E

Name: Common Organizational Level Tester (COLT)

Capability: The COLT Tester Set (CTS) is an s Nuclear Certified tester that is used in conjunction with aircraft specific Test Program Sets (TPSs) to perform operational capability verification of aircraft Stores Management System and armament components/assemblies in austere deployed locations. The CTS used with F-22 TPSs performs on aircraft testing of the F-22 Stores Management System and backshop testing of the F-22 Bomb Rack Units and Pylons. The CTS used with B-2 TPSs performs testing of the B-2 Rotary Launcher Assembly, Smart Bomb Rack Assembly and Bomb Rack Unit (BRU-44B/A). Description: The CTS consists of a COLT Tester Unit (CTU), power cable, and Common Accessory kit. The CTU consists of Commercial Off–The-Shelf (COTS) instrumentation, custom control software drivers, and Test Program Sets (TPS) to support the functional test requirements of the F-22 and B-2 weapon systems. The instrumentation consists of a VXI Technology VM2710A Digital Multimeter, a VXI Technology VM4016 Comparator, a VXI Technology VM1602 Time Stamp, a VXI Technology VM2001 Power Switch, and a signal Switch Matrix made up of six VXI Technology modules; four SM4000, one SM4002, and one SM5001. The CTU contains cooling, heating, shock and vibration resistance, and environmental protection for worldwide, flight-line operational environments. Test instrumentation components are used for test stimuli and measurement. The COLT operates on 115 VAC, 3 phase 400Hz or 115 VAC, 1 phase 50/60 Hz from ground power equipment or facility power. The CTU is approximately 22 inches in width, 22 inches in depth by 28 inches in height and weighs 125 lbs. The COLT Common Accessory Kit contains a Portable Display Control Unit (PDCU) which is a ruggedized Laptop computer, PDCU utility cable, Power Cable Adapters and Self Test Adapter Assembly. The Accessory Kit is approximately 28 inches wide, 28 inches deep and 16 inches high and weighs approximately 40 lbs. Characteristics: NSN: COLT (TTU-584/E): 4920-01-484-6268 COLT Common Accessory Kit: 4920-01-516-0191 P/N:

COLT (TTU-584/E): P/N ES125190-103 COLT Common Accessory Kit: P/N ES125276-101

Application: B-2 and F-22A Contractor / Status / Improvements / Special Equipment: Contractor Lockheed Martin Simulation, Training & Support, Orlando, FL Status Operationally deployed in support of the F-22A and B-2. Currently 81 COLTs fielded with 20 currently in production to be delivered in Nov 09. Improvements - Reliability upgrades to improve availability of the CTS and TPS on-going

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Management/Engineering: Management/Engineering - 647th AESS/SYAB, WPAFB, Sustainment 566th CBSS/GBLD Robins AFB Technical Order: 33D5-12-243-1

COLT TESTER UNIT

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COLT COMMON ACCESSORY KIT

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INTENTIONALLY LEFT BLANK

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CHAPTER TWENTYTHREE 1 June 2009

AIRCRAFT

FOR OFFICIAL USE ONLY

INTENTIONALLY LEFT BLANK

Nomenclature: B-1B

Name: Lancer

Capability: Carrying the largest payload of both guided and unguided weapons in the Air Force inventory, the multi-mission B-1 is the backbone of America's long-range bomber force. It can rapidly deliver massive quantities of precision and non-precision weapons against any adversary, anywhere in the world, at any time. Description: The B-1B's blended wing/body configuration, variable-geometry wings and turbofan afterburning engines, combine to provide long range, maneuverability and high speed while enhancing survivability. Forward wing settings are used for takeoff, landings, air refueling and in some high-altitude weapons employment scenarios. Aft wing sweep settings - the main combat configuration -- are typically used during high subsonic and supersonic flight, enhancing the B-1B's maneuverability in the low- and high-altitude regimes. The B-1B's speed and superior handling characteristics allow it to seamlessly integrate in mixed force packages. These capabilities, when combined with its substantial payload, excellent radar targeting system, long loiter time and survivability, make the B-1B a key element of any joint/composite strike force. The B-1 weapon system is capable of creating a multitude of far-reaching effects across the battlefield. The B-1 is a highly versatile, multi-mission weapon system. The B-1B's offensive avionics system includes high-resolution synthetic aperture radar, capable of tracking, targeting and engaging moving vehicles as well as self-targeting and terrain-following modes. In addition, an extremely accurate Global Positioning System-aided Inertial Navigation System enable aircrews to autonomously navigate globally, without the aid of ground-based navigation aids as well as engage targets with a high level of precision. The recent addition of Combat Track (CT) II radios permit an interim secure beyond line of sight reach back connectivity until Link-16 is integrated on the aircraft. In a time sensitive targeting environment, the aircrew can receive targeting data from the Combined Air Operations Center (CAOC) over CT II, and then update mission data in the offensive avionics system to strike emerging targets rapidly and efficiently. This capability continues to be employed on a daily basis in support of operations Enduring Freedom and Iraqi Freedom. The B-1B's self-protection electronic jamming equipment, radar warning receiver (ALQ-161) and expendable countermeasures (chaff and flare) system complements its low-radar cross-section to form an integrated, robust onboard defense system that supports penetration of hostile airspace. The ALQ-161 electronic countermeasures system detects and identifies the full spectrum of adversary threat emitters then applies the appropriate jamming technique either automatically or through operator manual inputs. Chaff and flares are employed against radar and infrared threat systems. B-1 capabilities are being continually enhanced following completion of the Conventional Mission Upgrade Program (CMUP). (CMUP improved lethality by adding the ability to carry up to 30 cluster munitions (CBU-87, -89, -97), a Global Positioning System receiver, and an improved weapons interface that allows the carriage of Joint Direct Attack Munitions (JDAM), the Joint Air to Surface Standoff Missile (JASSM), and Wing Corrected Munitions Dispenser (WCMD)- guided weapons (CBU-103, -104, -105) in addition to advanced secure radios (ARC210) and the ALE-50 Towed Decoy System. Current modernization effort is focused on the Fully Integrated Data Link (FIDL) program which provides line of sight and beyond line of sight Link 16 communication and upgraded rear cockpit displays. The recent addition of the Laptop Controlled Targeting Pod (LCTP), in response to a CENTAF Urgent Need Request gives the

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B-1B the capability to positively identify, track and attack targets, greatly decreasing the time required to prosecute time sensitive targets. LCTP Phase II will provide Laser-JDAM (GBU-54) capability and automated transfer of target coordinates from the pod. The B-1B holds 106 world records for speed, payload, range, and time of climb in its class. The National Aeronautic Association recognized the B-1B for completing one of the 10 most memorable record flights for 1994. The most recent records were made official in 2004. Characteristics: Primary Function - Long-range, multi-role, heavy bomber Power plant Four General Electric F101-GE-102 turbofan engine with afterburner Thrust 30,000-plus pounds with afterburner, per engine Wingspan 137 feet (41.8 meters) extended forward, 79 feet (24.1 meters) swept aft Length 146 feet (44.5 meters) Height 34 feet (10.4 meters) Weight approximately 190,000 pounds (86,183 kilograms) Max Takeoff Weight - 477,000 pounds (216,634 kilograms) Fuel Capacity 265,274 pounds (120,326 kilograms) Payload 75,000 pounds ( 34,019 kilograms) Speed 900-plus mph (Mach 1.2 at sea level) Range Intercontinental Ceiling More than 30,000 feet (9,144 meters) Armament 24 GBU-31 GPS-aided JDAM (both Mk-84 general purpose bombs and BLU-109 penetrating bombs) or 24 Mk-84 2,000-pound general purpose bombs or; Mk-65 naval mines; 84 Mk-82 500-pound general purpose bombs or; 84 Mk-62 500-pound naval mines; 30 CBU-87, -89, -97 cluster munitions; 30 CBU-103/104/105 WCMD, 24 AGM-158 JASSMs. Future Capability will include SDB I and 15 GBU-54 LJDAM. Crew Four (aircraft commander, copilot, and two weapon systems officers) Initial operating capability - October 1986 Contractor / Status / Improvements / Special Equipment: Contractor - Boeing, North America (formerly Rockwell International, North American Aircraft); Offensive avionics, Boeing Military Airplane; defensive avionics, EDO Corporation Status Active force, 64 (test, 2); ANG, 0; Reserve, 0 Management/Engineering: SPM: 427th ACSG, Tinker AFB, OK DSM: 812th AESG, WPAFB, OH

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Nomenclature: B-2A

Name: Spirit

Capability: The B-2A Spirit is a multi-role bomber capable of delivering both conventional and nuclear munitions. A dramatic leap forward in technology, the bomber represents a major milestone in the U.S. bomber modernization program. The B-2 brings massive firepower to bear, in a short time, anywhere on the globe through previously impenetrable defenses. Description: The B-2A low-observable, or "stealth," characteristics give it the unique ability to penetrate an enemy's most sophisticated defenses and threaten its most valued, and heavily defended, targets. Its capability to penetrate air defenses and threaten effective retaliation provides a strong, effective deterrent and combat force well into the 21st century. The revolutionary blending of low-observable technologies with high aerodynamic efficiency and large payload gives the B-2A important advantages over existing bombers. Its low-observability provides it greater freedom of action at high altitudes, thus increasing its range and a better field of view for the aircraft's sensors. Its unrefueled range is approximately 6,000 nautical miles (9,600 kilometers). Characteristics: Primary Function Multi-role heavy bomber Power plant Four General Electric F118-GE-100 engine Thrust 17,300 pounds each engine Wingspan 172.6 feet (52.6 meters) Length 69 feet (20.9 meters) Height 16.5 feet (5 meters) Weight 160,000 pounds (72,575 kilograms) Max Takeoff Weight 336,500 pounds (152,634 kilograms) Fuel Capacity 167,000 pounds (75750 kilograms) Payload 40,000 pounds (18,144 kilograms) Speed High subsonic Range Intercontinental Ceiling 50,000 feet (15,240 meters) Crew Two pilots Armament Conventional or nuclear weapons Weapon Capability B-2A GBU-31(V)1/B (JDAM-84) 16 GBU-31(V)3/B (JDAM-109) 16 GBU-38 (JDAM-82) 80 AGM-154 (JSOW) 16 (145 BLU-97/B submunitions) AGM-158 (JASSM) 16 CBU-87/89 34 GBU-28B/B, GBU-28C/B 8 Mk-82GP 80 Mk-62 Quick Strike Mine 80 Mk-84GP (2000lb) 16 B61-7 (Nuclear) 16 B61-11 (Nuclear) 16 B83 (Nuclear) 16

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Initial operating capability - April 1997 Inventory Active force: 20 (1 test); ANG: 0; Reserve: 0 Contractor / Status / Improvements / Special Equipment: Contractor - Northrop Grumman Corp. and Contractor Team: Boeing Military Airplanes Co., Hughes Radar Systems Group, General Electric Aircraft Engine Group and Vought Aircraft Industries, Inc. Status Inventory Management/Engineering: 726 AESG, WPAFB, OH

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Nomenclature: B-52H

Name: Stratofortress

Capability: Air Combat Command's B-52H is a long-range, heavy bomber that can perform a variety of missions. The bomber is capable of flying at high subsonic speeds at altitudes up to 50,000 feet (15,166.6 meters). It can carry nuclear or precision guided conventional ordnance with worldwide precision navigation capability. Description: In a conventional conflict, the B-52H can perform strategic attack, air interdiction, offensive counter-air and maritime operations. During Desert Storm, B-52s delivered 40 percent of all the weapons dropped by coalition forces. It is highly effective when used for ocean surveillance, and can assist the U.S. Navy in anti-ship and mine-laying operations. Two B-52Hs, in two hours, can monitor 140,000 square miles (364,000 square kilometers) of ocean surface. All B-52Hs are equipped with an electro-optical viewing system that uses platinum silicate forward-looking infrared and high resolution low-light-level television sensors to augment targeting, battle assessment, and flight safety, thus further improving its combat ability and lowlevel flight capability. Pilots wear night vision goggles (NVG) to enhance their vision during night operations. Night vision goggles provide greater safety during night operations by increasing the pilot's ability to visually clear terrain, avoid enemy radar and see other aircraft in a covert/lights-out environment. The use of aerial refueling gives the B-52H a range limited only by crew endurance. It has an unrefueled combat range in excess of 8,800 miles (14,080 kilometers). Characteristics: Primary Function Power plant Thrust Wingspan Length Height Weight Max Takeoff Weight Fuel Capacity Payload Speed Range Ceiling Crew -

Heavy bomber Eight Pratt & Whitney engines TF33-P-3/103 turbofan Each engine up to 17,000 pounds 185 feet (56.4 meters) 159 feet, 4 inches (48.5 meters) 40 feet, 8 inches (12.4 meters) Approximately 185,000 pounds (83,250 kilograms) 488,000 pounds (219,600 kilograms) 312,197 pounds 70,000 pounds (31,500 kilograms) 650 miles per hour (Mach 0.86) 8,800 miles (7,652 nautical miles) 50,000 feet (15,151.5 meters) Five (aircraft commander, pilot, radar navigator, navigator and electronic warfare officer Armament Approximately 70,000 pounds (31,500 kilograms) mixed ordnance – bombs, mines and missiles. (Modified to carry air-launched cruise missiles) Weapon Capability B-52 GBU-31(V)1/B (JDAM-84) 12 GBU-31(V)3/B (JDAM-109) 12 GBU-38 (JDAM-82) 12 AGM-154 (JSOW) 0 (145 BLU-97/B submunitions)

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AGM-158 (JASSM) 12 CBU-87/89 24 GBU-37/B (GAM-113) 0 GBU-28B/B 4 Mk-82GP 45 Mk-62 Quick Strike Mine 45 Mk-84GP (2000lb) 12 B61-7 (Nuclear) 8 B61-11 (Nuclear) 0 B83 (Nuclear) 8 AGM-86B ALCM (Nuclear) 20 AGM-86C CALCM (Conventional) 20 AGM-129 ACM (Nuclear) 12 CBU-103/104/105 WCMD 16 GBU-10 Laser Guided Bomb 10 GBU-12 Laser Guided Bomb 13 Mk63/Mk65 Quick Strike Mine 18 IR Countermeasures – The B-52H has the AN/ALE-20 Flare Ejector System which utilizes 12 AN/ALA-17 flare sets, with 16 flare bursts per set, and a maximum of 192 single flare bursts per aircraft. There are 12 corresponding flare ejector cases installed on the aircraft that hold each of the flare sets. This system can carry the following flares. ALA-17A Flare Cartridge ALA-17B Flare Cartridge Initial operating capability - April 1952 Inventory Active force, 85; ANG, 0; Reserve, 9 Contractor / Status / Improvements / Special Equipment: Contractor - Boeing Military Airplane Co. Status Inventory Management/Engineering: 540 ACSS/GFLC, Tinker AFB, OK

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Nomenclature: A-10

Name: Thunderbolt II

Capability: A-10 Thunderbolt II has excellent maneuverability at low air speeds and altitude, and is a highly accurate weapons-delivery platform making it the best aircraft to provide Close Air Support (CAS) for ground forces. It can loiter near battle areas for extended periods of time and operate under 1,000-foot ceilings (303.3 meters) with 1.5-mile (2.4 kilometers) visibility. Using night vision goggles, A-10 and OA-10 (Airborne Forward Controller) pilots can conduct their missions during darkness. Description: The aircraft can survive direct hits from armor-piercing and high explosive projectiles up to 23mm. Their self-sealing fuel cells are protected by internal and external foam. Manual systems back up their redundant hydraulic flight-control systems. This permits pilots to fly and land when hydraulic power is lost. Avionics equipment includes multi-band communications; Global Positioning System and inertial navigations systems; infrared and electronic countermeasures against air-to-air and airto-surface threats. The A-10 has a Pave Penny laser spot tracker system; a heads-up display to display flight and weapons delivery information; and a low altitude safety and targeting enhancement system, which provides constantly computed impact and release points for accurate ordnance delivery. There is also a low-altitude autopilot and a ground collision avoidance system. The A-10 is currently undergoing the precision engagement modification, which adds upgraded cockpit displays, moving map, hands on throttle and stick, digital stores management, LITENING and Sniper advanced targeting pod integration, situational awareness data link (SADL), GPS-guided weapons, and upgraded DC power. Precision engagement modified aircraft are designated as the A-10C. Thunderbolt IIs have Night Vision Imaging Systems, or NVIS, goggle compatible single-seat cockpits forward of their wings and a large bubble canopy which provides pilots all-around vision. The pilots are protected by titanium armor that also protects parts of the flight-control system. The redundant primary structural sections allow the aircraft to enjoy better survivability during close air support than did previous aircraft. Characteristics: Primary Function Power plant Thrust Wingspan Length Height Weight Max Takeoff Weight Fuel Capacity Payload Speed Range Ceiling Crew -

A-10 - close air support, OA-10 - airborne forward air control Two General Electric TF34-GE-100 turbofans 9,065 pounds each engine 57 feet, 6 inches (17.42 meters) 53 feet, 4 inches (16.16 meters) 14 feet, 8 inches (4.42 meters) 29,000 pounds (13,154 kilograms) 51,000 pounds (22,950 kilograms) 11,000 pounds (7,257 kilograms) 16,000 pounds (7,257 kilograms) 420 miles per hour (Mach 0.56) 800 miles (695 nautical miles) 45,000 feet (13,636 meters) One

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Armament - One 30 mm GAU-8/A seven-barrel Gatling gun with 1,174 to 1,350 rounds of ammunition (depending on the storage drum used) capable of firing 3,900 rounds per minute to defeat a wide variety of targets including tanks. - Up to 16,000 pounds of mixed ordnance on eight under-wing and three underfuselage pylon stations, including 500 pound Mk-82 and 2,000 pounds Mk-84 series low/high drag bombs, JDAM, wind corrected munitions dispenser or WCMD incendiary cluster bombs, combined effects munitions, mine dispensing munitions, AGM-65 Maverick missiles and laser-guided/electro-optically guided bombs; infrared countermeasure flares; electronic countermeasure chaff; jammer pods; 2.75-inch (6.99 centimeters) rockets; illumination flares and AIM-9 Sidewinder missiles. Countermeasures - The A-10 currently uses the ALE-40/47 dispensing system. With 2 wingtip and 2 wheel well stations, each station is capable of holding 4 MODS of Chaff or Flare. The C/F and MODS used include: - CHAFF: - RR-170 A/AL, RR-180/AL, RR-188/AL - FLARE, INFRARED (IR) COUNTERMEASURES, SIMULATOR: - M206, M206(T-2) Simulator, MJU-7A/B, MJU-7/B, MJU-7(T-2)B Simulator, M211, MJU-50/B - MJU-11 Chaff/Flare Magazine can carry: 30 ea RR-170 A/AL, RR-180/AL or RR-188/AL Chaff Cartridges or 30 ea M206, M206 (T-2) Flare Simulators - MJU-12 Flare Magazine can carry: 15 ea MJU-7A/B, 15 ea MJU-7/B or 15 ea MJU-7(T-2)B Flare Simulators The A-10 also utilizes illuminating and target marking flares dispensed by a SUU-25 Flare Dispenser. Each dispenser can hold up to 8 of the following Flares: - SUU-25 C/A, E/A: LUU-2/B, -2A/B, -2B/B, -2C/B, and -19/B (IR Illuminating Flares) LUU-1/B, -5/B, -6/B (Target Marking Flares) - SUU-25 F/A: LUU-2/B, -2A/B, -2B/B, and -19/B (IR Illuminating Flares) Initial operating capability - A-10A, 1977; A-10C, 2007 Inventory Active force, A-10, 143 and OA-10, 70; Reserve, A-10, 46 and OA-10, 6; ANG, A-10, 84 and OA-10, 18 Contractor / Status / Improvements / Special Equipment: Contractor - Fairchild Republic Co. Status Inventory Management/Engineering: 642 AESS, WPAFB, OH

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Nomenclature: F-15A-D

Name: Eagle

Capability: The F-15A-D Eagle is an all-weather, extremely maneuverable, tactical fighter designed to permit the Air Force to gain and maintain air supremacy over the battlefield. Description: The Eagle's air superiority is achieved through a mixture of unprecedented maneuverability and acceleration, range, weapons and avionics. It can penetrate enemy defense and outperform and outfight any current enemy aircraft. The F-15A-D has electronic systems and weaponry to detect, acquire, track and attack enemy aircraft while operating in friendly or enemy-controlled airspace. The weapons and flight control systems are designed so one person can safely and effectively perform air-to-air combat. The F-15A-D's superior maneuverability and acceleration are achieved through high engine thrust-to-weight ratio and low wing loading. Low wing-loading (the ratio of aircraft weight to its wing area) is a vital factor in maneuverability and, combined with the high thrust-to-weight ratio, enables the aircraft to turn tightly without losing airspeed. A multi-mission avionics system sets the F-15A-D apart from other fighter aircraft. It includes a heads-up display, advanced radar, inertial navigation system, flight instruments, ultrahigh frequency communications, tactical navigation system and instrument landing system. It also has an internally mounted, tactical electronic-warfare system, "identification friend or foe" (IFF) system, electronic countermeasures set, Joint Helmet Mounted Cuing System (JHMCS) and a central digital computer. The pilot's heads-up display (HUD) projects on the windscreen all essential flight information gathered by the integrated avionics system. This display, visible in any light condition, provides information necessary to track and destroy an enemy aircraft without having to look down at cockpit instruments. In addition, the JHMCS is a helmet mounted display and cueing system which provides information such as targeting cues and aircraft performance parameters and graphically displays them directly on the helmet visor. The F-15A-D's versatile pulse-Doppler radar system can look up at high-flying targets and down at low-flying targets without being confused by ground clutter. It can detect and track aircraft and small high-speed targets at distances beyond visual range down to close range, and at altitudes down to treetop level. The radar feeds target information into the central computer for effective weapons delivery. For close-in dogfights, the radar automatically acquires enemy aircraft, and this information is projected on the HUD. The F-15A-D's electronic warfare system provides both threat warning and automatic countermeasures against selected threats. A variety of air-to-air weaponry can be carried by the F-15A-D. An automated weapon system enables the pilot to perform aerial combat safely and effectively, using the HUD and the avionics and weapons controls located on the engine throttles or control stick. When the pilot changes from one weapon system to another, visual guidance for the required weapon automatically appears on the HUD. The F-15C/D aircraft is capable of using Conformal Fuel Tanks that attach to the aircraft fuselage sides and provide the ability for the aircraft to carry more fuel without the higher drag of external fuel tanks. Each Conformal Fuel Tank adds about 5000 pounds of addition fuel to the F-15C/D aircraft." Characteristics: Primary Function -

Tactical Fighter

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Power plant -

Two Pratt & Whitney F100-PW-100 or 220 turbofan engines with afterburners Thrust (C/D models) 23,450 pounds each engine Wingspan 42.8 feet (13 meters) Length 63.8 feet (19.44 meters) Height 18.5 feet (5.6 meters) Weight 31,700 pounds Max Takeoff Weight (C/D models) 68,000 pounds (30,844 kilograms) Fuel Capacity 26,520 pounds (with three external tanks (or 32,356 pounds (with Conformal Fuel Tanks installed and two external fuel tanks) Payload depends upon mission Speed 1,875 mph (Mach 2.5 plus) Range 2,173 nautical miles (2,501 miles) ferry range with three external fuel tanks or 2,666 nautical miles (3,068 miles) with conformal fuel tanks installed and two external fuel tanks (maximum takeoff weight) Ceiling 65,000 feet (19,812 meters) Crew F-15A/C: one. F-15B/D: two Armament - One internally mounted M-61A1 20mm 20-mm, six-barrel cannon with 940 rounds of ammunition; four AIM-9L/M/X Sidewinder and four or up to eight AIM-120 AMRAAMs, carried externally. Initial operating capability - September 1975 Inventory Total force, 522 Contractor / Status / Improvements / Special Equipment: Contractor - The Boeing Company Status Inventory Management/Engineering: 912 AESG, WPAFB, OH

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Nomenclature: F-15E

Name: Strike Eagle

Capability: The F-15E Strike Eagle is a dual-role fighter designed to perform air-to-air and air-to-ground missions. An array of avionics and electronics systems gives the F-15E the capability to fight at low altitude, day or night, and in all weather. Description: The aircraft uses two crew members, a pilot and a weapon systems officer. Previous models of the F-15 are assigned air-to-air roles; the "E" model is a dual-role fighter. It has the capability to fight its way to a target over long ranges, destroy enemy ground positions and fight its way out. The aircraft's navigation system uses a laser gyro and a Global Positioning System to continuously monitor the aircraft's position and provide information to the central computer and other systems, including a digital moving map in both cockpits. The APG-70 radar system allows aircrews to detect ground targets from long ranges. One feature of this system is that after a sweep of a target area, the crew freezes the air-to-ground map then goes back into air-to-air mode to clear for air threats. During the air-to-surface weapon delivery, the pilot is capable of detecting, targeting and engaging air-to-air targets while the weapons systems officer (WSO) designates the ground target. The low-altitude navigation and targeting infrared for night (LANTIRN) system allows the aircraft to fly at low altitudes, at night and in any weather conditions, to attack ground targets with a variety of precision-guided and unguided weapons. The LANTIRN system gives the F-15E unequaled accuracy in weapons delivery day or night and in poor weather, and consists of two pods attached to the exterior of the aircraft. The navigation pod contains terrain-following radar which allows the pilot to safely fly at a very low altitude following cues displayed on a heads up display (HUD). This system also can be coupled to the aircraft's autopilot to provide "hands off" terrain-following capability. The targeting pod contains a laser designator and a tracking system that mark an enemy for destruction at long ranges. Once tracking has been started, targeting information is automatically handed off to GPS or laser-guided bombs. One of the most important additions to the F-15E is the rear cockpit, and the weapons systems officer (WSO). On four screens, this officer can display information from the radar, electronic warfare or infrared sensors, monitor aircraft or weapons status and possible threats, select targets, and use an electronic "moving map" to navigate. Two hand controls are used to select new displays and to refine targeting information. Displays can be moved from one screen to another, chosen from a "menu" of display options. In addition to three similar screens in the front seat, the pilot has a transparent glass HUD at eye level that displays vital flight and tactical information. The pilot doesn't need to look down into the cockpit, for example, to check weapon status. At night, the screen is even more important because it displays a video picture nearly identical to a daylight view of the world generated by the forward-looking infrared sensor. Characteristics: Primary Function Power plant Thrust Wingspan Length -

Air-to-ground attack aircraft Two Pratt & Whitney F100-PW-220 or F100-PW-229 turbofan engines with afterburners 23,500 (F100-PW-220) - 29,000 (F100-PW-229) pounds per engine 42.8 feet (13 meters) 63.8 feet (19.44 meters)

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Height Weight Max Takeoff Weight Fuel Capacity Payload Speed Range -

18.5 feet (5.6 meters) 37,500 pounds ( 17,010 kilograms) 81,000 pounds (36,450 kilograms) 35,790 pounds (three external tanks plus conformal fuel tanks) depends upon mission 1,875 mph (Mach 2.5 plus) 2,254 nautical miles (2,594 miles) ferry range with conformal fuel tanks and three external fuel tanks Ceiling 60,000 feet (18,288 meters) Crew Pilot and weapon systems officer Armament - One 20mm multi-barrel gun mounted internally with 500 rounds of ammunition. Four AIM-9L/M Sidewinder missiles, or up to eight AIM-120 AMRAAM missiles. Most air-to-surface weapons in the Air Force inventory Maximum Load by Weapon System GBU-31 (2000lb JDAM) 5 GBU-39 (250lb SDB I) 20 GBU-38 (500lb JDAM) 9 GBU-39 (250lb SDB II) 20 GBU-54 (500lb L-JDAM) 7 AGM-65 6 GBU-10 5 AGM-158A (JASSM) 3 GBU-12 11 AGM-130 2 GBU-15 2 AGM-154 3 GBU-24 5 MK-82 12 GBU-27 6 MK-84 7 GBU-28 2 CBU-87/89/97 12 AIM-9X 4 CBU-103/104/105/107 9 AIM-120 AMRAAM 8 B61-3/4/10 6 Initial operating capability - September 1989 Inventory Total force, 217 Contractor / Status / Improvements / Special Equipment: Contractor - The Boeing Company Status Inventory Management/Engineering: 912 AESG, WPAFB, OH

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Nomenclature: F-16

Name: Fighting Falcon

Capability: The F-16 Fighting Falcon is a compact, multi-role fighter aircraft. It is highly maneuverable and has proven itself in air-to-air combat and air-to-surface attack. It provides a relatively low-cost, high-performance weapon system for the United States and allied nations. The F-16’s safety, survivability, and combat readiness statistics through sustained deployments under less than ideal conditions remains second to none. The F-16 continues to be used in support of the following rolls: Strategic Attack Interdiction Close Air Support Counter-Air Tactical Ballistic Missile Destruction SEAD (Suppression of Enemy Air Defense) DEAD (Destruction of Enemy Air Defense) Reconnaissance Description: In an air combat role, the F-16's maneuverability and combat radius (distance it can fly to enter air combat, stay, fight and return) exceed that of all potential threat fighter aircraft. It can locate targets in all weather conditions and detect low flying aircraft in radar ground clutter. In an airto-surface role, the F-16 can fly more than 500 miles (860 kilometers), deliver its weapons with superior accuracy, defend itself against enemy aircraft, and return to its starting point. An allweather capability allows it to accurately deliver ordnance during non-visual bombing conditions. In designing the F-16, advanced aerospace science and proven reliable systems from other aircraft such as the F-15 and F-111 were selected. These were combined to simplify the airplane and reduce its size, purchase price, maintenance costs and weight. The light weight of the fuselage is achieved without reducing its strength. With a full load of internal fuel, the F-16 can withstand up to nine G's -- nine times the force of gravity -- which exceeds the capability of most other current fighter aircraft. In addition, the integral ―lifting body‖ fuselage design coupled with incremental structural improvements has allowed payload capacity to increase to a gross weight of 52,000 lbs without increasing the size of the aircraft. The cockpit and its bubble canopy give the pilot unobstructed forward and upward vision, and greatly improved vision over the side and to the rear. The seat-back angle was expanded from the usual 13 degrees to 30 degrees, increasing pilot comfort and gravity force ―g‖ tolerance. The pilot has excellent flight control of the F-16 through its quad-redundant "fly-by-wire" system. Electrical wires relay commands, replacing the usual cables and linkage controls leaving the F-16 more tolerant to battle damage. For easy and accurate control of the aircraft during high G-force combat maneuvers, a side stick controller is used instead of the conventional center-mounted stick. Hand pressure on the side stick controller sends electrical signals to actuators of flight control surfaces such as flaperons, horizontal tails, and rudder. Avionics systems include a highly accurate, SAASM capable, GPS aided, inertial navigation system in which a computer provides steering information to the pilot. The plane has UHF and VHF radios, platform data-linking, plus an instrument landing system. It also has a detection / warning system and modular countermeasure pods and dispensers to be used against airborne or surface electronic threats. The fuselage has space for additional avionics systems and later models include an elongated dorsal for even more avionics and optional conformal fuel tanks (CFTs).

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Characteristics: Primary Function - Dual role tactical fighter and air-to-ground attack aircraft Power plant F-16C/D: one Pratt and Whitney F100-PW-200/220/229 or General Electric F110-GE-100/129 Thrust F-16C/D, 24,500-29,000 pounds Wingspan 32 feet, 8 inches (9.8 meters) Length 49 feet, 5 inches (14.8 meters) Height 16 feet (4.8 meters) Weight 19,700 pounds (through Blk 50) without fuel (8,936 kilograms) 20,700 pounds (Blk 52C) 22,100 pounds (Blk 52D) Max Takeoff Weight 42,500 pounds (1931 kilograms) (Through Blk 50) 52,000 pounds (Blk 52C/D) Fuel Capacity 7,000 pounds internal (3,175 kilograms); typical capacity, 12,000 pounds (through Blk 50) with two ext 370 gal tanks (5443 kilograms) Blk 52C capacity 17,100 lbs with 600 gal tanks and CFTs (2900 lbs) Payload Mission dependant Speed 1,500 mph (Mach 2 at altitude) Range More than 2,002 miles ferry range (1,740 nautical miles) Ceiling Above 50,000 feet (15 kilometers) (Operational Limit is 50K’) Crew F-16C, one; F-16D, one or two Armament - One M-61A1 20mm multi-barrel cannon with 500 rounds; external stations can carry up to six air-to-air missiles with conventional or nuclear air-to-surface munitions with electronic countermeasure pods and navigation/targeting pods Maximum Load by Weapon AIM-120 AMRAAM GBU-31 (2000lb JDAM) GBU-54 (500lb L-JDAM) GBU-10 (2000lb LGB) GBU-39 (250lb SDB I) AGM-158A (JASSM) CBU-103/104/105(WCMD) AGM-88 (HARM) SLAM-ER

6 2 4 2 8 2 4 2 2

AIM-9X GBU-38 (500lb JDAM) GBU-24 (2000lb LGB) GBU-12 (500lb LGB) GBU-39 (250lb SDB II) AGM-154 (JSOW) AGM-65 Harpoon

2 4 2 4 8 2 2 2

Initial operating capability - F-16A, January 1979; F-16C/D Block 25-32, 1981; F-16C/D Block 40-42, 1989; and F-16C/D Block 50-52, 1994 Inventory Total force, F-16C/D, 1,280 Contractor / Status / Improvements / Special Equipment: Contractor Lockheed Martin Corp. Status USAF Inventory Notes - Also operated by the USN and 25 Nations world-wide. There are 250 different and unique configurations with more than 4400 aircraft delivered.

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Management/Engineering: 312 AESG (Block 40/50), WPAFB, OH 501 ACSS/GFLA (Block 25/30/32), Hill AFB, UT

F16 Blk 62

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Nomenclature: F-22A

Name: Raptor

Capability: The F-22A Raptor is the Air Force's newest fighter aircraft. Its combination of stealth, super cruise, maneuverability, and integrated avionics, coupled with improved supportability, represents an exponential leap in warfighting capabilities. The Raptor performs both air-to-air and air-to-ground missions allowing full realization of operational concepts vital to the 21st century Air Force. The F-22A, a critical component of the Global Strike Task Force, is designed to project air dominance, rapidly and at great distances and defeat threats attempting to deny access to our nation's Air Force, Army, Navy and Marine Corps. The F-22A cannot be matched by any known or projected fighter aircraft. Description: A combination of sensor capability, integrated avionics, situational awareness, and weapons provides first-kill opportunity against threats. The F-22A possesses a sophisticated sensor suite allowing the pilot to track, identify, shoot and kill air-to-air threats before being detected. Significant advances in cockpit design and sensor fusion improve the pilot's situational awareness. In the air-to-air configuration the Raptor carries six AIM-120 AMRAAMs and two AIM-9 Sidewinders. The F-22A has a significant capability to attack surface targets. In the air-to-ground configuration the aircraft can carry two 1,000-pound GBU-32 Joint Direct Attack Munitions (JDAM) internally and will use on-board avionics for navigation and weapons delivery support. In the future air-to-ground capability will be enhanced with the addition of an upgraded radar and up to eight small diameter bombs. The Raptor will also carry two AIM-120s and two AIM-9s in the air-to-ground configuration. Advances in low-observable technologies provide significantly improved survivability and lethality against air-to-air and surface-to-air threats. The F-22A brings stealth into the day, enabling it not only to protect itself but other assets. The F-22A engines produce more thrust than any current fighter engine. The combination of sleek aerodynamic design and increased thrust allows the F-22A to cruise at supersonic airspeeds (greater than 1.5 Mach) without using afterburner -- a characteristic known as supercruise. Supercruise greatly expands the F-22A's operating envelope in both speed and range over current fighters, which must use fuel-consuming afterburner to operate at supersonic speeds. The sophisticated F-22A aero-design, advanced flight controls, thrust vectoring, and high thrustto-weight ratio provide the capability to outmaneuver all current and projected aircraft. The F-22A design has been extensively tested and refined aerodynamically during the development process. Characteristics: Primary Function Power plant Thrust Wingspan Length Height Weight -

Air dominance, multi-role fighter Two Pratt & Whitney F119-PW-100 turbofan engines with afterburners and two-dimensional thrust vectoring nozzles. 35,000-pound class (each engine) 44 feet, 6 inches (13.6 meters) 62 feet, 1 inch (18.9 meters) 16 feet, 8 inches (5.1 meters) 43,340 pounds (19,700 kilograms)

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Max Takeoff Weight Fuel Capacity -

83,500 pounds (38,000 kilograms) Internal: 18,000 pounds (8,200 kilograms); with 2 external wing fuel tanks: 26,000 pounds (11,900 kilograms) Payload Same as armament air-to-air or air-to-ground loadouts; with or without 2 external wing fuel tanks. Speed Mach 2 class with supercruise capability Range More than 1,850 miles ferry range with 2 external wing fuel tanks (1,600 nautical miles) Ceiling Above 50,000 feet (15 kilometers) Crew One Armament - One M61A2 20-millimeter cannon with 480 rounds, internal side weapon bays carriage of two AIM-9 infrared (heat seeking) air-to-air missiles and internal main weapon bays carriage of six AIM-120 radar-guided air-to-air missiles (air-to-air loadout) or two 1,000-pound GBU-32 JDAMs and two AIM-120 radar-guided airto-air missiles (air-to-ground loadout) Initial operating capability - December 2005 Inventory Total force, 91

F-22A Loadouts

Contractor / Status / Improvements / Special Equipment: Contractor - Lockheed-Martin, Boeing Status Production

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Management/Engineering: 778 AESG, WPAFB, OH

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Nomenclature: F-35

Name: Joint Strike Fighter (JSF) (Lightning II)

Capability: F-35 Lightning II is a fifth-generation, single-seat, single-engine, stealth-capable military strike fighter, a multirole aircraft that can perform close air support, tactical bombing, and air superiority fighter missions. The JSF aircraft design has three variants: conventional takeoff and landing variant for the Air Force, aircraft carrier-suitable variant for the Navy, and short takeoff and vertical landing variant for the Marine Corps. The United Kingdom, Italy, Australia, Canada, Denmark, Netherlands, Norway and Turkey are partnered with the U.S. and involved in the F-35 development. These aircraft are intended to replace aging fighter and attack aircraft currently in the inventory. Description: Integral to the aircraft’s low-observable equation is the large internal-weapons bay. When stealth is not required, the F-35 also can carry wingtip air-to-air missiles and up to 15,000 pounds of external ordnance mounted on underwing pylons. A pneumatically powered ordnance-release system replaces the traditional cartridge-powered equipment. This new design greatly reduces maintenance requirements. The 25 mm cannon will enable pilots to engage targets from higher altitudes and longer range. The F-35’s mission systems are designed to return the pilot to the role of tactician and to increase combat effectiveness dramatically. Next-generation sensors will provide the pilot coherent and fused information from a variety of onboard and off-board systems. Sophisticated data links will connect the aircraft to both ground-combat elements and airborne platforms. In addition to fighter-to-fighter data links, the F-35 will be equipped with satellite-communications capability for both transmitting and receiving. The aircraft’s onboard sensor suite is optimized to locate, identify, and destroy movable or moving ground targets under adverse weather conditions. This all-weather capability is achieved with the aircraft’s advanced electronically scanned array (AESA) radar built by Northrop Grumman. The AESA enables simultaneous air-to-ground and air-to-air operations. It can track moving ground targets and display them on a radar-generated terrain image, enabling precise target location relative to terrain features. These instruments, coupled with off-board sensors, will make the F-35 capable of all-weather close air support under the most demanding conditions. The JSF program was created to replace various aircraft while keeping development, production, and operating costs down. This was pursued by building three variants of one aircraft, sharing 80% of their parts: F-35A, a conventional takeoff and landing (CTOL) variant slated to replace U. S. Air Force (USAF) F-16 Fighting Falcons. Initial Operating Capability - 2013. F-35B, a short-takeoff and vertical-landing (STOVL) variant slated to replace the U. S. Marine Corps (USMC) AV-8 Harrier IIs and F/A-18 Hornets. Initial Operating Capability - 2012. F-35C, a carrier-based variant slated to replace U.S. Navy (USN) F/A-18 Hornets (A/B/C/D variants only). Initial Operating Capability - 2015. Characteristics: Primary Function Power plant Thrust -

Air dominance, multi-role fighter 1 × Pratt & Whitney F135 afterburning turbofan With afterburner: 40,000 lbf

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Secondary Powerplant Thrust Lift fan (STOVL) Wingspan Sing area Length Height Weight -

Max Takeoff Weight Fuel Capacity (internal) Payload Speed Range Ceiling Crew -

1 x General Electric/Roles-Royce F136 Afterburning turbofan With afterburner: 40,000 lbf 1 x Rolls-Royce Lift System driven from either F135 or F136 power plant, (18,000 lbf thrust) 35 ft 459.6 ft 50ft 6 in 17 ft 4 in A: 29,036 lb B: 32,161 lb C: 32,070 60,000 lb A: 18,480 lb; B: 14,003 lb: C: 20,085 Max Speed: Mach 1.6+ (1,200 mph) A: 1,200 nmi; B: 900 nmi; C: 1,400 nmi 1

Armament - 1 × GAU-22/A 25 mm cannon slated to be mounted internally w/180 rounds in the in the F-35A and a fitted external pod with 220 rounds in the F-35B and F-35C. Hardpoints: 6 with a capacity of 15,000 lb (6,800 kg) Missiles: Internal: 4 air-to-air missiles or 2 air-to-air missiles and 2 air-to-ground missiles. External: 6 air-to-air missiles or 4 air-to-ground weapons and 2 air-to-air missiles. Initial operating capability - 2012 Inventory - 3137 (planned Contractor / Status / Improvements / Special Equipment: Contractor - Lockheed Martin; Northrop Grumman; BAE Systems Status Production Management/Engineering: JSF/PO, Arlington VA

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Nomenclature: F/A-18A/D

Name: Hornet

Capability: The F/A-18 Hornet is a modern all-weather carrier-capable strike fighter jet, designed to attack both ground and aerial targets. Description: The F/A-18 Hornet is an all-weather fighter/attack aircraft built by Boeing, operated primarily by the USN/USMC for carrier operations, but also exported to multi-national interests. The aircraft is powered by two General Electric F404-GE-400 or F404-GE-402 (enhanced performance) turbofan engines with afterburner. The flight control surfaces operate via a ―fly by wire‖ system. Pilot-commanded control stick and rudder inputs are forwarded to two flight control computers, which in turn generate signals that allow for 3000-psi hydraulic-actuated control surface movement to give the pilot optimum flying qualities and handling performance in both the up and away and powered approach configurations. Pilot-controlled HOTAS (Hands-on-Throttle and Stick) allow for ease in pilot workload when operating mission essential systems. A HUD (Head-up-Display) provides the aircrew with accurate aircraft altitude, airspeed, and heading along with timely weapon employment parameters. Three cockpit digital display indicators (DDIs) enable the aircrew to process multiple aircraft and weapons parameters with relative ease. The Hornet has three distinct master modes: Navigation (NAV), Air-to-Air (A/A), and Air-toGround (A/G). NAV master mode is used primarily during administrative phases of flight, while the A/A and A/G modes can quickly be toggled to attack both airborne and ground targets. A total of nine wingtip, fuselage, and pylon stations are available for weapon placement. The fuselage stations are used to house air-to-air weapons and various targeting pods. The Hornet is capable of employing AIM-9, AIM-7, and AIM-120 A/A missiles and has provisions for chaff and flare dispensing. A/G weapons include general purpose bombs, GPS- and laser-guided munitions, Maverick, Rockeye, rockets, mines, and a host of Joint weapons. A 20-mm gun and multi-mode radar are located in the nose of the aircraft. External fuel tanks may be placed on the inboard and centerline stations for added endurance capability. F/A-18A, A+ and C models are single seat aircraft, while the F/A-18B, D, and Reconnaissance Configured F/A-18D, D(RC), can accommodate a crew of two. Currently, only the F/A-18A+, C, D and D(RC) models are capable of Joint weapons employment. The F/A-18A+ model is an upgraded version of the F/A-18A. F/A-18A+ upgrades include, but are not limited to: radar, AIM-120 AMRAAM, AIM-9X, GPS, ATFLIR, MIDS, CIT, OBOGS, and enhanced MUX bus capability. The F/A-18D(RC) is able to provide day and night, all weather, high-resolution imaging capabilities. The F/A-18D(RC) uses electro-optical (EO), infrared (IR), and synthetic aperture radar (SAR) sensors to gather image data. In addition, the Advanced Tactical Reconnaissance System (ATARS) sensor suite is installed in the nose bay in place of the 20-mm gun. Characteristics: Primary Function Power plant Thrust Wingspan Wing Area Length -

Dual role tactical fighter and air-to-ground attack aircraft Two F404-GE-400 or F404-GE-402 afterburning engines after burner: 17,500 lbf ; dry thrust: 11,000 lbf 40 ft 400 ft² 56 ft

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Height Weight -

15 ft 4 in Empty weight: 24,700 lb Loaded weight: 37,150 lb Max Takeoff Weight 51,550 lb Fuel Capacity Internal Speed F/A-18C/D maximum speed Mach 1.8 (1,190 mph) at level flight in altitudes of 36,089 ft. Range 2,070 mi (ferry), Combat radius 330 mi Ceiling 50,000 ft Crew F/A-18A/C: 1; F/A-18B/D: 2 (pilot and Weapons System Officer (WSO) Armament - M61A1 or M61A2 Vulcan 6-barrel rotary cannon with 578 rounds of 20mm ammunition is internally mounted in the nose F/A-18A-D has 9 hardpoints (2 wingtip, 4 underwing, and 3 fuselage, carrying up to 13,700 lb of missiles, rockets, bombs, fuel tanks, and pods: Missiles: 2 x AIM-9 Sidewinders on wingtips AIM-120 AMRAAM AIM-7 Sparrow AGM-88 HARM AGM-65 Maverick Missiles AGM-84D Harpoon AGM-84K SLAM-ER AGM-154 Joint Stand-Off Weapon (JSOW) Bombs: Joint Direct Attack Munition (JDAM) Paveway laser guided bombs Mk 80 Series GP bombs Mk-20 Rockeye II and CBU-series cluster bombs Avionics APG-73 Radar Litening targeting pod (USMC only) Initial operating capability - F/A-18A/B USN and USMC in 1982 F/A-18C/D 1987 Inventory Contractor / Status / Improvements / Special Equipment: Contractor - Boeing [McDonnell Douglas Aerospace] and Northrop Grumman (Airframe), General Electric (Engines), and Hughes (Radar) Status Inventory Management/Engineering: Naval Air Systems Command Patuxent River, MD

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Nomenclature: F/A-18E/F

Name: Super Hornet

Capability: The multi-mission F/A-18E/F "Super Hornet" strike fighter is an upgrade of the combat-proven night strike F/A-18C/D. The Super Hornet will provide the battle group commander with a platform that has range, endurance, and ordnance carriage capabilities comparable to the A-6 which have been retired. The Super Hornet performs both air-to-air and air-to-ground missions as well as strike tanker mission. Description: The multi-mission F/A-18E/F "Super Hornet" strike fighter is an upgrade of the combat-proven night strike F/A-18C/D. The F/A-18E/F aircraft are 4.2 feet longer than earlier Hornets, have a 25% larger wing area, and carry 33% more internal fuel which will effectively increase mission range by 41% and endurance by 50%. The Super Hornet also incorporates two additional weapon stations. This allows for increased payload flexibility by mixing and matching air-to-air and/or air-to-ground ordnance. The aircraft can also carry the complete complement of "smart" weapons, including the newest joint weapons such as JDAM and JSOW. The Super Hornet can carry approximately 17,750 pounds (8,032 kg) of external load on eleven stations. It has an all-weather air-to-air radar and a control system for accurate delivery of conventional or guided weapons. There are two wing tip stations, four inboard wing stations for fuel tanks or air-to-ground weapons, two nacelle fuselage stations for Sparrows or sensor pods, and one centerline station for fuel or air-to-ground weapons. An internal 20 mm M61A1or M61A2 Vulcan cannon is mounted in the nose. Carrier recovery payload is increased to 9,000 pounds, and its engine thrust from 36,000 pounds to 44,000 pounds utilizing two General Electric F414 turbo-fan engines. Although the more recent F/A-18C/D aircraft have incorporated a modicum of low observables technology, the F/A-18E/F was designed from the outset to optimize this and other survivability enhancements. The F/A-18C and F/A-18E are single seat aircraft. The D and F models are flown by two crew members. The aft seat in the D and F may be configured with a stick and throttle for the training environment (or without when crewed with a Weapons System Officer). Characteristics: Primary Function Power plant Dry Thrust Thrust w/afterburner Wing Span Wing area Length Height Weight Max Takeoff Weight Fuel Capacity Payload Max Speed Range -

Dual role tactical fighter and air-to-ground attack aircraft Twin F414-GE-400 engines 14,000 lb 22,000 lb 44.9 ft 500 ft² 60 ft 1 ¼ in 16 ft Empty weight: 30,564 lb Loaded weight: 47,000 lb 66,000 lb Internal F/A-18E: 14,400 lb, F/A-18F: 13,550 lb External Fuel: 5 X 480 gal tanks, totaling 16,380 lb Mach 1.8+ (1,190mph, 1900 km/h) at 40,000 ft 1,275 nmi (2,346 km) clean plus two AIM-9s Ferry range: 1,800 nmi (2,070 mi; 3,330 km)

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Ceiling 50,000 + ft Crew F/A-18E: 1, F/A-18 F: 2 Armament - 6-barrel rotary cannon with 520 rounds of 20mm ammunition is internally mounted in the nose F/A-18E/F has 11 hardpoints with a capacity of 17,750 pounds of external ordnance with provisions to carry combinations of: Missiles: 2 x Aim-9 Sidewinders on wingtips Aim-120 AMRAAM AIM-7 Sparrow AGM-88 HARM AGM-65 Maverick Missiles AGM-84D Harpoon AGM-84K SLAM-ER AGM-154 Joint Stand-Off Weapon (JSOW) Bombs: Joint Direct Attack Munition (JDAM) Paveway laser guided bombs MK 80 Series GP bombs MK-20 Rockeye II and CBU-series cluster bombs Initial operating capability - 1999 Inventory 350 (460 by 2012) Contractor / Status / Improvements / Special Equipment: Contractor - Boeing [McDonnell Douglas Aerospace] and Northrop Grumman (Airframe), General Electric (Engines), and Hughes (Radar) Status Production Management/Engineering: Naval Air Systems Command Patuxent River, MD

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Nomenclature: EA-18G

Name: Airborne Electronic Attack Aircraft “Growler”

Capability: The EA-18 will perform full-spectrum electronic surveillance and electronic attack of enemy threat radars and communications nets. Description: The EA-18 will perform full-spectrum electronic surveillance and electronic attack of enemy threat radars and communications nets. The EA-18 leverages the U.S. Navy's investment in the F/A-18E/F Super Hornet platform. A derivative of the two-seat F/A-18F Super Hornet - a platform which is in production today - the EA-18 is a highly flexible design that enables the warfighter to perform a broad range of tactical missions, operating from either the deck of an aircraft carrier or land-based fields. The EA-18 is 99 percent common with the Super Hornet and would be expected to significantly reduce support and training costs for the US Navy. The EA-18G’s electronic attack upgrades will meet EA-6B (ALQ-218, ALQ-99, USQ-113) Airborne Electronic Attack (AEA) capability to detect, identify, locate and suppress hostile emitters; provide enhanced connectivity to National, Theater and Strike assets; and provide organic precision emitter targeting for employment of onboard suppress ion weapons High-speed Anti-Radiation Missile (HARM) to fulfill operational requirements. The man in the loop operation and advanced information display system will allow real time assessment of the tactical situation and the appropriate response executed in accordance with the rules of engagement. The performance of the aircraft is compatible with the primary strike/fighter aircraft projected to be in the inventory in the 2010 time period, allowing it to be fully integrated into specific strike packages. It will also have the capacity to provide broad area coverage for extended periods of time to support numerous strikes or other air operations in a federated context. The EA-18G is being designed to perform a range of Electronic Warfare/Electronic Attack functions either simultaneously or independently. Characteristics: Primary Function Power plant Thrust Wingspan Sing Area Length -

Full-spectrum electronic surveillance and electronic attack of enemy threat radars and communications nets. 2 x General Electric F414-GE-400 turbofans 22,000 lbf each (afterburner); 14,000 lbf (dry thrust) 44 ft 8.5 in 500 ft² 60 ft 1.25 in

Height Empty weight Loaded weight Max Takeoff Weight -

16 ft 30,564 lb 47,000 lb 66,000 lb

Fuel capacity Speed Range Ceiling Crew Armament -

Internal: 14,000 lb; External: 5 480 gal tanks Mach 1.8 (1,190mph) at 40,000 ft 1,275 nmi; combat radius 390 nm; ferry range 1,800 nmi 50,000 ft 2 Phase I Growler will carry the AIM-120 AMRAAM for self-protection and AGM-88 HARM missiles. The 20 mm M61A1 cannon has been replaced by a pod of electronic boxes that control the AN/ALQ-218 and assist with the coordination AN/ALQ-99 jamming attacks.

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Initial operating capability Inventory Contractor / Status / Improvements / Special Equipment: Contractor - Boeing [McDonnell Douglas Aerospace] and Northrop Grumman (Airframe), General Electric (Engines), and Hughes (Radar) Status Production Management/Engineering: Naval Air Warfare Center Aircraft Div Patuxent River, MD

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Nomenclature: AV-8B

Name: Harrier II

Capability: The mission of the VMA STOVL squadron is to attack and destroy surface and air targets, to escort helicopters, and to conduct other such air operations as may be directed. Description: The AV-8B Harrier is a single-seat, light attack aircraft that provides close air support/intermediate range intercept/attack mission support to the Marine Air-Ground Task Force (MAGTF). By virtue of its Vertical/Short Take-Off or Landing (V/STOL) capability, the AV8B can operate from a variety of amphibious ships, rapidly constructed expeditionary airfields, forward sites (e.g., roads), and damaged conventional airfields. This makes the aircraft particularly well-suited for providing dedicated close air support. The AV-8BII+ features the APG-65 Radar common to the F/A-18, as well as all previous systems and features common to the AV-8BII. Air-to-surface weapons systems include: digital targeting data link, global positioning system, and the Litening II Targeting system. The AV-8B can carry and deliver an assortment of conventional stores such as the Mk 82 500 pound bomb, Mk 83 1,000 pound GP bomb, GBU-12 500 pound LGB, GBU-16 1,000 LGB, next-generation, precision-guided munitions, including the joint direct attack munition (JDAM), CBU-99 and CBU-78 Cluster Bomb Units, and 2.75" and 5" rockets. The NA configuration includes: night vision goggle-compatible cockpit controls and displays, a wide-field-of-view HUD, a Navigation Forward Looking Infrared (NAVFLIR) system, a Digital Map Unit (DMU), and an Angle Rate Bombing System (ARBS) with laser spot tracker, which provides first pass day or night target strike capability at low altitude/high speed. The Radar aircraft retains all night attack capability but integrates the AN/APG-65 radar system to extend the tracking capabilities of the aircraft for A/G delivery and A/A defense modes. V/STOL capability allows the AV-8B to be deployed with ground units using amphibious shipping and/or forward basing for rapid close air support response. Characteristics: Primary Function Power plant -

Thrust Wingspan Length Height Weight Max Takeoff Weight Fuel Capacity Payload Speed Range Ceiling Crew -

Dual role tactical fighter and air-to-ground attack aircraft TAV-8B/AV-8B Day Attack (DA): One Rolls Royce Pegasus F402-RR-406 turbofan engine with approx 20,280 pounds of thrust AV-8B Night Attack (NA)/AV-8B Radar: One Rolls Royce Pegasus F402-RR-408A turbofan engine with approx 23,500 pounds of thrust 20,280 - 23,500 lbs 30 ft 3 in 46 ft 3 in 11 ft 7 in 12,800 lb (empty) 31,000 lb (short takeoff) 18,900 (vertical takeoff) 9,000 lb 630 mph 900 nautical miles 1,700 mile (ferry) AV-8B DA/NA/Radar Aircraft: 1, pilot only; TAV-8B Trainer: 2

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Armament -

One fuselage-mounted 25 mm gun system Standard Air-to-Ground (A/G) load: Six Mk 82, 500 pound bombs Standard Air-to-Air (A/A) load: Four AIM-9M Sidewinder missiles Provisions for carrying up to 9,000 lbs of ordnance on seven stations Initial operating capability - Jan 1985 Contractor / Status / Improvements / Special Equipment: Contractor - Boeing Aircraft (Airframe Prime), Rolls Royce (Engine Prime) Status Inventory Management/Engineering: Naval Air Warfare Center Aircraft Div Patuxent River, MD

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Nomenclature: EA-6B

Name: Prowler

Capability: The EA-6B Prowler provides an umbrella of protection for strike aircraft, ground troops and ships by jamming enemy radar, electronic data links and communications. Other mission profiles include carrying out electronic surveillance tasks, armed reconnaissance, and providing defense against incoming anti-ship missiles. The Prowler has the ability to passively detect enemy radar without making its own presence known. Description: The U.S. Navy EA-6B Prowler electronic warfare aircraft enhances the strike capabilities not only of carrier air wings but of U.S. Air Force and allied forces as well. The EA-6B carries the ALQ-99 Tactical Jamming System, which includes a receiver, processor, and various missionconfigured jammer pods carried as external stores. The EA-6B has the USQ-113 Communications Jammer, and may also be armed with the highspeed anti-radiation missile (HARM) for enemy surface-to-air radar destruction and suppression. The EA-6B is a key contributor to the Suppression of Enemy Air Defenses Electronic Attack mission. Its ability to monitor the electromagnetic spectrum and actively deny an adversary's use of radar and communications is unmatched by any airborne platform worldwide. The Prowler can carry up to five pods (one belly mounted and two on each wing). Each pod is integrally powered and houses two jamming transmitters that cover one of seven frequency bands. The EA-6B can carry any mix of pods, fuel tanks and/or HARM anti-radiation missiles depending on mission requirements. The EA-6B's tail fin pod houses sensitive surveillance receivers, capable of detecting hostile radar emissions at long range. Emitter information is processed by the central mission computer. Detection, identification, direction-finding, and jammer-set-on-sequence may be performed automatically or by the crew. The Prowler has a crew of four, a pilot and three Electronic Counter-measures Officers (known as ECMOs). Characteristics: Primary Function Power plant Thrust Wingspan Length Height Weight -

Electronic Attack Two Pratt & Whitney J52-P408A turbojet engines 11,200 pounds (4,767 kilograms) per engine 53 feet (16.15 meters) 59 feet (17.98 meters) 15 feet (4.57 meters) 33,600 lbs empty Max Takeoff Weight - 61,500 lbs

Fuel Capacity Payload Speed Range Ferry Range Ceiling -

Maximum 651 mph (.99 mach; cruise .72 mach) 850 nautical miles (977.5 miles) 1,747 (5 drop tanks) 40,000 feet - maximum (12,186 meters) 37,600 feet - Service ceiling Crew 4 - Pilot and 3 electronic countermeasures officers Armament ALQ-99 Tactical Jamming System (TJS) Up to Four High Speed Anti-Radiation Missiles (HARM) Initial operating capability - 1984 Inventory 120 total

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Contractor / Status / Improvements / Special Equipment: Contractor - Grumman Aircraft Corporation Status Inventory Management/Engineering: Naval Air Warfare Center Aircraft Div Patuxent River, MD

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Nomenclature: P-3C

Name: Orion Maritime Patrol and Anti-Submarine Warfare Aircraft

Capability: Antisubmarine warfare (ASW)/Antisurface warfare (ASUW). P-3C's primary mission is to track and eliminate ballistic missile and fast attack submarines. Additional missions include surveillance and reconnaissance. Description: Originally designed as a land-based, long-range, anti-submarine warfare (ASW) patrol aircraft, the P-3C's mission has evolved in the late 20th and early 21st century to include surveillance of the battlespace, either at sea or over land. Its long range and long loiter time have proved invaluable assets during Operation Iraqi Freedom as it can view the battlespace and instantaneously provide that information to ground troops, especially U.S. Marines. The P-3C has advanced submarine detection sensors such as directional frequency and ranging (DIFAR) sonobuoys and magnetic anomaly detection (MAD) equipment, as well as electro-optical sensors. The avionics system is integrated by an upraded general purpose digital computer that supports all of the tactical displays, monitors and automatically launches ordnance and provides flight information to the pilots. In addition, the system coordinates navigation information and accepts sensor data inputs for tactical display and storage. Other avionics improvements include electronic flight data system (glass cockpit) instruments and improved communication equipment and navigation sensors. The P-3C's anti-submarine warfare systems include the AN/ARR-78(V) sonobuoy receiving system, the AN/ARR-72 sonobuoy receiver, two AQA-7 directional acoustic frequency analysis and recording sonobuoy indicators, and a AQH-4 (V) sonar tape recorder. Advanced aircraft are equipped with the UYS-1/USQ-78 acoustic system and an infrared detection system. The sensor suite also includes an ASQ-81 magnetic anomaly detector and an ASA-65 magnetic compensator. Sonobuoys are launched from within the main cabin and from external launching chutes. The airborne electronic surveillance receiver, ALQ-78(V) is carried on a pylon under the wing fairing. The ALQ-78(V) automatically operates in search mode, its target primarily being submarine radars. When a submarine radar signal is detected the system is switched to direction finding mode and the received signals are characterized. The latest aircraft are equipped with Raytheon AN/APS-137(V) multi-mission surveillance radar and ALR-95 ECM. Some P-3C aircraft are equipped with the ALR-47/ALE-47 missile warning system. The P-3C can carry a mixed payload of weapons internally and on ten underwing pylons. The bomb bay is in the underside of the fuselage forward of the wing. It is capable of carrying 1000 lb. and 2,000 lb. mines such as the mk25\mk52/mk62/mk63/mk56. The aircraft may also carry depth bombs, mk 46/50/54 torpedoes, Rockeye, Maverick, Harpoon and SLAM-ER. The underwing pylons can carry 2,000 lb. mines, torpedoes, rockets, rocket pods and 500lb mines. Characteristics: Primary Function Power plant Wingspan Length Height Max Takeoff Weight Payload Speed -

Anti-Submarine warfare (ASW)/Anti-Surface Warfare (ASUW) four Rolls Royce T56-A-14 turboprop engines, 4600 hp each 99.6 ft 116.7 ft 33.7 ft 139,760 lbs 20,000 lb Max: 405 knots; Cruise: 328 knots

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Range Ceiling Crew -

Mission Radius: 2,380 nautical miles; 28,300 ft three pilots, two naval flight officers, two flight engineers, three sensor operators, one in-flight technician. Armament 20,000 pounds of ordnance, including AGM-84 Harpoon, AGM-84E SLAM, AGM-84H/K and AGM-65F Maverick missiles, Mk46/50/54 Torpedoes, Countermeasures - expendables include: RR129/RR144/MJU8/27/3238/46/49/SM875. Initial operating capability - August 1969 Inventory 170 Contractor / Status / Improvements / Special Equipment: Contractor - Lockheed Martin Aeronautical Systems Company Status Inventory Management/Engineering: Naval Air Warfare Center Aircraft Div Patuxent River, MD (PMA-290)

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Nomenclature: AC-130H/U

Name: Gunship

Capability: The AC-130 gunship's primary missions are close air support, air interdiction and force protection. Missions in close air support are troops in contact, convoy escort and urban operations. Air interdiction missions are conducted against preplanned targets or targets of opportunity. Force protection missions include air base defense and facilities defense. Description: These heavily armed aircraft incorporate side-firing weapons integrated with sophisticated sensor, navigation and fire control systems to provide surgical firepower or area saturation during extended loiter periods, at night and in adverse weather. The sensor suite consists of a television sensor, infrared sensor and radar. These sensors allow the gunship to visually or electronically identify friendly ground forces and targets any place, any time. The AC-130U employs synthetic apertures strike radar for long-range target detection and identification. The gunship's navigational devices include the inertial navigation systems and global positioning system. Both the AC-130s employ the latest technologies and can attack two targets simultaneously. The AC-130H's call sign is "Spectre." The AC-130U's call sign is "Spooky.‖ The U-model is the third generation of C-130 gunships. All gunships evolved from the first operational gunship, the AC-47. Characteristics: Primary Function Power plant Thrust Wingspan Length Height Max Takeoff Weight Speed Range Ceiling Crew -

Close air support, air interdiction and force protection Four Allison T56-A-15 turboprop engines 4,910 shaft horsepower each engine 132 feet, 7 inches (40.4 meters) 97 feet, 9 inches (29.8 meters) 38 feet, 6 inches (11.7 meters) 155,000 pounds (69,750 kilograms) 300 mph (Mach .4) (at sea level) Approximately 1,300 nautical miles; unlimited with air refueling. 25,000 feet (7,576 meters) AC-130U - pilot, co-pilot, navigator, fire control officer, electronic warfare officer (officers) and flight engineer, TV operator, infrared detection set operator, loadmaster, and four aerial gunners (enlisted) Armament AC-130H: 40mm and 105mm cannons; AC-130U: 40mm and 105mm cannons and 25mm Gatling Gun. Counter Measures - The AC-130U/H carries 20 Countermeasure Dispensers. These 20 will be a combination of MJU-11 Chaff/Flare Magazines and MJU-12 Flare Magazines. MJU-11 Chaff/Flare Magazine: each magazine can hole 30 ea RR-170 or RR-188 Chaff Cartridges or 30 ea M206 Flares 0r 30 M206(T-2) Flare Simulators MJU-12 Flare Magazine: each magazine can hold 15 ea MJU-7/B Flares or 15 ea MJU-7A/B Flares or 15 MJU-7(T-2)B Flare Simulators Initial operating capability - Deployment Date: AC-130H, 1972; AC-130U, 1995 Inventory Active duty, AC-130H, 8; AC-130U, 17; Reserve, 0; ANG, 0

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Contractor / Status / Improvements / Special Equipment: Contractor - Lockheed/Boeing Corp. Status Inventory Management/Engineering: 572 ACSS/GFLA, Robins AFB, GA

AC-130H

AC-130U

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Nomenclature: HC-130P/N

Name: Hercules

Capability: Its mission is to extend the range of combat search and rescue helicopters by providing air refueling in hostile or contested airspace if required. Secondary mission capabilities include performing tactical delivery via airdrop or airland of pararescue specialist teams, small bundles, zodiac watercraft, or four-wheel drive all-terrain vehicles; and providing direct assistance to a survivor in advance of the arrival of a recovery vehicle. Description: The HC-130P/N is an extended-range, combat search and rescue version of the C-130 Hercules transport. Other capabilities are extended visual and electronic searches over land or water, tactical approaches and unimproved airfield operations at day or night, using night vision goggles. A team of three pararescue specialists, trained in emergency trauma medicine, harsh environment survival and assisted evasion techniques, is part of the basic mission crew complement. Combat Air Forces HC-130 aircraft are undergoing extensive modifications. Ongoing modifications include night vision goggle-compatible interior and exterior lighting, a personnel locator system compatible with aircrew survival radios, forward-looking infrared systems and advanced integrated radios. The HC-130 can fly in the day against a reduced threat; however, crews normally fly night, lowlevel, air refueling and airdrop operations using night vision goggles. It can fly low-level NVG tactical flight profiles to avoid detection. To enhance the probability of mission success and survivability near populated areas, crews employ tactics that include incorporating no external lighting or communications, and avoiding radar and weapons detection. The HC-130P/N is the only dedicated fixed-wing combat search and rescue platform in the Air Force inventory. The 71st and 79th Rescue Squadrons in Air Combat Command, the 102nd RQS and 210th RQS in the Air National Guard and the 39th RQS in the Air Force Reserve Command operate the aircraft. Characteristics: Primary Function Power plant Thrust Wingspan Length Height Weight Max Takeoff Weight Fuel Capacity Payload Speed Range Ceiling Crew -

Air refueling for combat search and rescue helicopters Four Allison T56-A-15 turboprop engines 4,910 shaft horsepower each engine 132 feet, 7 inches (40.4 meters) 98 feet, 9 inches (30.09 meters) 38 feet, 6 inches (11.7 meters) 83,000 pounds (37,648 kilograms) 155,000 pounds (69,750 kilograms) 73,000 pounds (10,724 gallons) 30,000 pounds (13,608 kilograms) 289 miles per hour (464 kilometers per hour) at sea level beyond 4,000 miles (3,478 nautical miles) 33,000 feet (10,000 meters) Three officers (pilot, co-pilot, navigator) and seven enlisted (flight engineer, airborne communications specialist, two loadmasters and three pararescuemen)

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Armament countermeasures/flares, chaff Initial operating capability - 1964 Inventory Active force, 13; ANG, 13; Reserve, 10 Contractor / Status / Improvements / Special Equipment: Contractor - Lockheed Aircraft Corp. Status Inventory Management/Engineering: 572 ACSS/GFLB, Robins AFB, GA

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Nomenclature: MC-130E/H/W

Name: Combat Talon I/II/ Combat Spear

Capability: The MC-130E Combat Talon I, MC-130H Combat Talon II, and Combat Spear provide infiltration, exfiltration and resupply of special operations forces and equipment in hostile or denied territory. Secondary missions include psychological operations and helicopter air refueling Description: The MC-130E Combat Talon I, MC-130H Combat Talon II, and Combat Spear provide infiltration, exfiltration and resupply of special operations forces and equipment in hostile or denied territory. Secondary missions include psychological operations and helicopter air refueling. An extensive electronic warfare suite enables the aircrew to detect and avoid potential threats. If engaged, the system will protect the aircraft from both radar and infrared-guided threats. The MC-130E, MC-130H, and MC-130W are equipped with aerial refueling pods to provide inflight refueling of special operations forces and combat search and rescue helicopters. The primary difference between the MC-130E, MC-130H, and MC-130W involves the degree of integration of the mission computers and avionics suite. The Combat Talon I was conceived originally and developed during the 1960s, and although extensively upgraded in the 1980-90s it still features analog instrumentation and does not fully integrate the sensors and communications suites. The Combat Talon II, designed in the 1980s, features an integrated glass flight deck which improves crew coordination and reduces the crew complement by two. The MC-130W takes a C-130H2 and adds an extensive array of electronic, mechanical, and structural modifications which gives AFSOC significantly increased capability. Characteristics: Primary Function Power plant Thrust Wingspan Length -

Height Weight Max Takeoff Weight Fuel Capacity Payload -

Speed Range Ceiling Crew -

Infiltration, exfiltration and resupply of special operations forces Four Allison T56-A-15 turboprop engines 4,910 shaft horsepower each engine 132 feet, 7 inches (40.4 meters) MC-130E: 100 feet, 10 inches (30.7 meters) MC-130H: 99 feet, 9 inches (30.4 meters) MC-130W: 98 feet, 9 inches (30.09 meters) 38 feet, 6 inches (11.7 meters) 155,000 pounds (69,750 kilograms) MC-130E: 53 troops, 26 paratroopers MC-130H:77 troops, 52 paratroopers or 57 litter patients MC-130W: 88 troops, 62 paratroops or 67 litter patients 300 mph 2,700 nautical miles (4,344 kilometers); Inflight refueling extends this to unlimited range 33,000 feet (10,000 meters) MC-130E: Two pilots, two navigators and an electronic warfare officer (officers); flight engineer, radio operator and two loadmasters (enlisted); MC-130H: Two pilots, a navigator

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and electronic warfare officer (officers); flight engineer and two loadmasters (enlisted) MC-130W: Two pilots, two navigators, flight engineer, two loadmasters Armament None Initial operating capability - MC-130E, 1966; MC-130H, June 1991; MC-130W, February 2009 Inventory Active force, MC-130H, 20, MC-130W, 12; Reserve, MC-130E, 10; ANG, 0 Contractor / Status / Improvements / Special Equipment: Contractor - Lockheed Status Inventory Management/Engineering: 572 ACSS/GFLB, Robins AFB, GA

ME-130H Combat Talon II

MC-130W Combat Spear

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Nomenclature: C-130

Name: Hercules

Capability: The C-130 Hercules primarily performs the tactical portion of the airlift mission. The aircraft is capable of operating from rough, dirt strips and is the prime transport for air dropping troops and equipment into hostile areas. The C-130 operates throughout the U.S. Air Force, serving with Air Mobility Command, Air Force Special Operations Command, Air Combat Command, U.S. Air Forces in Europe, Pacific Air Forces, Air National Guard and the Air Force Reserve Command, fulfilling a wide range of operational missions in both peace and war situations. Basic and specialized versions of the aircraft airframe perform a diverse number of roles, including airlift support, Antarctic ice resupply, aeromedical missions, weather reconnaissance, aerial spray missions, firefighting duties for the U.S. Forest Service and natural disaster relief missions. Description: Using its aft loading ramp and door the C-130 can accommodate a wide variety of oversized cargo, including everything from utility helicopters and six-wheeled armored vehicles to standard palletized cargo and military personnel. In an aerial delivery role, it can airdrop loads up to 42,000 pounds or use its high-flotation landing gear to land and deliver cargo on rough, dirt strips. The flexible design of the Hercules enables it to be configured for many different missions, allowing for one aircraft to perform the role of many. Much of the special mission equipment added to the Hercules is removable, allowing the aircraft to revert back to its cargo delivery role if desired. Additionally, the C-130 can be rapidly reconfigured for the various types of cargo such as palletized equipment, floor-loaded material, airdrop platforms, container delivery system bundles, vehicles and personnel or aeromedical evacuation. The C-130J is the latest addition to the C-130 fleet and will replace aging C-130E's. The C-130J incorporates state-of-the-art technology to reduce manpower requirements, lower operating and support costs, and provides life-cycle cost savings over earlier C-130 models. Compared to older C-130s, the J model climbs faster and higher, flies farther at a higher cruise speed, and takes off and lands in a shorter distance. The C-130J-30 is a stretch version, adding 15 feet to fuselage, increasing usable space in the cargo compartment. Characteristics: Primary Function Power plant -

Wingspan Length Height Cargo Compartment -

Speed -

Global airlift C-130E: Four Allison T56-A-7 turboprops; 4,200 prop shaft hp C-130H: Four Allison T56-A-15 turboprops; 4,591 prop shaft hp C-130J: Four Rolls-Royce AE 2100D3 turboprops; 4,700 horsepower 132 feet, 7 inches (39.7 meters) C-130E/H/J: 97 feet, 9 inches (29.3 meters) C-130J-30: 112 feet, 9 inches (34.69 meters) 38 feet, 10 inches (11. 9 meters) C-130E/H/J: length, 40 feet (12.31 meters); width, 119 inches (3.12 meters); height, 9 feet (2.74 meters). Rear ramp: length, 123 inches (3.12 meters); width, 119 inches (3.02 meters) C-130J-30: length, 55 feet (16.9 meters); width, 119 inches (3.12 meters); height, 9 feet (2.74 meters). Rear ramp: length, 123 inches (3.12 meters); width, 119 inches (3.02 meters) C-130E: 345 mph/300 ktas (Mach 0.49) at 20,000 feet C-130H: 366 mph/318 ktas (Mach 0.52) at 20,000 feet

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Max Takeoff Weight Maximum Allowable Payload -

Maximum Normal Payload -

Range at Maximum Normal Payload -

Range with 35,000 pounds of Payload -

Maximum Load troops

C-130J: 417 mph/362 ktas (Mach 0.59) at 22,000 feet C-130J-30: 410 mph/356 ktas (Mach 0.58) at 22,000 C-130E/H/J: 155,000 pounds (69,750 kilograms) C-130J-30: 164,000 pounds (74,393 kilograms) C-130E, 42,000 pounds (19,090 kilograms) C-130H, 42,000 pounds (19,090 kilograms) C-130J, 42,000 pounds (19,090 kilograms) C-130J-30, 44,000 (19,958 kilograms) C-130E, 36,500 pounds (16,590 kilograms) C-130H, 36,500 pounds (16,590 kilograms) C-130J, 34,000 pounds (15,422 kilograms) C-130J-30, 36,000 pounds (16,329 kilograms) C-130E, 1,150 miles (1,000 nautical miles) C-130H, 1,208 miles (1,050 nautical miles) C-130J, 2,071 miles (1,800 nautical miles) C-130J-30, 1,956 miles (1,700 nautical miles) C-130E, 1,438 miles (1,250 nautical miles) C-130H, 1,496 miles (1,300 nautical miles) C-130J, 1,841 miles (1,600 nautical miles) C-130J-30, 2,417 miles (2,100 nautical miles) C-130E/H/J: 6 pallets or 74 litters or 16 CDS bundles or 92 combat or 64 paratroopers, or a combination of any of these up to the

cargo

Crew loadmaster)

compartment capacity or maximum allowable weight. C-130J-30: 8 pallets or 97 litters or 24 CDS bundles or 128 combat troops or 92 paratroopers, or a combination of any of these up to the cargo compartment capacity or maximum allowable weight. C-130E/H: Five (two pilots, navigator, flight engineer and

C-130J/J-30: Three (two pilots and loadmaster) Aeromedical Evac Role - A basic crew of five (two flight nurses and three medical technicians) is added for aeromedical evacuation missions. Medical crew may be decreased or increased as required by the needs of patients. Armament None Initial operating capability - C-130A, Dec 1956; C-130B, May 1959; C-130E, Aug 1962; C-130H, Jun 1974; C-130J, Feb 1999 Inventory Active force, 151; Air National Guard, 181; Air Force Reserve, 103 Contractor / Status / Improvements / Special Equipment: Contractor – Boeing Company Status Inventory Management/Engineering: AMC, Scott AFB, IL

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Nomenclature: C-17

Name: Globemaster III

Capability: The C-17 is capable of rapid strategic delivery of troops and all types of cargo to main operating bases or directly to forward bases in the deployment area. The aircraft can perform tactical airlift and airdrop missions and can also transport litters and ambulatory patients during aeromedical evacuations when required. The inherent flexibility and performance of the C-17 force improve the ability of the total airlift system to fulfill the worldwide air mobility requirements of the United States. Description: The aircraft is operated by a crew of three (pilot, copilot and loadmaster), reducing manpower requirements, risk exposure and long-term operating costs. Cargo is loaded onto the C-17 through a large aft door that accommodates military vehicles and palletized cargo. The C-17 can carry virtually all of the Army's air-transportable equipment. Maximum payload capacity of the C-17 is 170,900 pounds (77,519 kilograms), and its maximum gross takeoff weight is 585,000 pounds (265,352 kilograms). With a payload of 169,000 pounds (76,657 kilograms) and an initial cruise altitude of 28,000 feet (8,534 meters), the C-17 has an unrefueled range of approximately 2,400 nautical miles. Its cruise speed is approximately 450 knots (.76 Mach). The C-17 is capable of airdropping 102 paratroopers and equipment. The design of the aircraft allows it to operate through small, austere airfields. The C-17 can take off and land on runways as short as 3,500 feet (1,064 meters) and only 90 feet wide (27.4 meters). Even on such narrow runways, the C-17 can turn around using a three-point star turn and its backing capability. Characteristics: Primary Function Power plant Thrust Wingspan Length Height Cargo Compartment -

Cargo and troop transport Four Pratt & Whitney F117-PW-100 turbofan engines 40,440 pounds, each engine 169 feet 10 inches (to winglet tips) (51.75 meters) 174 feet (53 meters) 55 feet 1 inch (16.79 meters) Length - 88 feet (26.82 meters) Width - 18 feet (5.48 meters) Height - 12 feet 4 inches (3.76 meters) Max Takeoff Weight 585,000 pounds (265,352 kilograms) Load 102 troops/paratroops; 36 litter and 54 ambulatory patients and attendants; 170,900 pounds (77,519 kilograms) of cargo (18 pallet positions) Speed 450 knots at 28,000 feet (8,534 meters) (Mach .76) Range Global with in-flight refueling Ceiling 45,000 feet at cruising speed (13,716 meters) Crew Three (two pilots and one loadmaster) Armament None Initial operating capability - 1993 Inventory Active duty, 158; Air National Guard, 8; Air Force Reserve, 8 Contractor / Status / Improvements / Special Equipment: Contractor – Boeing Company Status Inventory

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Management/Engineering: AMC, Scott AFB, IL

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Nomenclature: CV-22

Name: Osprey

Capability: The Osprey is a tiltrotor aircraft that combines the vertical takeoff, hover, and vertical landing qualities of a helicopter with the long-range, fuel efficiency and speed characteristics of a turboprop aircraft. It is available in three configurations: the combat assault and assault support MV-22 for the US Marine Corps; the long-range special operations CV-22 for US Special Operations Command (US SOCOM), (Its mission is to conduct long-range infiltration, exfiltration and resupply missions for special operations forces.); and the US Navy HV-22, for combat search and rescue, special warfare and fleet logistic support. Description: This versatile, self-deployable aircraft offers increased speed and range over other rotary-wing aircraft, enabling Air Force Special Operations Command aircrews to execute long-range special operations missions. The CV-22 can perform missions that normally would require both fixed-wing and rotary-wing aircraft. The CV-22 takes off vertically and, once airborne, the nacelles (engine and prop-rotor group) on each wing can rotate into a forward position The CV-22 is equipped with integrated threat countermeasures, terrain-following radar, forwardlooking infrared sensor, and other advanced avionics systems that allow it to operate at low altitude in adverse weather conditions and medium- to high-threat environments. The first operational CV-22 was delivered to Air Force Special Operations Command's 1st Special Operations Wing at Hurlburt Field, Fla., January 2007. Initial operating capability was declared March 2009 and a total of 50 aircraft will be delivered by 2017. The MV-22 achieved initial operating capability with the US Marine Corps in Iraq in September 2007. Characteristics: Primary function -

Special operations forces long-range infiltration, exfiltration, and resupply Power Plant Two Rolls Royce-Allison AE1107C turboshaft engines Thrust More than 6,200 shaft horsepower per engine Wingspan 84 feet, 7 inches (25.8 meters) Length 57 feet, 4 inches (17.4 meters) Height 22 feet, 1 inch (6.73 meters) Rotor Diameter 38 feet (11.6 meters) Speed 277 miles per hour (241 knots) (cruising speed) Ceiling 25,000 feet (7,620 meters) Max Vertical Takeoff Weight - 52,870 pounds (23,982 kilograms) Max Rolling Takeoff Weight - 60,500 pounds (27,443 kilograms) Range 2,100 nautical miles with internal auxiliary fuel tanks Payload 24 troops (seated), 32 troops (floor loaded) or 10,000 pounds of cargo Crew Four (pilot, copilot and two enlisted flight engineers) Armament GAU-18A RMWS (Ramp Mounted Weapon System) Date Deployed 2006 (with projected initial operational capability in 2009) Inventory Active force, 11

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Contractor / Status / Improvements / Special Equipment: Contractor - Bell Helicopter Textron Inc., and Boeing Company, Defense and Space Group, Helicopter Division Status Production Management/Engineering:

CV-22 Osprey refueled by an MC-130P

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CV-22 prepares for take off

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Nomenclature: AH-64D

Name: Longbow Apache

Capability: Conducts close combat attack, deep precision strikes, and armed reconnaissance and security in day, night, and adverse weather conditions. Description: The AH-64 Apache is a twin-engine, four bladed, multi-mission attack helicopter designed as a highly stable aerial weapons-delivery platform. With a tandem-seated crew consisting of the pilot, located in the rear cockpit position and the co-pilot gunner (CPG), located in the front position. The helicopter is designed as a weapons delivery platform and is equipped with: a M230E1, 30mm automatic gun, aerial rockets system (2.75 inch folding fin), and point target weapons system (Hellfire missiles). It is highly mobile, lethal, and can destroy armor, personnel, and materiel targets in obscured battlefield conditions. The Longbow incorporates millimeter wave fire control radar (FCR), radar frequency interferometer (RFI), fire-and-forget radar-guided Hellfire missile, and other cockpit management and digitization enhancements. With the addition of a new and highly sophisticated fire control radar (FCR), more commonly called the Longbow Fire Control Radar and the Modernized Target Acquisition Designation Sight (M-TADS), the AH-64D has become the most advanced aerial fighting vehicle in the world. The FCR provides the Apache with the ability to detect, classify, and prioritize stationary and moving targets both on the ground and in the air. The M-TADS provides the capability to find, locate, and engage enemy targets at greater distance than the legacy systems. The Video from UAS for Interoperability Teaming - Level 2 (VUIT-2) system provides two new capabilities to the Longbow fleet. The crewmembers receive video directly from UAVs and Joint assets, such as Litening and Sniper Pods. The crew can also transmit their own sensor video or re-trans UAV video to ground troops with ROVER or OSRVT (One System Remote Video Terminal). Characteristics: Max Gross Weight - 20,260 lbs. (23,000 lbs. for non tactical ferry flights) Speed 167 mph Combat Endurance - 2-4 hours (3 hours with internal auxiliary fuel tank) Range 110 NM with 20 min station time (185 NM and 20 min station time with auxiliary fuel tank) Crew 2 (pilot and co-pilot gunner) Armament M230E1 automatic gun (30mm chain gun) 1× 30x113 mm; 1,200 rounds (300 when internal auxiliary fuel tank is installed) AGM-114 HELLFIRE missiles 2.75‖ rockets Contractor / Status / Improvements / Special Equipment: Contractor - Manufacturer Airframe - Boeing (Mesa, AZ); Fire Control Radar - Northrop Grumman (Linthicum, MD); Lockheed Martin (Owego, NY); MTADS/PNVS – Lockheed Martin (Orlando, FL); Boeing (Mesa, AZ); Rotor blades: Ducommun AeroStructures (Monrovia, CA) Status Inventory Management/Engineering: SFAE-AV-AAH, Redstone Arsenal, AL

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Apache Longbow w/ VUIT-2 in Iraq

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Nomenclature: AH-6A

Name: Little Bird

Capability: Supports combat and contingency operations with a light, rapidly deployable helicopter capable of armed reconnaissance, security, target acquisition and designation, command and control, light attack, and defensive air combat missions. Description: The AH-6 Little Bird Gun, a light attack helicopter, has been tested and proven in combat. Armed with guns, Hellfire missiles, and 2.75-inch FFAR, it provides armed helicopter support to both ground and air special operations. The unrefueled range of the AH-6 is 250 nautical miles. These versions were all powered by a single Allison T-63 252 SHP engine. The latest versions of these aircraft, the AH-6J attack helicopter and MH-6J insertion and extraction transport, based on the MD-530F, feature a more powerful engine and improved avionics, including an embedded GPS/inertial navigation system and forward-looking infrared (FLIR). The AH-6J can be armed with two seven-tube 2.75 inch rocket launchers and two 7.62mm M134 "miniguns.‖ The "Little Bird" can also be armed with .50 Cal. machine guns, MK19 40mm grenade machine gun, Hellfire missiles, and Air-to-Air Stinger (ATAS) missiles. Characteristics: Engine Length Height Weight EmptyMaxi Takeoff Weight Max Speed Max Range Ceiling Climb Rate Crew Armament -

1 x Allison T63-A-5A turboshaft engine driving five-blade main rotor and two-blade tail rotor at 253shp. 23 ft 8.14 ft 1,128 lbs 2,701 lbs 134 mph 379 miles 7,300 ft 1,840 ft/min 2 2 x M134 7.62mm miniguns 2 x M261 7-shot rocket pod (0.5in FFAR rockets) 2 x M260 19-shot rocket pod (0.5in FFAR rockets) 2 x AGM-114 Hellfire Anti-tank Missiles 2 x 12.7mm machine guns 2 x Air-to-Air Stinger (ATAS) Missiles

Contractor / Status / Improvements / Special Equipment: Contractor Status Management/Engineering:

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Nomenclature: AH-1W/Z

Name: Super Cobra

Capability: Conducts close combat attack, deep precision strikes, and armed reconnaissance and security in day, night, and adverse weather conditions. Description: The AH-1W Super Cobra is a day/night marginal weather Marine Corps attack helicopter that provides enroute escort for assault helicopters and their embarked forces. It is the only western attack helicopter with a proven air-to-air and anti-radar missile capability. The primary mission of the AH-1W aircraft is as an armed tactical helicopter capable of helo close air support, low altitude and high speed flight, target search and acquisition, reconnaissance by fire, multiple weapons fire support, troop helicopter support, and point target attack of threatening armor. The AH-1W provides fire support and fire support coordination to the landing force during amphibious assaults and subsequent operations ashore. AH-1W is a two-place, tandem-seat, twin-engine helicopter capable of land- or sea-based operations. The rear seat pilot is primarily responsible for maneuvering the aircraft. The front pilot controls the aircraft's weapons systems, but he also has a full set of aircraft controls. The AH-1W distinguished itself with its more powerful T700-GE-401 fully marinized engines and advanced electronic weapons capability. The AH-1W has significantly improved power available in high altitude, hot environment, and single engine performance. The Super Cobra is armed with a 20mm turret gun, TOW, Hellfire, Sidewinder, Sidearm missiles, and 5 inch or 2.75 inch rockets. The HELLFIRE Missile System increased ordnance delivery and firepower capabilities. The AH-1W Super Cobra provides full night-fighting capability with the Night Targeting System (NTS). The Night Targeting System (NTS) further enhanced the AH-1W's warfighting capability by adding FLIR sensor, CCD TV sensor, Laser Designator/Rangefinder, Automatic Target Tracking and FLIR, and CCD TV video recording. A four bladed version of the AH-1W, designated the AH-1Z, now fielded; the addition of the extra blades dramatically improves the performance envelope of the AH-1W. Characteristics: Primary Function Power plant Thrust Wingspan Length Height Weight Max Takeoff Weight Fuel Capacity Payload Speed Range Ceiling Crew Countermeasures Armament -

Attack Helicopter two T700-GE-401 turboshaft engines provide 3,380 shp

Empty: 12,300 lb 18,500 lb

Max 195 mph, Cruise 173 mph 14,750 ft 2 in tandem (pilot in rear, copilot/gunner in front) AN/ALE-39/47 Chaff system and SUU-25 Flare dispensers One M197 three barrel 20 mm gun (mounted under the nose with 750 round ammo container) Underwing attachments for up to eight TOW missiles, eight Hellfire missiles, or two AIM-9M Sidewinder

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Missiles; Can also be equipped with 2.75 or 5 Inch Rocket Launchers Initial operating capability - AH-1W - 1985 AH-1Z - 2007 Inventory Contractor / Status / Improvements / Special Equipment: Contractor - Bell Helicopter TEXTRON, Inc. (Prime), General Electric, Kollsman Inc. Status Inventory Management/Engineering: Naval Air Warfare Center Aircraft Div Patuxent River, MD

AH-1W

AH-1Z

AH-1Z

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Nomenclature: OH-58D

Name: Kiowa Warrior

Capability: Supports combat and contingency operations with a light, rapidly deployable helicopter capable of armed reconnaissance, security, target acquisition and designation, command and control, light attack, and defensive air combat missions. Description: The Kiowa Warrior is a rapidly deployable single-engine, two-man, lightly armed reconnaissance helicopter that features advanced avionics, navigation, communication, weapons, and cockpit integration systems. Its mast-mounted sight houses a thermal imaging system, low-light television, and a laser rangefinder/designator permitting target acquisition and engagement at stand-off ranges and in adverse weather. The navigation system can convey precise target locations to other aircraft or artillery via its advanced digital communications system. It can also transmit battlefield imagery to deliver near real-time situational awareness to command and control elements. The Kiowa Warrior provides anti-armor, anti-personnel, and anti-aircraft capabilities at stand-off ranges. Kiowa Warrior fielding is complete, but the Army is installing safety and performance modifications to keep the aircraft safe and mission-effective until it is retired. Characteristics: Max Gross Weight Empty Weight Height Width Length Rotor Diameter Max Cruise Speed Range Ceiling Crew Armament -

5,200 lbs (armed) 3,289 lbs 12 ft 10.6 in 6 ft 5 in 33 ft 4 in 35 ft 138 mph 299 miles (sea level, no weapons, 10% reserve) 19,000 ft 2 Air-to-air Stinger (ATAS) (2 round launcher); .50 caliber machine gun (500 rounds); HYDRA 70 (2.75 in) rockets (7-shot pod); AGM-114 HELLFIRE missiles (2-round launcher); (It can carry two missile systems or the .50 caliber MG by itself)

Contractor / Status / Improvements / Special Equipment: Contractor - Bell Helicopter, Textron (Fort Worth, TX); DRS Optronics Inc. (Palm Bay, FL); Rolls Royce Corp. (Indianapolis, IN); Honeywell, Inc. (Albuquerque, NM); Smiths (Grand Rapids, MI) Status Inventory Management/Engineering: SFAE-AV-ASH-KW, Redstone Arsenal, AL

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Nomenclature: HH-60G

Name: Pave Hawk

Capability: The primary mission of the Air Force HH-60G Pave Hawk helicopter is to conduct day or night combat search and rescue, or CSAR, operations into hostile environments to recover downed aircrew or other isolated personnel during war. Because of its versatility, the HH-60G is also tasked to perform military operations other than war. These tasks include civil search and rescue, emergency aeromedical evacuation, disaster relief, international aid, counterdrug activities and NASA space shuttle support. Description: The Pave Hawk is a highly modified version of the Army Black Hawk helicopter which features an upgraded communications and navigation suite that includes integrated inertial navigation/global positioning/Doppler navigation systems, satellite communications, secure voice, and Have Quick communications. All HH-60Gs have an automatic flight control system, night vision goggles with lighting and forward looking infrared system that greatly enhances night low-level operations. Additionally, Pave Hawks have color weather radar and an engine/rotor blade anti-ice system that gives the HH-60G an adverse weather capability. Pave Hawk mission equipment includes a retractable in-flight refueling probe, internal auxiliary fuel tanks, two crew-served 7.62mm or .50 caliber machineguns, and an 8,000-pound (3,600 kilograms) capacity cargo hook. To improve air transportability and shipboard operations, all HH-60Gs have folding rotor blades. Pave Hawk combat enhancements include a radar warning receiver, infrared jammer and a flare/chaff countermeasure dispensing system. HH-60G rescue equipment includes a hoist capable of lifting a 600-pound load (270 kilograms) from a hover height of 200 feet (60.7 meters), and a personnel locating system that is compatible with the PRC-112 survival radio and provides range and bearing information to a survivor's location. A limited number of Pave Hawks are equipped with an over-the-horizon tactical data receiver that is capable of receiving near real-time mission update information. The Pave Hawk is a twin-engine medium-lift helicopter operated by Air Combat Command, Pacific Air Forces, Air Education and Training Command, U.S. Air Forces in Europe, Air National Guard and Air Force Reserve Command. Characteristics: Primary Function Power plant Thrust Rotary Diameter Length Height Weight -

Fuel Capacity Payload Speed -

combat search and rescue and military operations other than war in day, night or marginal weather conditions. Two General Electric T700-GE-700 or T700-GE-701C engines 1,560-1,940 shaft horsepower, each engine 53 feet, 7 inches (14.1 meters) 64 feet, 8 inches (17.1 meters) 16 feet, 8 inches (4.4 meters) Empty 11,516 lbs Mission Gross Weight 17,432 lbs Max Takeoff Weight 22,000 lbs (9,900 kilograms) 4,500 lbs (2,041 kilograms) depends upon mission 184 mph (159 knots)

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Range 504 nautical miles Ceiling 14,000 feet (4,267 meters) Crew Two pilots, one flight engineer and one gunner Armament Two 7.62mm or .50 caliber machineguns Initial operating capability - 1982 Inventory Active force, 64; ANG, 18; Reserve, 23 Contractor / Status / Improvements / Special Equipment: Contractor - United Technologies/Sikorsky Aircraft Company Status Inventory Management/Engineering:

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Nomenclature: MH-60

Name: Pave Hawk

Capability: The primary mission of the MH-60 is to conduct overt or covert infiltration, exfiltration, and resupply of special operations forces across a wide range of environmental conditions. An armed version, the Direct Action Penetrator (DAP), has the primary mission of armed escort and fire support. Secondary missions of the MH-60 include external load, CSAR and MEDEVAC operations. The MH-60 is capable of operating from fixed base facilities, remote sites, or ocean going vessels. Description: The MH-60L Direct Action Penetrator (DAP) is an MH-60L modified to mount a variety of offensive weapons systems. Its mission is to conduct attack helicopter operations utilizing area fire or precision guided munitions and armed infiltration or exfiltration of small units. It is capable of conducting direct action (DA) missions as an attack helicopter or has the capability to reconfigure for troop assault operations. In the Direct Action role, the DAP would not normally be used as a primary transport for troops or supplies because of high gross weight limits. The DAP is capable of conducting all missions during day, night, or adverse weather conditions. Also known informally as the "AH-60L", this upgrade of MH-60L was initiated in 1990 with the addition of FLIR, radar and standard UH-60 external stores support systems. Two Black Hawk companies of 160th SOAR each have a MH-60K platoon and MH-16K-DAP/AH-60L platoon. The MH-60L Direct Action Penetrator (DAP) armaments include a mix of multiple 30-mm Chain Gun, racks of four AGM-114 Hellfire and 2.75 in rocket pods, 40 mm grenade launcher or trainable 7.62 mm Gatling guns. An integrated fire control systems and a head-up-display (HUD) allow the crew to aim the weapons. The MH-60K is the current top-of-the-line SOA medium helicopter. It was designed with much input from actual 160th pilots. The MH-60K features a fully integrated NVG compatible glass cockpit. It can carry twelve soldiers over 750 miles without refueling. A mission management system is also part of the aircraft's equipment. Electronic sensors and counter measures have also been added and improved to increase the aircraft's effectiveness and ability to survive the battlefield. Characteristics: Primary Function Power plant Thrust Rotary Diameter Length Height Weight -

Fuel Capacity Payload Speed Range Ceiling Crew Armament -

conduct overt or covert infiltration, exfiltration, and resupply of special operations forces Two General Electric T700-GE-701C engines 1,560-1,940 shaft horsepower, each engine 53 feet, 7 inches (14.1 meters) 64 feet, 8 inches (17.1 meters) 16 feet, 8 inches (4.4 meters) Empty 11,516 lbs Mission Gross Weight 17,432 lbs Max Takeoff Weight 22,000 lbs (9,900 kilograms) 4,500 lbs (2,041 kilograms) depends upon mission 184 mph (159 knots) (max speed 294 mph) 504 nautical miles 14,000 feet (4,267 meters) Four; Pilot, Co-pilot, two door gunners Various combinations:

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M230 30mm cannon (1100 rounds) @ 625 rounds per minute (RPM) M261 FFAR-2.75 ― 19 rocket pods AGM-114 Hellfire anti-tank missiles M134 7.62mm miniguns Contractor / Status / Improvements / Special Equipment: Contractor - United Technologies/Sikorsky Aircraft Company Status Inventory Management/Engineering:

MH-60K

MH-60L DAP

MH-60L DAP

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Nomenclature: UH-60A/L

Name: Black Hawk

Capability: Provide air assault, general support, aeromedical evacuation, command and control and special operations support to combat and stability and support operations within the US Army. Description: The UH 60 Black Hawk is a utility tactical transport helicopter that replaced the UH-1 "Huey". The versatile Black Hawk has enhanced the overall mobility of The Army, due to dramatic improvements in troop capacity and cargo lift capability, and will serve as The Army's utility helicopter in the Objective Force. On the asymmetric battlefield, it provides the commander the agility to get to the fight quicker and to mass effects throughout the battlespace across the full spectrum of conflict. An entire 11-person, fully-equipped infantry squad can be lifted in a single Black Hawk, transported faster than in predecessor systems, in most weather conditions. The Black Hawk can reposition a 105 mm Howitzer, its crew of six, and lift up to 30 rounds of ammunition in a single lift. The Black Hawk has performed admirably in a variety of missions, including air assault, air cavalry and aeromedical evacuations. In addition, modified Black Hawks operate as command and control, electronic warfare, and special operations platforms. The aircraft's critical components and systems are armored or redundant, and its airframe is designed to progressively crush on impact to protect the crew and passengers. UH-60A UH-60C UH-60L UH-60M

UH-60Q

Original U.S. Army version, carries a crew of four and up to 11 passengers. Equipped with a T-700-GE-700 engines. Modified version for C2 missions UH-60A with upgraded T-700-GE-701C or T-700-GE-701D/CC engines, improved durability gearbox, and additional vibration absorbers. UH-60L upgraded with improved design wide chord rotor blades, T-700-GE701D Engines, improved durability gearbox, integrated Vehicle Management Systems (IVHMS) computer, and modern "Glass Cockpit" flight instrument suite. Planned to replace all UH-60A and L aircraft with the U.S. Army. UH-60A modified for medical evacuation. Aircraft since re-designated HH-60A.

Characteristics: Primary Function -

Utility helicopter to transport personnel and material UH-60A UH-60L Max Gross Weight 20,250 lbs 22,000 lbs, 23,500 (external cargo) Speed 139 kt 150 kt Endurance 2.3 hrs 2.1 hrs Mac Range 320 nm 306 nm External Load 8,000 lbs 9,000 lbs Internal Load 2,640 lbs (or 11 combat-equipped troops) Length 64 ft 10 in Height 16 ft 10 in Rotor Diameter 53 ft 8 in Crew 4 (2 pilots; 2 crew chiefs) Armament two 7.62mm machine guns Initial operating capability - 1979

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Contractor / Status / Improvements / Special Equipment: Contractor - United Technologies (Stratford, CT); General Electric (Lynn, MA) Status Inventory Management/Engineering:

UH-60L

UH-60Q

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Nomenclature: CH-53D

Name: Sea Stallion

Capability: The CH-53D is a medium lift helicopter designed to transport personnel, supplies and equipment in support of amphibious and shore operations. The CH-53D Sea Stallion is designed for the transportation of equipment, supplies and personnel during the assault phase of an amphibious operation and subsequent operations ashore. Capable of both internal and external transport of supplies, the CH-53D is shipboard compatible and capable of operation in adverse weather conditions both day and night. The CH-53D is now filling a role in the Marine Corps' medium lift helicopter fleet. Description: The twin-engine helicopter is capable of lifting 7 tons (6.35 metric tons). Improvements to the aircraft include T64GE-416 engines, elastomeric rotor head, external range extension fuel tanks, crashworthy fuel cells, ARC-210 radios, and defensive electronic countermeasure equipment. The helicopter will carry 32 passengers in its normal configuration and 55 passengers with centerline seats installed. The CH-53D is a more capable version of the CH53A introduced into the Marine Corps in 1966. Used extensively both afloat and ashore, the Sea Stallion was the heavy lift helicopter for the Marine Corps until the introduction of the CH53E triple engine variant of the H-53 family into the fleet in 1981. The CH-53D has performed its multi-role mission lifting both equipment and personnel in training and combat, most recently in Operation Iraqi Freedom and are deploying to Operation Enduring Freedom in FY09. All Marine Corps CH-53D helicopters are currently assigned to Marine Corps Base Hawaii, Kaneohe Bay. The CH-53D Sea Stallion’s cargo/troop compartment measures 30 feet long by 7'/2 feet wide and 6'/2 feet high and has a rear door and loading ramp. To facilitate cargo handling, a remotely controlled winch is located at the forward end of the compartment. There is space for a jeep with trailer, a 105mm howitzer or a Hawk missile system. If passengers are carried, 32 combat-equipped troops or 24 litter patients can be accommodated. Twin-turbine engines turn a single, six-bladed main rotor which has an automatic blade-folding system. Engine air separators have been incorporated on many models to reduce power loss in a sand/dust environment. An automatic flight control system lessens pilot fatigue on long missions. Characteristics: Primary Function Power plant Thrust Performance -

Rotary Diameter Length Height Width -

Medium lift helicopter designed to transport personnel, supplies and equipment in support of amphibious and shore operations Two General Electric T64-GE-416 turboshaft engines 4,380 shaft horsepower per engine Designed to carry 8,000 lbs. of cargo at a cruise speed of 130 KIAS, with a maximum level flight speed of 130 KIAS, at sea level on a standard day 72 feet 3 inches (21.7 meters) Fuselage: 67 feet 2 inches (20.1 meters) Rotors turning: 88 feet 5 inches (26.6 meters) 24 feet 11 inches (7.2 meters) Rotor: 72 feet 3 inches (21.7 meters) Fuselage: 24 feet (7.3 meters)

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71 in

Cabin dimensions -

Weight Internal Load External Load Fuel Capacity Range Endurance Ceiling Speed Rotor Systems Armament -

Crew Date Deployed -

Length: 30 feet (9.2 meters) Width: 8 feet (2.4 meters) 63 Height: 6 feet 5 inches (1.9 meters) in Cargo door opening: Empty: 23,608 lbs. 90 in Max Gross: 42,000 lbs. 32 troops or 24 litter patients plus four attendants or 8,000 lbs. cargo Hook rated to 20,000 lbs. 13,178 lbs 578 nautical miles (665 statute miles, 1064km);886 nautical miles Ferry Range 4.5 hrs 12,450 ft 130 KIAS 6 blades on main rotor Two door mounted.50 BMG XM218 machine guns in the side doors. or three .50 Cal Browning Machine Gun (BMG) GAU-21 machine guns (1 ramp mounted) Two pilots and one to three aircrew (one crew chief/right gunner, 1 left gunner, 1 tail gunner (combat crew) 1966

Contractor / Status / Improvements / Special Equipment: Contractor - Sikorsky Aircraft Corporation (SAC) Division of United Technologies Corp. (UTC) Status Inventory 34 Active, 0 Reserve Management/Engineering: Naval Air Warfare Center Aircraft Div Patuxent River, MD

2 CH-53 Ds Landing

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Nomenclature: CH-53E

Name: Super Stallion

Capability: The CH-53E is a heavy lift helicopter designed to transport heavy equipment and supplies during the ship-to-shore movement of an amphibious assault and during subsequent operations ashore. As the Marine Corps' heavy lift helicopter designed for the transportation of material and supplies, the CH-53E is compatible with most amphibious class ships and is carried routinely aboard LHA (Landing, Helicopter, Assault: an amphibious assault ship), LPH (Landing Platform, Helicopter: an amphibious assault ship) and now LHD (Landing, Helicopter, Dock: an amphibious assault ship) type ships. Description: The CH-53E is capable of lifting 16 tons (14.5 metric tons) at sea level, transporting the load 50 nautical miles (57.5 miles) and returning. A typical load would be a 16,000 pound (7264 kilogram) M198 howitzer or a 26,000 pound (11,804 kilogram) Light Armored Vehicle. The aircraft also can retrieve downed aircraft including another CH-53E. The 53E is equipped with a refueling probe and can be refueled in flight giving the helicopter indefinite range. Derived from an engineering change proposal to the twin-engine CH-53D helicopter, the CH-53E has consistently proven its worth to the Fleet commanders with its versatility and range. With four and one half hours' endurance, the Super Stallion can move more equipment over rugged terrain in bad weather and at night. During Operation Eastern Exit two CH-53Es launched from amphibious ships and flew 463 nautical miles (532.45 miles) at night, refueling twice enroute, to rescue American and foreign allies from the American Embassy in the civil war-torn capital of Mogadishu, Somalia in January of 1990. Two CH-53Es rescued Air Force Capt. Scott O'Grady in Bosnia in June 1995. The platform has been critical to the success of OEF, OIF, and HOA. The CH-53E is a follow-on for its predecessor, the CH-53D. Improvements include the addition of a third engine to give the aircraft the ability to lift the majority of the Fleet Marine Force's equipment, a dual point cargo hook system, improved main rotor blades, and composite tail rotor blades. A dual digital automatic flight control system and engine anti-ice system give the aircraft an all-weather capability. The helicopter seats 32 passengers in its normal configuration and has provisions to carry 55 passengers with centerline seats installed. With the dual point hook systems, it can carry external loads at increased airspeeds due to the stability achieved with a dual point system. Characteristics: Primary Function -

Power plant Thrust Performance -

Rotary Diameter Rotor Systems -

Heavy lift helicopter designed to transport heavy equipment and supplies during the ship-to-shore movement of an amphibious assault and during subsequent operations ashore Three General Electric T64-GE-416 turboshaft engines 4,380 shaft horsepower per engine Designed to carry 32,000 lbs. of cargo externally at a cruise speed of 100 KIAS to a range of 50 nautical miles on a sea level tropical (32 degrees C) day. At destination, the helicopter can hover for 5 minutes, release its cargo, return 50 nautical miles without payload at speed for best range, and have 20 minutes of fuel in reserve. The helicopter is also designed to retrieve another CH-53E at a range of 20 nautical miles. 79 feet (24 meters) (CH-53D 72 feet) 7 blades on main rotor

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Length Height Width Cabin dimensions -

Weight -

Internal Load -

Fuel Capacity Range Endurance Ceiling Speed Armament -

Crew Date Deployed -

Fuselage: 73.4 feet (22.4 meters) Rotors turning; 99 feet.5 inches (30.2 meters) 28 feet 4 inches (7.3 meters) Rotor: 79 feet (24.1 meters) 71 in Fuselage: 24 feet (7.3 meters) Length: 30 feet (9.2 meters) Width: 8 feet (2.4 meters) 63 Height: 6 feet 5 inches (1.9 meters) in Cargo door opening: Empty: 37,500 lbs. 90 in Design Gross: 46,500 lbs. Max weight on wheels; 69,750 lbs. (31,666 kilograms) 32 troops or 24 litter patients plus four attendants or 15,000 lbs. cargo Max Gross weight w/External Load: 73,500 lbs. (33,369 kilograms) External load: Hook rated to 36,000 lbs. 13,178 lbs. without refueling; 580 nautical miles; with aerial refueling: indefinite 4 hrs (unrefueled) 18,500 ft 172.5 mph; 150 knots Two door mounted.50 BMG XM218 machine guns in the side doors. or three .50 Cal Browning Machine Gun (BMG) GAU-21 machine guns (1 ramp mounted) Two pilots and one to three aircrew (one crew chief/right gunner, 1 left gunner, 1 tail gunner (combat crew) 1981

Contractor / Status / Improvements / Special Equipment: Contractor - Sikorsky Aircraft Corporation (SAC) Division of United Technologies Corp. (UTC) Status Inventory, 146 Active, 6 Reserve Management/Engineering: Naval Air Warfare Center Aircraft Div Patuxent River, MD

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Nomenclature: UH-1N/Y

Name: Iroquois

Capability: Utility helicopter, primarily used for search and rescue, command and control and maritime special operations missions. Description: The HH-1N Iroquois helicopter is used by the Navy for shore-based search and rescue duties. The UH-1N Iroquois is used by the Marine Corps to provide all-weather, day-or-night airborne command, control and coordination for assault support operations. Additionally, it is used for assault transport and maritime special operations, forward air control, aeromedical evacuation of casualties from the field and tactical recovery of aircraft and personnel missions. The H-1 family of helicopters, popularly known as the Huey, is the most successful military helicopter ever produced — more than 16,000 have been produced since 1956. Originating from a 1955 U.S. Army contract for a medical evacuation helicopter, the first Navy/Marine Corps Iroquois variant, the UH-1E, was first procured in 1964. Deliveries of the current version, the HH/UH-1N, began in 1971. The last, and newest, UH-1N was delivered in January 1979. Both the Navy HH-1N fleet and the Marine Corps UH-1N fleet are scheduled to start being replaced by the UH-1Y in March 2008. The UH-1N could be in the fleet until 2014 when the last UH-1Y is delivered. Characteristics: Primary Function Utility and transport helicopter Power plant Two Pratt and Whitney T400-CP-400 turbo shaft engines, 1,250 hp Length 57 ft (fuselage 42 ft 4 in) Height 14 ft 5 in Weight Empty: 6,370 lb Max Takeoff Weight 10,500 lb Rotar Diameter 48 ft Speed Max cruise speed 110 knots Range 286 miles Ceiling 17,300 ft Crew Pilot, copilot, crew chief, gunner, plus 6 to 8 combat equipped troops Armament 7.62mm or GAU-21 .50 caliber machine gun; 2.75 rockets Initial operating capability - Jan 1971 Inventory UH-1Y Future 100 Contractor / Status / Improvements / Special Equipment: Contractor - Bell Helicopter Company Status Inventory Management/Engineering: Naval Air Warfare Center Aircraft Div Patuxent River, MD

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UH-1N

UH-1Y

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Nomenclature: H-46

Name: Sea Knight

Capability: Provide all-weather, day/night assault transport of combat troops, supplies, and equipment during amphibious and subsequent operations ashore. While the primary function of the H-46 is troop assault, movement of supplies and equipment is secondary. Additional tasks are: combat and assault support for evacuation and other maritime special operations; over-water search and rescue; support for mobile forward refueling and rearming points; as well as aeromedical casualty evacuation. Description: The H-46 aircraft are dual-piloted, twin-turbine General Electric T58 Series turbo-shaft engines, tandem-rotor helicopters that are relatively insensitive to wind direction. It has a large cabin and cargo-handling system, allowing for the option to carry up to 12 combat-loaded troops or the capability of being outfitted to carry medical evacuation litters in case of disasters. Additionally, its large center of gravity range optimizes it for vertical replenishment missions. It has the fuel endurance to stay airborne for approximately two hours, or up to three hours with the use of an additional internal tank. Characteristics: ENGINE (shp) (2) T58-GE-16A Series turbo-shaft engines Maximum Power 1,870 Continuous Power 1,770 FUEL CAPACITY (gal) 660 WEIGHTS (lbs.) Raw (Empty) Weight: 15,500 External Cargo Hook: 10,000 (capacity) Maximum Gross Weight: 24,300 DIMENSIONS Overall - External Cabin - Internal Height, rotors turning/folded 16 ft 11.6 in./16 ft 8 in. Height: Width, rotors turning/folded 51 ft/14 ft 9 in. Width: Length, rotors turning/folded 84 ft 4 in./45 ft 7.5 in Length: PERFORMANCE (reported at maximum gross weight) Maximum Speed (knots/mph) 136/156 Range at VBR (nmi): Cruise Speed (knots/mph) 120/138 Service Ceiling (ft): Rate of Climb (fpm) 1,433 ROTOR SYSTEM Blades per Hub 3 Blade Fold Automatic/Manual Speed (rpm) 264 at 100% Nr CREW Normal 4 (pilot, copilot, crew chief and 1 mechanic) Combat 6 (pilot, copilot, crew chief and 3 aerial gunners) PAYLOAD Combat 12 troops Medical Evacuation 15 litters and 2 attendants Cargo 5 pallets or 5 tri-walls

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6 ft 6 ft 24 ft 2 in. 180-360 14,000

Contractor/Status/Improvements/Special Equipment: Contractor: Boeing Vertol Company Status: Active Inventory Management/Engineering: PMA-226/NAVAIRSYSCOM

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Nomenclature: CH-47

Name: Chinook

Capability: Transport ground forces, supplies, ammunition and other battle-critical cargo in support of worldwide combat and contingency operations. Description: The CH-47 Chinook is a twin-turbine, tandem-rotor, heavy-lift transport helicopter with a useful load of up to 25,000 pounds. As the Army’s only heavy-lift helicopter, the mission of the CH-47 is to transport troops (including air assault), supplies, weapons and other cargo in combat, combat support, and combat service support operations. The Chinook’s cockpit accommodates tow pilots and an observer. It has a triple hook system, which provides stability to large external loads or the capacity for multiple eternal loads. Large external loads such as 155mm howitzers can be transported at speeds up to 260 km/h using the triple hook load configuration. Multiple external loads can be delivered to two or three separate destinations in one sortie. The cabin provides 42 cubic meters of cargo space and 21 square meters of cargo floor area and can accommodate two HMMWVs or a HMMWV together with 105mm howitzer and gun crew. The main cabin can hold up to 33 fully equipped troops. The Chinook is equipped with two T55-GA714 turbo-shaft engines, which are pod-mounted on either side of the rear pylon under the rotor blades. The self-sealing fuel tanks are mounted in external fairings on the sides of the fuselage. The fixed tanks hold 1,030 gallons of fuel. Three additional fuel tanks can be carried in the cargo area. The Chinook has undergone numerous upgrades since the first CH-47A model entered the Army service in 1962. Operational history: CH-47A Chinook entered service in Vietnam with the U.S. Army 1st Cavalry Division in late 1965. The CH-47B was the standard troop transport used by the U.S. Army 1st Cavalry Division in Vietnam. During the Gulf War of 1991, 163 CH-47Ds served in Operations Desert Shield and Desert Storm. The CH-47D saw wide use in Operation Enduring Freedom in Afghanistan and Operation Iraqi Freedom in Iraq. The Chinook was used in air assault missions, inserting troops into fire bases and later bringing food, water, and ammunition. It is typically escorted by attack helicopters such as the Apache for protection. The CH-47D was particularly useful in the mountainous terrain of Afghanistan where high altitudes and temperatures limited the use of the Black Hawk. Variants. The MH-47D variant was developed for Special Forces operations and has in-flight refueling capability, a fast-rope rappelling system and other upgrades. The current model used by US Army Special Operations is the MH-47E. A recapitalization program of the CH-47F will provide a more reliable, less costly to operate aircraft compatible with joint digital connectivity requirements in the future force with an extended life of approximately 20 years. Key modifications integrate a new-machined airframe, an upgraded T55-GA-714A engine to restore performance capability, Common Avionics Architecture System, Air Warrior, Common Missile Warning System enhanced air transportability, Digital Automatic Flight Control System (DAFCS), and an Extended Range Fuel System II for self-deployment missions. The CH47F is expected to remain the Army’s heavy-lift helicopter until at least the 2020-2025 time frame. The MH-47G Special Operations Aviation (SOA) version is currently being delivered to the U.S. Army. It is similar to the MH-47E, but features a more sophisticated avionics including a digital Common Avionics Architecture System (CAAS). On November 9, 2006, the HH-47, a new variant of the Chinook based on the MH-47G, was

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selected by the United States Air Force as the winner of the Combat Search and Rescue (CSAR-X) competition. Four development HH-47s will be built. Characteristics: Power PlantMax Gross Weight Empty Weight Height Width Length Max speedNormal cruise speedRate of climbRotor systemRange Ceiling Crew Troop capacityLitter capacitySling-load capacity Armament -

two Lycoming T55-GA-714 turbo-shaft engines 50,000 lbs 23,401 lbs 18ft 11 in 98 ft 10 in 170 knots/184 mph 130 knots/137 mph 1,522 ft/min three manual-folding blades per hub (tow hubs); 225 revolutions per minute; 60 ft rotor span 450 m/741 km 18,500 ft/ 5,640 m 3 (pilot, co-pilot, and flight engineer) 33 troops combat loaded 24 26,000 lb center hook; 17,000 lb forward/aft hook; 25,000 lb tandem M1334 7.62mm minigun, M240 7.62mm machine gun

Contractor / Status / Improvements / Special Equipment: Contractor - Boeing Status Inventory Management/Engineering:

SOF Team Jumps from MH-47

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INTENTIONALLY LEFT BLANK

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CHAPTER TWENTYFOUR 1 June 2009

UNMANNED AERIAL VEHICLES (UAV)

FOR OFFICIAL USE ONLY

INTENTIONALLY LEFT BLANK

Nomenclature: MQ-1B

Name: Predator

Capability: The MQ-1B Predator is a medium-altitude, long-endurance, remotely piloted aircraft. The MQ-1B's primary mission is armed reconnaissance against critical, time sensitive targets. The MQ-1B is a Joint Forces Air Component Commander-owned theater asset for reconnaissance, surveillance and target acquisition in support of the Joint Forces commander. Description: The MQ-1B Predator system consists of four aircraft (with sensors), a ground control station, a Predator Primary Satellite Link, and approximately 55 personnel for deployed 24-hour operations. The basic crew for the Predator is one pilot and one sensor operator. They fly the aircraft from the ground control station (GCS) via a line-of-sight data link or a satellite data link for beyond line-of-sight flight. The aircraft is equipped with a color nose camera (generally used by the pilot for flight control), a day variable-aperture TV camera and a variable-aperture infrared camera (for low light/night). The cameras produce full motion video. The MQ-1 Predator carries the Multi-spectral Targeting System with inherent AGM-114 Hellfire missile targeting capability and integrates electro-optical, infrared, laser designator and laser illuminator into a single sensor package. The aircraft can employ two laser-guided Hellfire missiles with the MTS ball. The system is composed of four major components which can be deployed for worldwide operations. The Predator aircraft can be disassembled and loaded into a shipping container sometimes referred to as the "coffin." The ground control system is transportable in a C-130 (or larger) transport aircraft. The Predator aircraft can operate on a 5,000 by 75 feet (1,524 meters by 23 meters), hard surface runway with clear line-of-sight. The ground data terminal antenna provides line-of-sight communications for takeoff and landing. The Predator Primary Satellite Link (PPSL) provides over-the-horizon communications for the aircraft. The primary employment mode for Predator is called Remote Split Operations. The aircraft is launched from the Forward Operating Location (FOL) using a smaller version of the GCS call the Launcher and Recovery GCS (LRGCS). Once airborne, the aircraft is handed off to a crew in a CONUS based GCS which conducts the mission via extended communication links. Following the mission, the aircraft is handed back to the LRGCS for recovery. The aircraft includes an ARC-210 radio, an APX-100 IFF/SIF with Mode 4 and a turbo-charged engine. The latest upgrade enhances maintenance and performance, and includes notched tails, split engine cowling, steel braided hoses and an improved engine block. The "M" is the Department of Defense designation for multi-role and "Q" means unmanned aircraft system. The "1" refers to the aircraft being the first of a series of purpose-built remotely piloted aircraft systems. Characteristics: Primary Function Power plant Thrust Wingspan Length Height Weight -

Armed reconnaissance, airborne surveillance and target acquisition Rotax 914 I four cylinder engine 115 horsepower 48.7 feet (14.8 meters) 27 feet (8.22 meters) 6.9 feet (2.1 meters) 1,130 pounds (512 kilograms) empty

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Maxi Takeoff Weight 2,250 pounds (1,020 kilograms) External Payload 300 pounds Fuel Capacity 660 pounds (100 gallons) Loiter Speed Cruise speed around 84 mph (70 knots), up to 135 mph Maximum Speed 120 KIAS Endurance 24+ Hours (Clean) Service Ceiling up to 25,000 feet (7,620 meters) Max Range, No Relay up to 400 nautical miles (454 miles) Max Range with Relay Crew Two (pilot and sensor operator) Armament two laser-guided AGM-114 Hellfire missiles Launcher Modified M299 Missile Launcher Rail Launch Wheeled Recovery Wheeled Initial operating capability - March 2005 Inventory In Production Contractor / Status / Improvements / Special Equipment: Contractor - General Atomics Aeronautical Systems Incorporated Status Production Management/Engineering: 703 AESG, WPAFB, OH

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Nomenclature: MQ-1C

Name: Sky Warrior

Capability: The Sky Warrior provides the U.S. Army with a long-endurance, persistent ISR and tactical strike capability featuring a heavy-fuel engine for increased supportability in the field Description: The Sky Warrior will be operating in a reconnaissance, surveillance and target acquisition role. It will be part of an integrated command, control, communications and intelligence system. The U.S. Army plans to field this advanced Unmanned Aerial System (UAS) to assume some of the roles currently performed by the Air Force's Predator in 2009. The major difference between Sky Warrior and preceding models of Predator is its use of a diesel engine to meet Army onefuel requirements. Taking off from an airfield, the Sky Warrior is operated via the Army’s One System GCS and lands via an automatic takeoff and landing system. The Sky Warrior’s payload includes EO/IR and SAR with moving target indicator (SAR/MTI) capabilities. Additionally, two 250-pound and two 500-pound hard points under the main wings provide an attack capability. Sky Warrior UAS will be fielded to each of the Army’s divisions. Characteristics: Primary Function Power plant 1 X Thielert Heavy-Fuel Engine (JP-8, diesel), 135 HP (100kW) Thrust 135 HP Wingspan 56 ft (17 m) Length 28 ft (8 m) Height 6.9 ft (2.1 m) Weight 1130 lbs. Maxi Takeoff Weight 3,200 lbs. (1,451 kg) External Payload Total Payload (Fuel + 1,075 lb (488 kg) Payloads) Fuel Capacity 600 lbs Loiter Speed Maximum Speed 155 mph (135 knots ) Endurance 26 hr w/250 lb. payload Service Ceiling 29,000 ft (8,840 m) Max Range, No Relay Max Range with Relay Crew Two (pilot and sensor operator) Armament 4 AGM-114 Hellfire Missiles Sensor EO/IR/laser rangefinder/laser designator Datalink SATCOM (BLOS-Ku-band; LOS-C-band (TDCL)) Guidance Tracking Launch Wheeled on Runway Recovery Wheeled on Runway Initial operating capability Inventory 0 delivered/132 Aircraft Planned (11 systems; 12 UAVs per system)

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Contractor / Status / Improvements / Special Equipment: Contractor - General Atomics Aeronautical Systems, Inc Status Management/Engineering:

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Nomenclature: MQ-9

Name: Reaper

Capability: The MQ-9 Reaper is a medium-to-high altitude, long endurance remotely piloted aircraft system. The MQ-9 can perform as either a persistent hunter-killer against emerging targets to achieve joint force commander objectives or as an intelligence, surveillance and reconnaissance asset, employing sensors to provide real-time data to commanders and intelligence specialists at all levels. Description: The typical system consists of 4 air vehicles, a ground control station (GCS), communication equipment/links, spares and support personnel. The crew for the MQ-9 is a pilot and a sensor operator, who operate the aircraft from a remotely located GCS using the same Remote Split Operations concept as the MQ-1 Predator. To meet combatant commanders' requirements, the MQ-9 delivers tailored capabilities using mission kits that may contain various weapons and sensor payload combinations. The MQ-9 baseline system has a robust sensor suite for targeting. Imagery is provided by an infrared sensor, a color/monochrome daylight TV and an image-intensified TV. The video from each of the imaging sensors can be viewed as separate video streams or fused with the IR sensor video. The laser rangefinder/designator provides the capability to precisely designate targets for laser-guided munitions. Synthetic aperture radar will enable Joint Direct Attack Munitions targeting. The aircraft is also equipped with a color nose camera, generally used by the pilot for flight control. Each MQ-9 aircraft can be disassembled into main components and loaded into a container for air deployment worldwide in Air Force airlift assets such as the C-130. The MQ-9 air vehicle operates from standard U.S. airfields. The MQ-9 Reaper aircraft is larger and more powerful than the MQ-1 Predator and is designed to go after time-sensitive targets with persistence and precision, and destroy or disable those targets. The "M" is the Department of Defense designation for multi-role and "Q" means unmanned aircraft system. The "9" refers to the series of purpose-built remotely piloted aircraft systems. Characteristics: Primary Function - Unmanned hunter/killer or ISR weapon system Power plant Honeywell TPE331-10GD turboprop engine Thrust 900 shaft horsepower maximum Wingspan 66 feet (20.1 meters) Length 36 feet (11 meters) Height 12.5 feet (3.8 meters) Weight 4,900 pounds (2,223 kilograms) empty Maxi Takeoff Weight 10,500 pounds (4,760 kilograms) External Payload 3,750 pounds (1,701 kilograms) Fuel Capacity 4,000 pounds (602 gallons) Speed cruise speed around 230 KTAS, (200 KIAS) Endurance 14 Hours (loaded) Service Ceiling up to 50,000 feet (15,240 meters) Crew Two (pilot and sensor operator) Armament Combination of AGM-114 Hellfire missiles, GBU-12 Paveway II and GBU-38 Joint Direct Attack Munitions

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Launcher/Rack -

BUR-15/A Bomb Rack Modified M299 Missile Launcher Rail Launch Wheeled Recovery Wheeled Initial operating capability - expected in fiscal 2009 Contractor / Status / Improvements / Special Equipment: Contractor - General Atomics Aeronautical Systems, Inc. Status Production Management/Engineering: 703 AESG, WPAFB, OH

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Nomenclature: RQ-4

Name: Global Hawk

Capability: The RQ-4 Global Hawk is a high-altitude, long-endurance unmanned aircraft system with an integrated sensor suite that provides intelligence, surveillance and reconnaissance, or ISR, capability worldwide. Global Hawk's mission is to provide a broad spectrum of ISR collection capability to support joint combatant forces in worldwide peacetime, contingency and wartime operations. The Global Hawk complements manned and space reconnaissance systems by providing near-real-time coverage using imagery intelligence or IMINT, sensors. Description: The Air Force RQ-4 Global Hawk is a high-altitude, long-endurance unmanned aircraft designed to provide wide area coverage of up to 40,000 nm per day. The Global Hawk system consists of the RQ-4 aircraft, mission control element, or MCE, launch and recovery element, or LRE, sensors, communication links, support element and trained personnel. The IMINT sensors include synthetic aperture radar, electro-optical and medium-wave infrared sensors. The system offers a wide variety of employment options. The long range and endurance of this system allow tremendous flexibility in meeting mission requirements. The LRE, located at the aircraft base, launches the aircraft until handoff to the MCE contains functions required to launch, recover and operate an aircraft while en route to or from the target area. The LRE contains one pilot station providing the capability to operate one aircraft with no sensor operations. The Global Hawk will eventually carry the airborne signals intelligence payload. One version of Global Hawk will carry the Radar Technology Insertion Program active electronically scanned array radar. Characteristics: Primary Function Power plant Thrust Wingspan Length Height Weight Max Takeoff Weight External Payload Fuel Capacity Loiter Speed Maximum Speed Endurance Service Ceiling Max Range, No Relay Crew Armament Datalink Guidance Tracking Launch Recovery -

High-altitude, long-endurance intelligence, surveillance and Reconnaissance (ISR) Rolls-Royce-North American AE3007H turbofan 7,600 lbs. Blk 10 116 feet (35.3 meters); Blk 20/30/40 130.9 feet (39.8 meters) Blk 10 44 feet (13.4 meters); Blk 20/30/40, 47.6 feet (14.5 meters) Blk 10 15.2 (4.6 meters); Blk 20/30/40, 15.3 feet (4.7 meters) Blk 10, 11,350 pounds (5,148 kilograms); Blk 20/30/40, 14,950 lbs. (6,781 kilograms) Blk 10, 26,750 lbs. (12,133 kg); Blk 20/30/40, 32,250 lbs. (14628 kg) Blk 10, 2,000 lbs. (907 kg); Blk 20/30/40, 3,000 lbs. (1,360 kg) Blk 10, 15,400 lbs. (6,985 kg); Blk 20/30/40, 17,300 lbs. (7847 kg) Blk 10, 340 knots (391 mph); Blk 20/30/40, 310 knots (357 mph) 36 hours 60,000 feet Blk 10, 9,500 nautical miles; Blk 20/30/40, 8,700 nautical miles Three (LRE pilot, MCE pilot and sensor operator) N/A Ku SATCOM, CDL, LOS UHF SATCOM/LOS, INMARSAT Wheeled Wheeled

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Initial operating capability - TBD Inventory Active force, Blk 10: 7; Blk 20: 6; Blk 30: 1; Blk 40: 0 Contractor / Status / Improvements / Special Equipment: Contractor - Northrop Grumman (Prime), Raytheon, LE Comm Status Deployed/Operational Management/Engineering:

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Nomenclature: RQ-5A/MQ-5B/C

Name: Hunter

Capability: The Hunter system is capable of carrying out the following missions: real-time imagery intelligence, artillery adjustment, battle damage assessment, reconnaissance and surveillance, target acquisition and battlefield observation. Description: The MQ-5B/C has a fixed-wing, twin tail-boom design with a fuel-carrying center wing. It is powered by two 'heavy fuel' diesel engines developed by Northrop Grumman, one to 'push' and one to 'pull' the air vehicle. These allow the air vehicle to operate at higher altitudes of 6,100m (25,000ft) and increase endurance from 30 hours. The avionics suite includes upgraded mission computers, a new LN-251 Global Positioning System / Inertial Navigation System (GPS/INS), an APX-118 IFF transponder and an auxiliary power distribution unit. The suite introduces a relay mode that allows one Hunter to control another at extended ranges or over terrain obstacles. The extended centre wing has two external hard points capable of carrying weapons such as the Northrop Grumman Viper Strike laser-guided munition. The external payload is 60kg (130lb) on each wing. The primary payload on the RQ-5 is the Multi-Mission Optronic Payload (MOSP), developed by IAI Tamam, which includes television and Forward Looking Infrared (FLIR) to provide day / night surveillance capability. US Army Hunters can be fitted with new sensors including a third-generation FLIR and a spotter for the day TV camera. Hunter is capable of carrying other advanced mission payloads and has been used as a payload demonstration platform. Payloads have included a laser designator and various communications systems. A communications relay payload extends VHF/UHF communications beyond line of sight. Electronic countermeasures payloads have included communications warning receiver, communications jammer and radar jammer supplied by Northrop Grumman. Ground Control Station (GCS): The GCS-3000 ground control station, manned by two operators, tracks, commands, controls and communicates with the air vehicle and its payload. One ground control station can control one air vehicle or two air vehicles in relay. An enhanced mission planner provides flexible automated tactical mission planning and access to Digital Terrain Elevation Data (DTED), CD ROM map data and data from the Defense Mapping Agency (DMA). The GCS has three control bays and an optional intelligence bay. The pilot control bay controls the flight of the air vehicle. An observer control bay controls the payload functions. The navigation control bay is equipped with a digital map display which traces the flight path and monitors the progress of the mission. The intelligence bay provides data processing and distribution capabilities. Characteristics: Primary Function Power plant Thrust Wingspan Length Height Weight External Payload (MaxPer wing) Total Payload (Fuel +

Unmanned reconnaissance and hunter/killer weapon system Mercedes HFE (X2) 57 hp (X2) 54.5 feet (16.6m) 24.4 feet (7.5m) 7.5 feet (2.28m) 130 pounds (60 kg) 670 pounds (309 kg)

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Payloads) Fuel Capacity 421 pounds (602 gallons) JP-8 Loiter Speed 111km/h to 148km/h Maximum Speed222km/h Enduranceover 30 hours Service Ceiling 25,000 feet (7,620 meters) Max Range, No Relay127km Max Range with Relay200km Crew Two (pilot and sensor operator) Armament GBU-44/B Viper Strike Datalink Guidance Tracking Launch Wheeled Recovery Wheeled Initial operating capability Inventory Active force Contractor / Status / Improvements / Special Equipment: Contractor - Northrop Grumman Status Production Management/Engineering:

Ground Control Station

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Nomenclature: RQ-7B

Name: Shadow

Capability: The Shadow system is capable of carrying out the following missions: real-time imagery intelligence, artillery adjustment, battle damage assessment, reconnaissance and surveillance, target acquisition and battlefield observation. Description: The RQ-7 Shadow unmanned aerial vehicle (UAV) is used by the United States Army and Marine Corps. Launched from a rail, it is recovered with the aid of arresting gear similar to jets on an aircraft carrier. Its gimbal-mounted, digitally-stabilized, liquid nitrogencooled electro-optical/infrared (EO/IR) camera relays video in real time via a C-band LOS data link to the ground control station (GCS). Characteristics: Primary Function Power plant Thrust Wingspan Length Height Weight Max Takeoff Weight External PayloadTotal Payload (Fuel + Payloads) Fuel Capacity Loiter Speed Maximum SpeedEnduranceService Ceiling Max Range, No Relay Max Range with Relay Crew Armament Datalink Guidance Tracking Launch Recovery Inventory -

Unmanned reconnaissance Wankel UAV Engines 741, 38 hp (28.5kW) each 38 hp 14 ft 12.2 ft (3.9m) 3.3 ft (1m) 186 lbs. (77 kg) 100 lb (45 kg) 380 lbs. 12 gal (44 L) of 87 octane gasoline or 100LL Avgas (with few Modifications) max: 150 kts dash Loiter: 60 kts 7.5 hours @ 50 kts 15,000 feet (Electronic Line of Sight (ELOS)) 125 km Two (pilot and sensor operator) N/A

Rail Wheels Active force

Contractor / Status / Improvements / Special Equipment: Contractor - AAI Corporation Status Production Management/Engineering: NAVAIR, PMA-263 , NASD Patuxent River , MD

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Nomenclature: RQ-8B

Name: Fire Scout

Capability: Description: The RQ-8B will provide unprecedented situational awareness and precision targeting support for the U.S. Navy, and the U.S. Army. MQ-8B features four-blade main rotor, in contrast to the larger-diameter three-blade rotor of the RQ-8A, to reduce noise and improve lift capacity and performance. The four-blade rotor had already been evaluated on Fire Scout prototypes. They boost gross takeoff weight by 500 pounds to 3,150 pounds (by 225 kg to 1,430 kg), with payloads of up to 700 pounds (320 kg) for short-range missions. The MQ-8B is fitted with stub wings as well. The wings will serve both an aerodynamic purpose as well as an armament carriage location, to include weapons such as Hellfire missiles, Viper Strike laser-guided glide weapons, and in particular pods carrying the "Advanced Precision Kill Weapon System (APKWS)", a laser-guided 70 millimeter (2.75 inch) folding-fin rocket, which the Army sees as ideal for the modern battlefield. The Army is also interested in using the Fire Scout to carry up to 90 kilograms (200 pounds) of emergency supplies to troops in the field. The MQ-8B is being modified to permit rapid swap out of payload configurations. The current sensor configuration of a day/night turret with a laser target designator will of course remain an option. Alternate sensor payloads in consideration include a Tactical Synthetic Aperture Radar TSAR with Moving Target Indicator (MTI) capability, a multispectral sensor, a SIGINT module, the Target Acquisition Minefield Detection System (TAMIDS), and the Tactical Command Data Link (TCDL). The Army wants the Fire Scout to operate as an element of an integrated ground sensor network as well. Characteristics: Primary Function Power plant Thrust Main rotor diameter Length Height Weight Maxi Takeoff Weight External Payload Total Payload (Fuel + Payloads) Fuel Capacity Loiter Speed Maximum Speed Endurance Service Ceiling Max Range, No Relay Max Range with Relay Crew Armament Sensor Datalink Guidance Tracking Launch -

Unmanned hunter/killer weapons system Rolls Royce Allison Model 250-C20W 320 shp continuous 27 ft 6 in (8.4 m) 22.87 ft (8.4 m) 9.42 ft (2.9 m) 3,150 lb (1,430 kg) 600 lb.

1292 lb. 125 + knots 8 + hrs 20,000 ft (6,100 m)

EO/IR/laser designator and rangefinder LOS C2, Ku-band/UHF

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Recovery Initial operating capability Inventory Contractor / Status / Improvements / Special Equipment: Contractor - Northrop Grumman Unmanned Systems Status Management/Engineering: Naval Air Warfare Center Aircraft Div Patuxent River, MD

Control Station with Tactical Control System Software

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Nomenclature: RQ-11B

Name: Raven

Capability: The RQ-11B Raven Small Unmanned Aircraft System is a small man-portable UAS that performs reconnaissance, surveillance, and target acquisition missions for Army, USMC and USSOCOM forces. Description: The Raven back-packable UAS features two air vehicles or AVs, a ground control unit, remote video terminal, transit cases and support equipment. Typically two specially trained users operate the Raven UAV. The craft is launched by hand and powered by an electric motor. The UAV can be controlled manually or can autonomously navigate a preplanned route. The Raven includes a color electro-optical camera and an infrared camera for night operations. The air vehicle is hand-launched, weighs less than 5 pounds, has a range of 10 kilometers and an endurance of up to 90 minutes. It can fly up to altitudes of 1,000 feet (305 m) above ground level (AGL), and 15,000 feet mean sea level (MSL), at a flying speed of 28-60 mph. The Raven can be either remotely controlled from the ground station or fly completely autonomous missions using GPS waypoint navigation. The UAV can be ordered to immediately return to its launch point simply by pressing a single command button. Characteristics: Primary Function Power plant Thrust Wingspan Length Height Weight Maxi Takeoff Weight External Payload -

Reconnaissance and Air Surveillance Aveox 27/26/7-AV electric motor (200 watt DC) 4 ft 3 in (1.4 m) 3 ft 7 in (1.1 m) 4.2 lb 4.2 lb (1.9 kg) EO, 2 cameras POV switchable in flight: standard resolution camera, fixed FOV, and high resolution camera. Optional IR microbometer

Total Payload (Fuel + Payloads) Fuel Capacity N/A battery powered Loiter Speed Maximum Speed 60 mph (32 to 45 knots) Endurance 90 min Service Ceiling 15,000 (MSL) ft Max Range, No Relay 6.2 miles Max Range with Relay Crew 1 Ground Controller Armament N/A Datalink Guidance Tracking Launch Hand Launched Recovery Deep Stall Initial operating capability - 2006 Inventory -

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Contractor / Status / Improvements / Special Equipment: Contractor - AV Inc. US Status Deployed Management/Engineering: NAVAIR, PMA-263, Patuxent River Naval Air Station

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Nomenclature: None

Name: Wasp

Capability: Air Force Special Operations Command (AFSOC) selected the Wasp III as its Battlefield Air Targeting Micro Air Vehicle (BATMAV). Description: Wasp Block III is Equipped with forward and side looking color video cameras, as well as a modular forward or side looking electro-optical infrared payload. AFSOC uses these systems in support of ground combat controller teams. The Wasp III payload integrates several fixed cameras performing different tasks. The forward camera maintains field orientation with a broad view of the scene, while the side view camera, utilizing higher power magnification is generally used for target investigation. To maintain continuous coverage of a specific target, the Wasp automatically circles around it, maintaining the designated target in the side camera's field of view. The system is packed in a small suitcase, rapidly assembled within few minutes and is launched by hand toss. WASP is nearly silent and, when flown at night, it's almost undetectable. The smaller Wasp III is deployed by the US Marine Corps at the platoon level. To maintain commonality among deployed systems, the Wasp III uses a ground control system common to the Raven B and Puma UASs. The Wasp III mission endurance is 45 minutes, at a range of 5 km. At its mission termination point the Wasp lands horizontally over flat surface. A water landing version based on the WASP III is currently deployed. Characteristics: Primary Function -

Reconnaissance and Air Surveillance Wasp Block II Wasp Block III 1 X 10 watt DC Electric 1 X 10 watt DC Electric

Power plant Thrust Wingspan 16.1 in (41 cm) Length 9.3 in Height Weight 290 g . Maxi Takeoff Weight 290 g . Fuel Capacity N/A battery powered Loiter Speed Maximum Speed 25-37 mph (40-60 km/h) Endurance 40-60 min Service Ceiling 10,000 (ASL) ft Max Range, No Relay 2.5 miles (4 km) Crew 1 ground controller Armament N/A Launch Sling shot / Hand launched Recovery Skid landing, no wheels Initial operating capability - 2008 Inventory -

28.5 in (72 cm) 9.3 in 450 g 450 g

25-40 mph (40-65 km/h) 45 min 3.1 miles (5 km)

Contractor / Status / Improvements / Special Equipment: Contractor – Aerovironment Inc , USA Status Deployed

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Management/Engineering: NAVAIR, PMA-263, Patuxent River Naval Air Station

Wasp Block II

Wasp Block II

Hand Controller

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Nomenclature: TBD

Name: ScanEagle

Capability: Performs Intelligence, Surveillance, and Reconnaissance (ISR), missions. Description: The ScanEagle Unmanned Aerial Vehicle (UAV) is a 40 lb (18 kg) UAV designed for continuous mission of 15+ hours, cruising at speeds of 50 kt at an altitude of 5,000m. The system was designed for autonomous field operation. ScanEagle carries a payload of 6 kg, operating at a ceiling of 5,000 meters. It can be launched and retrieved over any terrain, including naval operations. The Unmanned Aerial System (UAS) includes a UAV, a Sky Wedge hydraulic launcher, Sky Hook retrieving system, and mobile ground control element. The longendurance, fully autonomous ScanEagle is equipped with nose-mounted inertial-stabilized camera turret, designed to track an object of interest for extended periods of time. It carries inertially stabilized electro-optical (EO) and infrared (IR) cameras that allow the operator to track both stationary and moving targets. ScanEagle is launched autonomously from a pneumatic SuperWedge catapult launcher and flies either preprogrammed or operator-initiated missions. The Insitu-patented SkyHook™ system is used to retrieve the UAS, capturing it by way of a rope suspended from a 50-foot-high tower. The system makes ScanEagle runway-independent and minimizes its impact on shipboard operations, similar to a vertical-takeoff-and-landing vehicle. ScanEagle is currently deployed with the US Marine Corps and US Navy in Iraq and Afghanistan, where the system flew over 100,000 hours since inception of the system in July 2005. Characteristics: Primary Function -

Power plant Thrust Wingspan Length Height Diameter Weight Max Takeoff Weight External Payload Total Payload (Fuel + Payloads) Fuel Capacity Loiter Speed Maximum Speed Endurance Service Ceiling Max Range, No Relay Max Range with Relay Crew Armament -

Land / Sea based long-endurance Intel, Surveillance and Reconnaissance 3W-Modeellmotoren 3W-24 1kW unleaded auto gasoline singlecylinder, two-stroke, spark-ignited, loop-scavenged piston engine 1.5 hp 2.9 m / 10 ft 1.2 m / 4 ft 0.5 m 7 in. 42 lbs. 15.4 kg 4.3 kg

48 knots 70 knots 20 hours 5,000 m

2 N/A

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Datalink None Guidance Tracking Launch Pneumatic Recovery Skyhook System Initial operating capability Inventory Contractor / Status / Improvements / Special Equipment: Contractor - Boeing Advanced Unmanned Systems Group and The Insitu Group, Inc Status - Inventory Management/Engineering: NAVAIR, PMA-263, Patuxent River Naval Air Station

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Nomenclature: RQ-16A

Name: T-Hawk

Capability: The T-Hawk backpackable UAV is to be used at platoon level for short-range surveillance, reconnaissance, target acquisition and battle management. The initial military evaluation focused on the detection of IEDs (Improvised Explosive Devices). Description: Each T-Hawk is small enough to carry in a backpack and is equipped with video cameras to relay information back to foot soldiers using a portable handheld terminal. The circular vehicle, weighing 17 pounds and 14 inches in diameter, can easily fly down to inspect hazardous areas for threats without exposing warfighters to enemy fire. It also has the ability to take off and land vertically from complex desert and urban terrains without using runways or helipads. The system has been deployed in Iraq to keep American troops safer by identifying enemy threats from the sky. The deployment is the first time a ducted-fan unmanned aerial vehicle (UAV) has been used during combat missions. The system requires minimal operator training. The ground station can be used to program a flight path for the T-Hawk or to control the craft manually. The aircraft also can be optionally equipped with electro-optical cameras for daylight operations or infrared cameras for night missions. Precise controls allow the T-Hawk to operate at very high altitudes or just inches from the ground, providing unprecedented hover and stare capabilities for enemy detection or other missions in war zones." In 2007, the U.S. Navy acquired 20 Micro Air Vehicles, designated YRQ-16A, for evaluation in Iraq by the U.S. MultiService Explosive Ordnance Disposal Group. Characteristics: Primary Function Power plant Thrust Wingspan Length Height Diameter Weight Maxi Takeoff Weight External Payload Total Payload (Fuel + Payloads) Fuel Capacity Loiter Speed Maximum Speed Endurance Service Ceiling Max Range, No Relay Max Range with Relay Crew Armament Datalink Guidance Tracking Launch -

Reconnaissance and Air Surveillance 3W-56 56cc Bower Twin piston engine; 3 kW (4 hp)

14 in. 17 lb.

.

40 knots 40 min 7,000 ft

N/A

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Recovery Initial operating capability Inventory Contractor / Status / Improvements / Special Equipment: Contractor - Honeywell Status Development Management/Engineering: NAVAIR, PMA-263, Patuxent River Naval Air Station

YRQ-6A

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CHAPTER TWENTYFIVE 1 June 2009

TEST AND TRAINING INSTRUMENTATION

FOR OFFICIAL USE ONLY

INTENTIONALLY LEFT BLANK

Nomenclature: AN/ARQ-52B (V)17 - Pod AN/ARQ-52C (V)17 - Pod (New) AN/ARQ-52B (V)18 - Plate

Name: Advanced Range Data System (ARDS)

Capability: Provides precision GPS/IMU based Time Space Position Information (TSPI) for Test and Evaluation (T&E) test operations on land, sea, and air platforms. It is also used to provide TSPI data for Developmental Testing and Operational Testing (DT/OT). Description: The Advanced Range Data System (ARDS) is a TSPI instrumentation suite providing GPS/IMU based TSPI as well as participant MIL-STD-1553 buss data on selected air platforms for T&E testing. The ARDS suite includes both a pod configuration for external wing station mounting and a plate configuration for internal mounting on air, ship and ground platforms. The pod can be flown on the LAU-7 guided missile launcher via the AIM-9 umbilical; LAU-127 via the AIM120 1760 connector; other launch rails that support the AIM-9 missile and the AIM-120 AMRAAM. The datalink system transmits the real-time differentially corrected GPS TSPI data (Method I solution) and air platform MIL-STD-1553 buss data (when required) to a ground station for processing, display, and analysis. The TSPI data collected can be post processed for even greater accuracy (Method III solution). The datalink has the ability to relay through other participants up to five deep when no ground stations are within line of sight. ARDS is currently used by all three military services for individual and joint T&E test operations and, in some cases, training applications. The ARDS is also capable of using missile simulations to derive real-time kill probabilities and uplink kill status through the ARDS datalink to select military participant platforms. The ARDS suite of hardware was first fielded in 1990 and has evolved in capability and performance with a number of enhancements and Service Life Extension Programs (SLEP) and continues to be heavily utilized by the T&E ranges as a key TSPI data source. Characteristics: Datalink -

Control and data through a dual frequency 1350 – 1450 MHz band TDMA phase modulated transmitter at 80 – 110 watts peak power. Supports 25 participants at a 10Hz data rate.

TSPI -

Rockwell Collins P/Y code GNP-10 GPS receiver tightly coupled with a 1º per hour Litton LN-200 fiber optic gyro.

Data Products -

Processed TSPI data, raw GPS and IMU data, and platform generated MIL-STD-1553 buss data.

Data Storage -

On board data storage utilizing an Intelligent Flash Solid State Recorder.

Encryption -

NSA approved Range Encryption Module (REM).

Primary Power -

Requires both 115VAC/400Hz (or 60Hz), and 28VDC

Pod Length (in.) -

138.66

Pod Diameter (in.) - 5 Pod Weight (lbs.) - AN/ARQ-52B (V)17 (No Ballast): 135.18 AN/ARQ-52B (V)17 (With Ballast): 179.53 AN/ARQ-52C (V)17 (P-5 TCTS Forward Hgr, No Ballast): 138.65 AN/ARQ-52C (V)17 (P-5 TCTS Forward Hgr, With Ballast): 183.00

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Carriage Options: Joint Service - F-35 US Air Force - F-22A, F-15, F-16, A-10, B-1B, B-2A, C-17, C-130, other programs. US Navy UH-1N/Y, AH-1W/Z, F/A-18, EA-6B, AV-8B, SH-60, V-22, P-3C, shipboard applications, Multi-Mission Aircraft (MMA), E-2D, CH-53D/E, manned and unmanned ground and sea targets/platforms. US Army AH-64D, RAH-66, UH-60, manned and unmanned ground targets/platforms. Contractor / Status / Improvements / Special Equipment: Long Term Sustainment Contractor - TYBRIN/Tri-Service GPS Sustainment Management Office. Status - 1) Production complete. 2) System fully deployed in 1999. 3) System in sustainment phase. Management/Engineering: The long term sustainment of the ARDS hardware and software suite is managed and supported by the Tri-Service GPS Sustainment Management Office (GPS SMO) at the Naval Air Warfare Center Weapons Division (NAWCWD) at China Lake, California. ARDS sustainment is accomplished through the use of a Contractor Logistic Support (CLS) contract. TYBRIN Corporation is the current prime contractor for the ARDS CLS sustainment contract. The Tri-Service GPS SMO manages all aspects of long term sustainment including maintenance, repair, replacement of obsolete parts, short-term and permanent modifications, configuration control, documentation and drawings, and enhancements including technology insertion. The Tri-Service GPS SMO is currently executing the Air Force, Navy, and Army’s ARDS Service Life Extension Program (SLEP) which will ensure the ARDS can continue to support existing T&E requirements through 2015. Configurations:

AN/ARQ-52B (V)17 Pod

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AN/ARQ-52B (V)18 Plate

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AN/GRQ-29 (V) ARDS Master/Remote Ground Station

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Nomenclature: AN/ASQ-T50(V)1 AN/ASQ-T50(V)2

Name: P5 Combat Training System/Tactical Combat Training System

Capability: Provides realistic Air Combat Training to the warfighter. Description: The P5 Combat Training System/Tactical Combat Training System (P5CTS/TCTS) is a multiparticipant training system, supporting both small and large scale exercises, employing instrumentation pods on high activity participant aircraft, and having ground subsystem components. The system contains an air-to-air data link for sharing participant GPS based time-space-position information, and is capable of both rangeless and ground-based live monitor operations. P5CTS/TCTS can employ simulated weapons. The Instrumentation pods have a data recorder, facilitating post mission data merge and training event playback for individual or group training. Characteristics (Instrumentation Pod): Data Link L-Band and S-Band variants Primary Power 115 VAC, 400 Hz single phase Length (in.) 142 Diameter (in.) 5 Weight (lbs.) (V)1: 135 (V)2: 146 (V)2 with ballast: 189 Transportability Transportable in a shipping container by truck, rail, air, or sea Carriage Options: Aircraft: A-10 F-5 F-15 F-16 F/A-18 Several coalition aircraft

Launcher: Any AIM-9 compatible rail

Contractor / Status / Improvements / Special Equipment: Contractor - Cubic Defense Applications, San Diego, CA Status Production and Deployment Management/Engineering: Air Force (P5CTS) program led by 689 ARSS, Eglin AFB, FL. PM responsibilities shared with Navy (TCTS) through PMA-205, Patuxent River, MD

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Nomenclature: TBD

Name: Common Range Integrated Instrumentation System (CRIIS)

Capability: The Common Range Integrated Instrumentation System (CRIIS) provides world-class test instrumentation capabilities for land, sea, and air platforms. Description: CRIIS will be the next generation range data system that will provide enhanced Time, Space, Position Information (TSPI) accuracy and selected participant data bus information for test and training event participants. An advanced spectrally efficient datalink will transmit the data to a ground station for further processing and analysis. CRIIS will be developed with an overall goal of maximizing commonality among range instrumentation systems for Test and Evaluation (T&E) and possible training applications, if funded and directed. CRIIS will replace the Advanced Range Data System (ARDS) which is approaching the end of its design life and cannot be efficiently updated to overcome obsolescence or resolve deficiencies identified by range users. Characteristics: Datalink Enhanced data transfer flexibility, control, and transmission; spectrally efficient TSPI Increased accuracy and faster data update rates Modularity Component miniaturization for better internal mounting flexibility Security Enhanced system security with new encryption technology TENA Compliance with Test and Training Enabling Architecture (TENA) Carriage Options (Projected): Joint Service - F-35 US Air Force - F-22A, F-15, F-16, A-10, B-1B, B-2A, C-130 CAP/AMP, UAVs, Uninhabited Combat Air Vehicle (UCAV), Airborne Laser (ABL), X Programs, other programs US Navy UH-1N/Y, AH-1W/Z, F/A-18 E/F/G, SH-60, V-22, shipboard applications, MultiMission Aircraft (MMA), E-2D, CH-53 Replacement, VXX Presidential Helicopter, UAVs, Airborne Laser (ABL). US Army: AH-64D, RAH-66, Blackhawk, Tracked Vehicles, Dismounted Infantry, UAVs, Patriot, BD5J, Future Combat System (FCS), Unmanned Ground Vehicles, Drones, Payload Drops Contractor / Status / Improvements / Special Equipment: Contractors - Rockwell Collins & Boeing (Pending Downselect - Currently in Source Selection) Status Risk Reduction/Technology Maturation Management/Engineering: Air Force CRIIS program led by 672 Air Armament Systems Squadron under the 728 Air Armament System Group, 308 Air Armament Systems Wing, Eglin AFB, FL

25-6

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Configurations:

25-7

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INTENTIONALLY LEFT BLANK

25-8

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APPENDIX A 1 June 2009

AIRCRAFT AND WEAPONS MATRIX AIRCRAFT GUN MATRIX AIRCRAFT RACK MATRIX AIRCRAFT LAUNCHER MATRIX

FOR OFFICIAL USE ONLY

X X X X X X X X X X X X X X X

X X X X X X X X

X X X X X

X X X X X X X X

X X X X X X X X

P-3C

EA-6B

AV-8B

F/A-18E/F EA-18G

F/A-18A-D

F-35

X X X X X X X X

MK 58 MOD 1 MARINE LOCATION MARKER

MK 62 QUICK STRIKE MINE MK 63 QUICK STRIKE MINE MK 65 QUICK STRIKE MINE MK 76 PRACTICE BOMB MK 77 MOD 5, 6 FIRE BOMB MK 81 GP 250 lb. MK 82 GP 500 lb. MK 83 GP 1,000 lb. MK 84 GP 2,000 lb. MK106 5LB PRACTICE BOMB MJU-1, M129/E1 LEAFLET GP BLU-109/B, A/B, B/B, & C/B HARD TAR PEN BLU-110/B, A/B, B/B, & C/B GP BOMB BLU-111/B, A/B, B/B, & C/B GP BOMB BLU-113A/B DESERT STORM SPECIAL BLU-116A/B SPECIAL PURPOSE BOMB BLU-117/A/B GP BOMB BLU-117/B, B/B, C/B GP BOMB BLU-119/B CRASHPAD BLU-121A/B ENHANCED BLAST WPN BLU-122/B HARD TARGET PENETRATOR BLU-126/B LOW-COLLATERAL BOMB MK 66 2.75 INCH ROCKET MK 71 5.0 INCH ZUNI ROCKET CBU-78 GATOR MINE CBU-87 CEM CBU-89 GATOR MINE CBU-97 SFW MK 20, CBU-99/100/B, A/B, B/B CBU-103 to 105 WCMD CBU-107/B CBU-116/118 PDU-5/B & SUU-76C/B GBU-10 MK-84 PAVEWAY I GBU-10 MK-84 or BLU-117 PAVEWAY II GBU-10 BLU-109 PAVEWAY II GBU-12 MK-82 PAVEWAY I GBU-12 MK-82 PAVEWAY II GBU-12F/B MK82 OR BLU-111

F-22A

F-16A/B BLK 10/15 F-16C/D BLK 25/30 F-16 C/D BLK 40 F-16C/D BLK 50

X

F-15E

A-10

M117 GP MK 56 MOORED MINE

F-15A-D

AIRCRAFT AND WEAPONS MATRIX (1 June 2009)

X X X X X X X

X X X X X X X

X X

X X X X X X

X X X

X

X

X X X X X X X

X X X

X X X

X

X X X

X X X X X X X X X X

X X X X P X

X X X X

X X

X

X

X P

X

X

X

X

X

X

X X X

X X

X X X

X X X

X

X X X X

X X X X

X X

X X

X X

X X

X

X

X

P X X X X

X X X X X

X - Weapon is integrated on Aircraft P - Weapon is planned to be integrated on Aircraft in the Future

A-1

FOUO

X X

AH-6

AH-64

OH-58D

AH-1W/Z

X

MQ-9

X

MQ-1B

UH-1N/Y

H-60

MH-60

CH-53D/E

MC-130

HC-130

AC-130U

AC-130H

B-52H

B-2A

B-1B

AIRCRAFT AND WEAPONS MATRIX (Continued) (1 June 2009)

X

X

X

X

M117 GP MK 56 MOORED MINE MK 58 MOD 1 MARINE LOCATION MARKER

MK 62 QUICK STRIKE MINE MK 63 QUICK STRIKE MINE MK 65 QUICK STRIKE MINE MK 76 PRACTICE BOMB MK 77 MOD 5, 6 FIRE BOMB MK 81 GP 250 lb. MK 82 GP 500 lb. MK 83 GP 1,000 lb. MK 84 GP 2,000 lb. MK106 5LB PRACTICE BOMB MJU-1, M129/E1 LEAFLET GP BLU-109/B, A/B, B/B & C/B HARD TAR PEN BLU-110/B, A/B, B/B, & C/B GP BOMB BLU-111/B, A/B, B/B, & C/B GP BOMB BLU-113A/B DESERT STORM SPECIAL BLU-116A/B SPECIAL PURPOSE BOMB BLU-117A/B GP BOMB BLU-117/B, B/B, C/B GP BOMB BLU-119/B CRASHPAD BLU-121A/B ENHANCED BLAST WPN BLU-122/B HARD TARGET PENETRATOR BLU-126/B LOW-COLLATERAL BOMB MK 66 2.75 INCH ROCKET MK 71 5.0 INCH ZUNI ROCKET CBU-78 GATOR MINE CBU-87 CEM CBU-89 GATOR MINE CBU-97 SFW MK 20, CBU-99/100/B, A/B, B/B CBU-103 to 105 WCMD CBU-107/B CBU-116/118 PDU-5/B & SUU-76C/B GBU-10 MK-84 PAVEWAY I GBU-10 MK-84 or BLU-117 PAVEWAY II GBU-10 BLU-109 PAVEWAY II GBU-12 MK-82 PAVEWAY I GBU-12 MK-82 PAVEWAY II GBU-12F/B MK82 OR BLU-111

X X

X X X

X X

X

X X

X X

X

X

X

X X X X X

X X

X

X X

X X

X X X

X

X - Weapon is integrated on Aircraft P - Weapon is planned to be integrated on Aircraft the future

A-2

FOUO

X GBU-15 MK-84 X GBU-15 BLU-109 X EGBU-15 BLU-109, BLU-121 X X X GBU-16 MK 83 or BLU-110 X X X X X X X GBU-24/B MK-84 X X X X X X X GBU-24A/B BLU-109 X X GBU-24B/B BLU-109A/B X GBU-24E/B BLU-109A/B X X GBU-24G/B BLU-116A/B X X X GBU-27A/B X X X GBU-27 BLU-109 X GBU-28A/B, B/B BLU-113/B, BLU-113A/B X GBU-28C/B BLU-122/B X GBU-28E/B BLU-113/B or BLU-113A/B X X X X X P X X GBU-31 JDAM 2000 lb. X P X P X GBU-32 JDAM 1000 lb. X X X X X X X X GBU-38 JDAM 500 lb. X GBU-39A/B SDB I FLM 250 lb. P X P P P P P GBU-39/B SDB I 250 lb. GBU-43/B MOAB GBU-44/B VIPER STRIKE Pave Way IV DUAL MODE GPS/INS LGB X X X GBU-51/B BLU-126/B X P X GBU-52/B BLU-126/B P X X X X P X P X GBU-54/B LJDAM 500 lb. X P ADM-141A,B TALD X P ADM -141C ITALD P P X X X P P ADM-160B MALD P P P P P P P ADM-160C MALD-J X X X X X X AGM-65 A, B TV MAVERICK X X X X X X X AGM-65 D, G IR MAVERICK P X X X AGM-65 E LASER MAVERICK X X X X X X X AGM-65 H/K MAVERICK X X AGM-84D HARPOON X P AGM-84H/K SLAM-ER AGM-86B ALCM AGM-86C/D CALCM X X X X X P X AGM-88B HARM P X X X X X X AGM-88C HARM P P P P AGM-88E AARGM AGM-114 AGM-129A ACM X AGM-130A MK-84 X - Weapon is integrated on Aircraft P - Weapon is planned to be integrated on Aircraft in the Future

A-3

FOUO

P-3C

EA-6B

AV-8B

F/A-18E/F EA-18G

F/A-18A-D

F-35

F-22A

F-16C/D BLK 50

F-16 C/D BLK 40

F-16C/D BLK 25/30

F-16A/B BLK 10/15

F-15E

F-15A-D

A-10

AIRCRAFT AND WEAPONS MATRIX (Continued) (1 June 2009)

X X

X X X X X

P

P

P P

P

OH-58D

X X

AH-64

X

AH-6

X

X X X P X X

AH-1W/Z

MQ-9

MQ-1B

UH-1N/Y

H-60 MH-60

CH-53D/E

MC-130

HC-130

AC-130U

AC-130H

B-52H

B-2A

GBU-15 MK-84 GBU-15 BLU-109 EGBU-15 BLU-109, BLU-121 GBU-16 MK 83 or BLU-110 GBU-24/B MK-84 GBU-24A/B BLU-109 GBU-24B/B BLU-109A/B GBU-24E/B BLU-109A/B GBU-24G/B BLU-116A/B GBU-27A/B GBU-27 BLU-109 GBU-28A/B, B/B BLU-113/B, 113A/B GBU-28C/B BLU-122/B GBU-28E/B BLU-113/B or BL:U-133A/B GBU-31 JDAM 2000 lb. GBU-32 JDAM 1000 lb. GBU-38 JDAM 500 lb. GBU-39A/B SDB 1 FLM 250 lb. GBU-39/B SDB 250 lb. GBU-43/B MOAB GBU-44/B VIPER STRIKE Pave Way IV DUAL MODE GPS/INS LGB GBU-51/B BLU-126/B GBU-52/B BLU-126/B GBU-54 LJDAM 500 lb. ADM-141A,B TALD ADM -141C ITALD ADM-160B MALD ADM-160C MALD-J AGM-65A, B TV MAVERICK AGM-65D,G IR MAVERICK AGM-65E LASER MAVERICK AGM-65H/K MAVERICK AGM-84D HARPOON AGM-84H/K SLAM-ER AGM-86B ALCM AGM-86C/D CALCM AGM-88B HARM AGM-88C HARM AGM-88E AARGM AGM-114 AGM-129 ACM AGM-130A MK-84

B-1B

AIRCRAFT AND WEAPONS MATRIX (Continued) (1 June 2009)

X X

P

P P

X X

X X

X X X

X - Weapon is integrated on Aircraft P - Weapon is planned to be integrated on Aircraft in the Future

A-4

FOUO

X X X X X X

AV-8B

X

X

X

X

X

X

P

X

X X X X P X

P X X X P

P

X X

X X

X X

X

X

X

X X X X

X

X

X

X X X X P X

P X X X P X X

X X X X X X X

X X P X X X

X X P X X X

X

X X

X X P X X X P X X

P

X P

P

P

P P

X

X

X X X

X X

X X

X X

X - Weapon is integrated on Aircraft P - Weapon is planned to be integrated on Aircraft in the Future

A-5

FOUO

P-3C

EA-18G

P

EA-6B

F/A-18E/F

X X

F/A-18A-D

X P

F-22A

F-16A/B BLK 10/15 F-16C/D BLK 25/30 F-16 C/D BLK 40 F-16C/D BLK 50

F-15E

F-15A-D

X X P

F-35

AGM-130C BLU-109 AGM-154 JSOW AGM-158A JASSM AGM-158B JASSM ER AIM-7M/P SPARROW AIM-9B, E, J SIDEWINDER AIM-9M SIDEWINDER AIM-9N/P SIDEWINDER AIM-9X NEXT GEN SIDEWINDER AIM-120A AMRAAM AIM-120B AMRAAM AIM-120C BLK C-3 - C-7 AMRAAM AIM-120D AMRAAM BDU-33D/B 25 lb. PRAC BOMB BDU-38 PRACTICE BOMB BDU-45 PRACTICE BOMB BDU-48 10 lb. PRACTICE BOMB BDU-50 500 lb. PRACTICE BOMB BDU-56 2000 lb. PRACTICE BOMB BDU-59B/B LGTR B61 B83

A-10

AIRCRAFT AND WEAPONS MATRIX (Continued) (1 June 2009)

X

AGM-130C BLU-109 AGM-154 JSOW AGM-158A JASSM AGM-258B JASSM ER AIM-7F/M SPARROW AIM-9B, E, J SIDEWINDER AIM-9M SIDEWINDER AIM-9N/P SIDEWINDER AIM-9X NEXT GEN SIDEWINDER AIM-120A AMRAAM AIM-120B AMRAAM AIM-120C BLK C-3 – C-7 AMRAAM AIM-120D AMRAAM BDU-33D/B 25 lb. PRAC BOMB BDU-38 PRACTICE BOMB BDU-45 PRACTICE BOMB BDU-48 10 lb. PRACTICE BOMB BDU-50 500 lb. PRACTICE BOMB BDU-56 2000 lb. PRACTICE BOMB BDU-59B/B LGTR B61 B83

X X

X X

X P

X

X

X X

X

X

X X

X X

X X

X X

X - Weapon is integrated on Aircraft P - Weapon is planned to be integrated on Aircraft in the Future

A-6

FOUO

OH-58D

AH-64

AH-6

AH-1W/Z

MQ-9

MQ-1B

UH-1N/Y

H-60

CH-53D/E

MC-130

HC-130

AC-130U

AC-130H

B-52H

B-2A

B-1B

AIRCRAFT AND WEAPONS MATRIX (Continued) (1 June 2009)

F-16 F-22A F-35 B-1B B-2A B-52H AC-130H AC-130U CH-53D/E H-46 CH-47 AH-64 HH-60 MH-60 UH-1N/Y AH-6 F/A-18A-D F/A-18E-F EA-18G AV-8B EA-6B P-3C AH-1W/Z MQ-9 CV-22

A-10 F-15A-D F-15 E

AIRCRAFT GUNS/RACKS MATRIX (1 June 2009) GUNS GAU-2B/A (“Minigun Gun 7.62mm)

X

X X X X

GAU-8/A (“Avenger” Cannon 30mm) X X

GAU-12/U (Cannon 25mm)

X X X X

GAU-18/A (Machine Gun .50 Cal)

X X

X X

GAU-19A Gatling Gun (50. Caliber) X X

GAU-21 (Machine Gun .50 Cal)

X

X

X

GAU-22/A (Cannon 25mm)

X X

M-137A1 (Cannon 105mm)

X

M197 (20mm) Gatling Gun X

M230 (30mm) Chain Gun M2A1 (“Bofors” Cannon 40mm)

X X X X X

M240D (Machine Gun 7.62mm) M61A1 (“Vulcan” Cannon 20mm)

X

X X X

X X X

M61A2 (Lightweight Cannon 20mm) Mk-44 (“Bushmaster” Cannon 30mm)

X X

X

M218 (Machine Gun .50 Cal)

X

RACKS X

14-INCH BOMB RACK

X

A-6 BOMB RELEASE AERO 7A-5 BOMB RACK EJECTOR

X

AERO 7B-4 BOMB RACK EJECTOR

X X

B-11 BOMB SHACKLE

X

BRU-15/A BOMB RACK X

BRU-32A/A EJECT UNIT RACK ASS

X

BRU-32B/A EJECT UNIT RACK ASS

X X

BRU-33A/A RACK ASSEMBLY

X

BRU-36A/A, B/A BOMB EJECT RK X X

BRU-41/A BOMB EJECTOR RACK BRU-42/A IMPROVED MULTIPLE EJECTOR RACK

X X X

BRU-44B/A BOMB RACK BRU-46/A BOMB RACK

X

X

BRU-47/A BOMB RACK

X

X X

BRU-52 BOMB RACK

X X

BRU-55/A BOMB EJECT RACK BRU-56/A (30 INCH EJECT RACK)

X

X - Weapon is integrated on Aircraft P - Weapon is planned to be integrated on Aircraft in the Future

A-7

FOUO

X

X

B-52H AC-130H AC-130U CH-53D/E AH-64 HH-60 MH-60 UH-1N/Y ARH/AH-6 F/A-18A-D F/A-18E-F EA-18G AV-8B CV-22 AH-1W/Z

F-16 F-22A F-35 B-1B B-2A

F-15A-D F-15E

A-10

AIRCRAFT GUNS/RACKS MATRIX (Continued) (1 June 2009) RACKS (Continued)

X

BRU-57/A SMART RACK

X

BRU-59/A BOMB EJECTOR RACK X

BRU-61/A COMMON CARRIAGE ASSEMBLY

P

BRU-67/A BOMB RACK

P

BRU-68/A BOMB RACK

P

P

X

CLUSTER BOMB RACK (CBR) MA-4 FAMILY OF 14” BOMB RACKS

X X X

MAU-12 BOMB RACK MAU-40/A BOMB RACK

X

MAU-50/A BOMB RACK

X

X

X X X

SMART BOMB RACK ASSEMBLY (SBRA) X X X

SUU-20 BOMB DISPENSER TER 9/A TRIPLE EJECTOR RACK TER 9/A MOD TRIPLE EJECTOR RACK

X X X

X

X X

X - Weapon is integrated on Aircraft P - Weapon is planned to be integrated on Aircraft in the Future

A-8

FOUO

X

CH-53D/E AH-64 H-60 MH-60 AH-1W.Z UH-1N/Y AH-6 F/A-18A-D F/A-18E-F EA-18G AV-8B P-3C EA-6B MQ-1B MQ-9

AC-130U

B-52H

AC-130H

B-2A

B-1B

F-35

F-16

F-22A

F-15

A-10

AIRCRAFT LAUNCHERS MATRIX (1 June 2009) LAUNCHERS

X

16S210 (AIM-9) 1760 CONV BOMB MOD (SECBM)

X

CONV BOMB MODULE (CBM) DUAL RAIL ADAPTER (DRA)

X X

LAU-7/A-6, B/A, B/A-1, D/A, E/A

X

LAU-7/A-7 X

LAU-61C/A X

X

X

X

X X

X

X X

X X

X

X X

X

X

LAU-10C/B, D/B X

LAU-68D/A (2.75 FFAR) LAU-88 (AGM-65)

X X

LAU-105/A (AIM-9)

X

LAU-106A/A (AIM-7 & AIM-120)

X

X

LAU-7C/A

LAU-68AA/, B/A, LAU-131/A (2.75 FFAR)

X

X

LAU-115C/A

X

LAU-115D/A

X

LAU-116/A, LAU-116A/A

X

LAU-116B/A

X

LAU-117A(V)2/A (AGM-65)

X X

X X X X

LAU-117A(V)3/A (AGM-65)

X X X

X X

LAU-118A(V)1/A (AGM-88)

X

X X

X

LAU-118A(V)4/A (AGM-88) LAU-127A/A, B/A, D/A, and E/A GUIDED MISSILE LAU

X

X X

X

X

X X X

LAU-127C/A, F/A GML LAU-128A/A, D/A, and B/A LAU-129A/A (AIM-9 & AMRAAM)

X X

X X

LAU-139 GML LAU-141/A CRL

X

LAU-142/A AVEL

X X

LAU-144/A 180-INCH ROT LAU LAU-147/A

P

LAU-148/A

P X

ROTARY LAUNCHER (AGMBRL) ROTARY LAUNCHER ASSEMBLY

X X

M299 MISSILE LAUNCHER

X X X X X X

MOD M299 MISSILE LAUNC RAIL

X - Weapon is integrated on Aircraft P - Weapon is planned to be integrated on Aircraft in the Future

A-9

FOUO

MISSILE DESIGNATIONS Rockets and guided missiles use the following designation symbols:

YAI M - 7 F Status Pref ix (Prototy pe) Launch Env ironment (Air Launched) Mission Sy mbol (Intercept) Vehicle Ty pe Sy mbol (Guided Missile) Design Number (7th Missile) Series Sy mbol (6th Version of AIM-7)

Status J Special Test, Temporary N Special Test, Permanent X Experimental Y Prototype Z Planning

Launch Environment A Air B C F G H L M P R S

Multiple Coffin Individual Runway Silo Stored Silo Launched Mobile Soft Pad Ship Underwater

Mission D Decoy E Special Electronics Installation G Surface Attack I Intercept, Aerial Q Drone T Training U Underwater Attack W Weather

A-10

Vehicle Type M Guided Missile/ Drone N Probe R Rocket

FOUO

MUNITIONS DESIGNATIONS Munitions use of the following designation symbols:

CB U - 87 A / B Item Identif ication (Cluster Bomb) "U" f or Unit Serial Number (87th Cluster Bomb) Model (1st v ersion of CBU-87) Installation (Aircraf t installed, expended)

Identification Designator AD AG BB BD BL BR BS CB CC CD CN DS

Certain adapting items Air to ground Explosive items Simulated bombs Bombs and mines Bomb racks and shackles Stabilizing & retarding device Cluster bomb Actuator cartridges Clustered munitions, not end item Miscellaneous containers Target directing device

LK LM LU M MA MD MH MJ MK ML MT PA

Ammunition links Ground-based launchers Illuminating units Army designation for munitions Miscellaneous armament items Miscellaneous simulated munitions Munitions handling equipment Munitions countermeasures Navy designation for bombs Miscellaneous munitions Mounts External munitions dispensing device Leaflet dispenser Ammunition Internal dispenser Dummy rockets Rockets Gun/bomb/rocket sights Stores suspension and release (dispenser containers) Miscellaneous tanks Test items Warheads Training warheads

FM FS FZ GA GB GF GP

Fuzes Fuze safety-arming device Fuze-related item Aircraft gun Guided bombs Gun related items Podded guns

PD PG PW RD RL SA SU

GU KA KM LA

Miscellaneous guns Munitions clustering hardware Kits Aircraft installed launchers

TM TT WD WT

A B E

Aircraft Installed, Fixed Aircraft installed, Expendable Ground Item, Moveable, not a Vehicle (Box for Munitions)

Installation Designator

A-11

FOUO

APPENDIX B ACRONYM LIST 1 June 2009 AAC AAED AAFL AARGM ABF ABL A/C ACAT ACC ACCM ACE ACM ACMI ACPTS ACS ACSS ACTD ACU AD ADAM ADG ADTS ADS AEA AESA AF AFG AFMC AFMSS AFRC AFRL AFS AFSOC AG AGL AGM AGMBRL AH AIM AIR AJ AJGPS/INS

Air Armament Center Advanced Airborne Expendable Decoy Advanced Airship Flying Laboratory Advanced Anti-Radiation Guided Missile Annular Blast Fragmentation Airborne Laser Aircraft Acquisition Category Air Combat Command Aircraft Countermeasures Adaptive Carriage Environment Advanced Cruise Missile Air Combat Maneuvering Instrumentation Armament Circuit Pre-load Test Set Armament Control System Aircraft Support Squadron Advanced Concept Technology Demonstration Avionics Control Unit Area Dominator Adapter Items Area Denial Artillery Munition Adapter Group Air Data Test Set Active Denial System Airborne Electronic Attack Advanced Electronically Scanned Array Air Force Air Foil Group Air Force Material Command Air Force Mission Support System Air Force Reserve Command Air Force Research Laboratory Avionics Flight Software Air Force Special Operations Command Air to Ground Above Ground Level Air to Ground Laser Air-to-Ground Missile Aircraft Guided Missile and Bomb Rotary Launcher Attack Helicopter Air Intercept Missiles Air Inflatable Retarded Anti-Jamming Anti-Jam Global Position System aided Initial Navigation System

B-1

FOUO

ALC ALCM ALE ALIC ALM ALS AMCOM AMI AMO AMRAAM AMST AMSTE ANG AP AP/AM or APAM APC APDS APDS-T APERS-T API APICM APIT APKWS APT AR ARDEC ARDS ARH ARL ARS ARSG ARSS ARSW ARVA AS ASC ASW ASUW ATA ATADS ATACMS ATAS ATD ATK ATL ATP ATR

Air Logistics Center Air Launched Cruise Missile Ammunition Loading Equipment Air Launcher Interface Computer Accurate Low Collateral Munition Ammunition Loading System Army Material Command Avionics Mid-Life Improvement Air and Marine Operations Advanced Medium Range Air-to-Air Missile Agile Munitions Support Tool Affordable Moving Surface Target Engagement Air National Guard Armor Piercing Anti-Personnel/Anti-Materiel Armored Personnel Carrier Armored Piercing Discarding Sabot Armor Piercing Discarding Sabot-Trainer Anti-Personnel Projectile with Tracer Armor Piercing Incendiary Anti-Personnel Improved Conventional Munition Armor Piercing Incendiary Tracer Advanced Precision Kill Weapon System Armor Piercing Tracer Automatic Rifle Armament Research, Development and Engineering Center Advanced Range Data System Anti-Radiation Homing Armed Reconnaissance Helicopter Army Research Laboratory Aluminum Rail Set Armament Systems Group Armament Systems Squadron Armament Systems Wing Armed Robotic Vehicle-Assault Armament Section Aeronautical Systems Center Anti-Submarine Warfare Anti-Surface Warfare Autonomous Target Acquisition Advanced Tactical DE System Army Tactical Missile System Air-to-Air Stinger Advanced Technology Demonstration Alliant Techsystems Attack Advanced Tactical Laser Authority to Proceed Autonomous Target Recognition

B-2

FOUO

AUP AUR AURCs AV AVEL AWE BATMAV BB BD BDU BCT BIT BL BLK BLOS BLU BM BOL BR BRA BRU BS C2 C3 CAAS CAE CALCM CAOC CARE CAS

CATM CAV CB CBM CBR CBSS CBU CC CD CCD CCLR CCG

Advanced Unitary Penetrator All Up Round All Up Round Containers Air Vehicle AMRAAM Vertical Ejection Launcher Aircraft Weapon Equipment Aircraft Weapon Electronics Battlefield Air Targeting Micro Air Vehicle Explosive Items Simulated Bombs Bomb Dummy Unit Brigade Combat Team Built-in-Test Bombs and Mines Block Beyond Line of Sight Bomb, Live Unit Bomb Logistics Unit Ballistic Missile Back of Launcher Bomb Racks and Shackles Bomb Rack Assembly Bomb Rack Unit Bomb Release Unit Stabilizing & Retarding Devices Command Control Command Control and Communications Common Avionics Architecture System Carrier Aircraft Equipment Conventional Air Launched Cruise Missile Combined Air Operations Center Carriage and Release Equipment Combat Ammunition System Control Actuation Section Control Actuator System Close Air Support Captive Air Training Missile Common Aero Vehicle Chemical Biological Cluster Bomb Conventional Bomb Module Cluster Bomb Rack Combat Support Squadron Cluster Bomb Unit Actuator Cartridges Clustered Munitions, not end item Charged Coupled Device Close Combat Lethal Recon Computer Control Group

B-3

FOUO

CEB CEM CEP CFMRE CGU CHAMP CHG C-IED CL CLAWS CLOAR CLS cm C-MANPADS CM-ATS CMBRE CMDDS CMDS CMOS CMRA CMUP CN CNO COIL COLT CONOPS CONUS COTS CPHD CPG CPGS CRADA CRD CRIIS CRL CTS CS CSAR CSM CSOP CSRL CSS CT CTOL CTU

Combined Effects Bomb Combined Effects Munitions Circular Error Probability Common Field-Level Memory Reprogramming Equipment Guidance Control Unit Counter-electronics HPM Advanced Munitions Program Charge Counter-Improvised Explosive Device Confidence Level Complementary Low Altitude Weapon System Common Low Observable Auto Router Contractor Logistic Support Centimeter Counter Man-Portable Air Defense Systems Cruise Missile Automatic Test Systems Common Munitions Bit Reprogramming Equipment Countermeasures Decoy Dispensing Set Countermeasures Dispenser Set Complementary metal-oxide-semiconductor Common Missile Radar Altimeter Conventional Mission Upgrade Program Common Name Miscellaneous Containers Chief of Naval Operations Chemical Oxygen Iodine Laser Common Organizational Level Tester Concept of Operations Continental United States Commercial Off The Shelf Copperhead Co-Pilot Gunner Conventional Prompt Global Strike Cooperative Research and Development Agreement Complete Round Code (Air Force Use Only) Navy uses NALC Common Range Integrated Instrumentation System Configurable Rail Launcher COLT Tester Set Control Test Set Control Section Tear Gas Combat Search and Rescue Conventional Strike Missile Combat Security Outposts Common Strategic Rotary Launcher Common Smart Submunition Cable Tester Combat Track Conventional Takeoff and Landing COLT Tester Unit

B-4

FOUO

CV DAFCS DAGR DAP DARPA DASALS DE DEAD DCL DCP DCPOFP DHS DIFR DIME DLI DLY DM DMA DMLGB DMPI DMU DODIC DOD DPF DPICM DRA DS DSU DT DTED DT/OT DTRA DTS DU EA EBC EBR ECBM ECCG ECCM ECM ECMO ECSS ECU EDL EED EEPROM

Carrier Variant Digital Automatic flight Control System Direct Attack Guided Rocket Defense Armored Penetrator Defense Advanced Research Projects Agency Distributed Aperture Semi-Active Laser Seeker Directed Energy Destroy Enemy Aid Defense Dual Compatible Launcher Display Control Processor Display Control Processor Operational Flight Program Department of Homeland Security Directional Frequency and Ranging Dense Inert Metal Explosive Designator/Laser Imager Delay Detection and Monitoring Defense Mapping Agency Dual Mode Laser Guided Bomb Desired Mean Point of Impact Digital Map Unit Department of Defense Identification Code Department of Defense Dispenser Proximity Fuze Dual Purpose Improved Conventional Munition Dual Rail Adapter Target Directing Device Proximity Sensor Designator for Fuzes (DS = Sensor + Unit) Developmental Test Digital Terrain Elevation Data Developmental Test/Operational Test Defense Threat Reduction Agency Depot Test Set Depleted Uranium Electronic Attack Electric Band Cutter Extended Battle Rifle Extended Bit-Rate Enhanced Conventional Bomb Module Enhanced Computer Control Group Electronic Counter-Countermeasures Electronic Countermeasures Electronic Counter-measures Officers Expeditionary Combat Support System Electrical Conversion Unit Electronic Control Unit Evolutionary Data Link Electro Explosive Devices Electrically Erasable Programmable Read Only Memory

B-5

FOUO

EFP EGBU (E)GBU EHF ELOS E&MD EMB EMD EMF EMI EO EOC EOD EO/IR EP ER-MLRS ERMP ERP ERO ES-1 ESAD ESAF ESD ESM ESTS ET EUC EUE EWSR F2T2 F2T2EA FAA FAASV FAC FAC(A) FAR FAU FCC FCR FCS FDE FFAR FIDL FIST FIU FLIR

Explosively Formed Projectile Enhanced Guided Bomb Designator Enhanced Guided Bomb Designator Extremely High Frequency Electronic Line of Sight Engineering & Manufacturing Development Enterprise Management Baseline Engineering Manufacturing Development Electromotive Force Electromagnetic Interference Electrical Optical Early Operational Capability Explosive Ordnance Disposal Explosive Ordnance Detachment Electro-Optical/Infrared Electronic Protection Extended-Range Multiple Launch Rocket System Extended Range Multi-Purpose (Army UAV) Enterprise Resource Planning Extended Range Ordnance Eglin Steel Electronic Safe-Arm Device Electronic Safe Arm Firing Electronic Safe and Arm Fuze Electrostatic Discharge Electronic Support Measures Electronic System Test Set Electronic Time Electronic Control Unit Extended User Evaluation Executive Weapon System Review Find, Fix, Target, Track Find, Fix, Target, Track, Engage and Asses Federal Aeronautics Association Field Artillery Ammunition Supply Vehicle Forward Air Controller Forward Air Controller Airborne False Alarm Rate Fin Actuator Unit Full Combat Capability Fire Control Radar Future Combat System Force Development Evaluation Folding Fin Aircraft Rocket Fully Integrated Data Link Fault Isolation System Tester Fire Support Team (Army Artillery) Fuze Interface Unit Forward Looking Infrared Radar

B-6

FOUO

FLM FLS FM FMCP FMOFP FMS FMU FO FOC FOTD FOUO FOV FPA fps FP FRPC FRTC FS FSE ft/s FW FZ FZU GA GaAs GAINS GAM GAP GAU GB GBU GCS GCU GE GEU GF GFU CG GGSMM GHz GIG GMLA gm GMG GLM GMLRS GMTI

Focused Lethality Munitions Forward Landing Strips Field Manual Fuzes Flight Management Control Processor Flight Management Operational Flight Program Foreign Military Sales Munition Fuze Unit (Fuze Series Designator follows) Forward Observer Full Operational Capability Fiber Optic Towed Decoy For Official Use Only Field of View Focal Plane Array Feet per second Forward Presence Full Range Practice Cartridge Full Range Training Cartridge Fuze Safety-Arming Device Fire Support Element Foot per second Fixed Wing Fuze-related Item Wind Driven Generator Aircraft Gun Gallium Arsenide Global Positioning System Aided Internal Navigation System GPS Aided Munition Global Asset Positioning Airborne Gun Unit Guided Bomb Guided Bomb Unit Ground Control Station Guidance Control Section Guidance Control Unit General Electric Guidance Electronic Unit Gun Related Items Gun Feeder Unit Gas Generation Gas Generation System Mass Model Gigahertz Global Information Grid Guided Missile Launch Assembly Gram Grenade Machine Gun Grenade Launcher Module Guided Multiple Launch Rocket System Ground Moving Target Indicator

B-7

FOUO

GMTS GOTS GP GPS gr GS GU GWOT H&I HARM HAS HAT HC HDBT HE HE/HF HE/PD HE/PD/DLY HEAT HEDP HEI HEI-P HEIT HEL ME/MO HEMTT HEP HERA HERO HF HIMARS HMMWV HOB HOBS HOJ HP HPM HQ HRR HTPB HTSF HTVSF HSAB HSP HSSW HUMRAAM HUD I2R

Guided Missile Test Set Government off the Shelf General Purpose Podded Guns Global Positioning System Grain Guidance Section Miscellaneous Guns Global War on Terror Harassment and Interdiction High Speed Anti-Radiation Missile Hardened Aircraft Shelter HPM Amplifier Transmitter White Smoke Hard and Deeply Buried Target High Explosive High Explosive/High Fragmentation High Explosive Point Detonating High Explosive Point Detonating Delay High Explosive Anti-tank High Explosive Dual Purpose High Explosive Incendiary High Explosive Incendiary-Plugged High Explosive Incendiary Tracer High-Energy Laser High-Explosive Multi-Option Heavy Expanded Mobility Tactical Truck High Explosive Plastic High Explosive Rocket Assisted Hazards and Electromagnetic Radiation to Ordnance High Fragmentation High Mobility Artillery Rocket System High Mobility Multipurpose Wheeled Vehicle Height of Burst High-Off-Boresight Home-On-Jam Horse Power High Power Microwave Headquarters High Resolution Radar Hydroxyl-terminated Polybutadiene Hard Target Smart Fuze Hart Target Void Sensing Fuze Heavy Stores Adapter Beam High Speed Penetrator High Speed Strike Weapon HMMWV armored with AMRAAMS Heads Up Display Imaging Infrared

B-8

FOUO

IADS IBS-R ICC ICD ICM ICP ICSMS IDM IDS IED IFC IFCS IFF IIR ILLUM ILMS IM IMER IMINT IMIRS IMP IMPLC IMU IMV In. INS INS-r IOC IR IRAD IRCM IRCCM IRU ISR ITALD ITER ITV IVHMS IWIU JAGM JAMS JASSM JASSM-ER JAST JCM JCTD JDAM JDAM AMSTE

Integrated Air Defense System Integrated Broadcast Service Receiver Initial Combat Capability Initial Capabilities Document Improved Conventional Munition Improved Crew Protection Integrated Conventional Stores Management System Impact Delay Mode Interface Control Document Improvised Explosive Device Integrated Functional Capability Improved Fire Control System Identification Friend or Foe Imaging Infrared Illumination Improved Launcher Mechanical System Insensitive Munitions Improved Multiple Ejector Rack Imagery Intelligence Improved Modular Infrared Sensor Impact Integrated Multi-Platform Launch Controller Inertial Measurement Unit Instrument Measurement Vehicle Inch Inertial Navigation System Inertial Navigation System Replacement Initial Operational Capability Infrared Internal Research and Development Infrared Countermeasures Infrared Counter-Countermeasures Inertial Reference Unit Intelligence, Surveillance, and Reconnaissance Improved Tactical Air-Launched Decoy Improved Triple Ejector Rack Instrument Test Vehicle Integrated Vehicle Management Systems Integrated Weapons Interface Unit Joint Air-to-Ground Missile Joint Attack Munition Systems Joint Air-to-Surface Stand-Off Missile JASSM- Extended Range Joint Advanced Strike Technology Joint Common Missile Joint Capability Technology Demonstration Joint Direct Attack Munition Joint Direct Attack Munition Affordable Moving Surface Target Engagement

B-9

FOUO

JHMCS JHSW JMEM JMPS JPF JSF JSOW JTD JTF JTV J-UCAS JVC KA KAC KE KEP kg KM KPPs kW LA LAD LADAR LALS LAM LANTIRN LAP LAPES LASIP LAT LAU lb lbs. LCF LCMCM LCTP LCU LCW LD LDGP LDTP LEA LGB LGBU

Joint Helmet Mounted Cuing System Joint High Speed Weapon Joint Munitions Effectiveness Manual Joint Mission Planning System Joint Programmable Fuze Joint Strike Fighter Joint Stand-Off Weapon Joint Technical Data Joint Task Force Jettison Test Vehicle Joint Unmanned Combat Aerial System Jet Vane Control Munitions Clustering Hardware Knight's Armament Company Kinetic Energy Kinetic Energy Projectile Kilogram Kits Key Performance Parameters Kilo Watt Aircraft Installed Launchers Low Angle Delivery Laser Detection and Ranging Linkless Ammunition Loading System Loitering Attack Missile Low-Altitude Navigation and Targeting Infrared for Night Load Assembly and Pack Low Altitude Parachute Extraction System Light Artillery System Improvement Program Lot Acceptability Test Launch Adapter Unit Pound Pounds Long Conductive Fiber Low Cost Mini-Cruise Missile Laptop Controlled Targeting Pod Life Cycle Upgrade Original Long Cord Low Drag Low Drag General Purpose Laptop Controlled Targeting Pod Launcher Electronics Assembly Laser Guided Bomb Laser Guided Bomb Unit

LGTR LJDAM LK LM

Laser Guided Training Round Laser Joint Direct Attack Munition Ammunition Links Ground-based Launchers

B-10

FOUO

LME LNO LOAL LOBL LoCo LOCO LOGIR LOS LP/C LPC/GMLA LRCP LRE LRGCS LRIP LRMSG LRU LSAC-H LU LWCMS LWL m M MA MAC MACE MACS MAD MAGR MAGTF MAJCOM MALD MALD-J MANPADS MAPAM MAU MBO MBTS MBX MCE MCS MD MDA MDT MDU

Locally Manufactured Equipment Liaison Officer Lock-on After Launch Lock-on Before Launch Low Collateral Damage Low Collateral Low-cost Guided Imaging Rocket Line of Sight Launch Pod/Containers Launch Pod Container/Guided Missile Launch Assembly Long Range Capability Plan Launch and Recovery Equipment Launch and Recovery Ground Control Station Low Rate Initial Production Long Range Missile Group Line Replacement Unit Line Replaceable Units Low Signature Armored Cab-HIMARS Illuminating Units Lightweight Company Mortar System Light Weight Launchers Meter Army Designation for Munitions Multi-role (Department of Defense designation for multi-role) Miscellaneous Armament Items Metal Augmented Charge Munition Assembly Conveyor Microwave Aerial Counter Electronics Monitor and Control Equipment Modular Artillery Charge System Magnetic Anomaly Detection Miniature Airborne GPS Receiver Marine Air-Ground Task Force Major Command Miniature Air Launched Decoy MALD Jammer Variant Man-Portable Air Defense System Mortar Anti-Personnel Anti-Materiel Miscellaneous Armament Unit Munitions Adapter Unit Motor Burn Out Missile Bit Test Set Multi-phase Blast Explosive Mission Control Equipment Modular Combat Shotgun Miscellaneous Simulated Munitions Missile Defense Agency Missile Detect and Track Multipurpose Display Unit

B-11

FOUO

MDUR MEP MER MFD MFOM MG MGL MH MHT MHU MIL-STD MILSPEC MITL MJ MJU MK ML MLCS MLRS MLSTS MLT mm MMA MMHE MMLA MMP MMS MMSI MMW MNC-I MO MOAB MOD MOFA MOFM MOLT MOP MOSP MOTS MOUT MPE MPRL MPS MPSM MRA MRATA MRIU

Multipurpose Display Unit Replacement Mission Equipment Package pp 12-26 Multi-Function Display Multiple Launch Rocket System (MLRS) Family of Munitions Machine Gun Multiple Grenade Launcher Munitions Handling Equipment Munitions Handling Trailer Munitions Handling Truck Munitions Handling Unit Military Standard Military Specification Man-In-The-Loop Munitions Countermeasures Mobile Jettison Unit Mark (Navy Weapons Designator for Bombs) Miscellaneous Munitions Modular Launcher Communications System Multiple Launch Rocket System Missile Launch System Test Set Munitions Lift Trailer Millimeter Multi-Mission Maritime Aircraft Munitions Material Handling Equipment Missile Munitions Loading Adapter Munitions Movement Plan Mission Management Subsystem Miniature Munitions Sores Interface Millimeter Wave Multi-National Corps - Iraq Multi-Option Massive Ordnance Air Blast (MOAB) Modification Model Multi-Option Fuze for Artillery Multi-Option Fuze for Mortars Manually Operated Lift Truck Massive Ordinance Penetrator Multi-Mission Optronic Payload Modified or Modifiable off the Shelf Military Operations on Urban Terrain Mission Planning Environment Multi-Purpose Rotary Launcher Mission Planning System Multi-Purpose Submunition Mechanical Ram Assembly Missile Radar Altimeter Test Assembly Missile Remote Interface Unit

B-12

FOUO

MRP MS MSGL MSL m/s MSUG MSUS MT MTADS/M-TADS MTI MTK MTSQ MTV MUSTANG MW N NALC

NAS NASAMS NATO MAU NAVAIR NAVAIRSYSCOM NAVFLIR NAWC NAWCWD NDI NEW NG NIIRS NLOS NLOSC NM NSB NTS NTSR NVD NVG NVIS OAPT OCS OEF OFP OFP OFS OH

Munitions Requirement Process Miznay Szhardin Multiple-shot Grenade Launcher Missile Meters Per Second Missile Sustainment Group Missile Sustainment Squadron Mechanical Time Mounts Modernized Target Acquisition Designation Sight Moving Target Indicator Moving Target Kill Mechanical Time Superquick Magnesium/Teflon/Viton Multi-User System Tester Next Generation Mega Watt Navy Navy Ammunition Logistics Code (Air Force used CRD) NALC codes can be found in Navy Supplement (NAVSUP) P-802 TW010-AA-ORD-010 (NALC Manual) Naval Air Station Norwegian Advanced Surface-to-Air Missile System North Atlantic Treaty Organization Miscellaneous Armament Unit Naval Air Naval Air Systems Command Navigation Forward Looking Infrared Naval Air Warfare Center Naval Air Warfare Center Weapons Development, China Lake Non Developmental Item Net Explosive Weight National Guard National Imagery Interpretability Rating Scale Non Line of Site Non Line of Site Cannon Nautical Mile Near Surface Burst Night Targeting System Non Traditional Surveillance & Reconnaissance Night Vision Device Night Vision Goggles Night Vision Imaging Systems Off-Aircraft Pylon Tester Operational Cable Set Operation Enduring Freedom Operational Flight Plan Operational Flight Test Program Flight Management System Operational Flight Software Observation Helicopter

B-13

FOUO

OIF OPR OSHA OSI OSRVT OT OT/E OTS P3I P5CTS P5CTS/TCTS PA PACS PAD PATEC PATS PAU PAW PBX PBXN PC PD PD/DLY PDDM PDCU PDW PE PELE PEO PEP PG PGM PGMPS PGS PGSM PGU PHaSR PIBD PID PIDS PLGS PLOCAAS PMA PNVS POL POM POP PPE

Operation Iraqi Freedom Office of Primary Responsibility Occupational Safety and Health Administration Air Force Office of Special Investigations One System Remote Video Terminal Operational Test Operational Test and Evaluation Off the Shelf Pre-Planned Product Improvement P5 Combat Training System P5 Combat Training System/Tactical Combat Training System External Munitions Dispensing Device Programmable Armament Control Set Prompt Agent Defeat Portable Automatic Test Equipment Calibrator Portable Automated Test Station Positive Arming Units Passive Attack Weapon Plastic Bonded Explosive Plastic Bonded Explosive with a polyurethane or fluoroelastomer binding ingredient Personal Computer Point Detonating Pont Detonating/Delay Power Distribution Denial Munitions Portable Display Control Unit Personal Defense Weapon Precision Engagement Penetrator with Enhanced Lateral Efficiency Program Executive Office Producibility Enhancement Program Ammunitions Precision Guided Munition Precision Guided Munition Planning System Precision Guided Sub-munitions Precision Guided Sub-Missile Precision Guidance Unit Personnel Halting and Stimulation Response Point Initiating Base Detonating Positive Identification Pylon Integrated Dispenser System Precision Laser Guidance Set Powered Low Cost Autonomous Attack System Program Management Air Pilot Night Vision Sensor Petroleum Oil Lubricants Program Objective Memorandum Period of Performance Pre-Production Engineering

B-14

FOUO

PPM PPS PPSL PREPO PROP PRX PS PSAS p-SDF PSI PSYOPS PTDS PW Q QRC QRU QTDD R&D RAA RAAMS RAD RAID RAM RAMS RAMICS RAP RD RDU RDX REM RF RFI RHA RIFL RISTA RL RLA RM RMP RNP ROE RP rpm RQS RR RRLP RSTA RTIC

Pneumatic Power Module Pneumatic Power Source Predator Primary Satellite Link Prepositioned Propellant Proximity Propulsion Section Persistent Surface Attack Systems pyrotechnic Self Destruct Fuzes Pounds per Square Inch Psychological Operations Persistent Threat Detection System Internal Dispenser Unmanned Aircraft System Quick Reaction Capability Quick Reaction Unitary Quad/Target Detection Device Research and Development Required Available Assets Remote Anti-Armor Mine System Ram Air Decelerator Ram Air Inflated Decelerator Reliability, availability, and Maintainability Reliability Asset Monitoring System Rapid Mine Clearing System Rocket Assisted Projectile Dummy Rockets Refrigerated Detector Unit Cyclotrimethylenetrinitramine, also known cyclonite, hexogen, and T4, is an explosive Range Encryption Module Radio Frequency Radio Frequency Interferometer Rolled Homogeneous Steel Reversible In-Flight Locking Reconnaissance, Intelligence, Surveillance, Target Acquisition Rockets Rotary Launcher Assembly Rocket Motor Radar Modernization Program Required Navigation Performance Rules of Engagement Red Phosphorous Revolutions Per Minute Rescue Squadron Risk Reduction Reduced Ricochet Limited Penetration Real Time Information in Cockpit

B-15

FOUO

RW RxTx S/W S&A S-A SAASM SADL SAF SAL SAM SAPHEI SAR SASR SASS SAW SB SBRA SBRC SCAS SCW SDB SDD SDL SEAD SECBM SED SFW SHP SID SIGINT SIT SLAM-ER SLAP SLAP-T SLEP SM SMO SMOFP SMP SOF SOPD SP SPM SPO SQ SRR SRTA SRU

Rotary Wing Receiver/Transmitter Software Safe and Arming or Safe and Arm Safety Arming Device Selective Availability Anti-Spoofing Module Situational Awareness Data Link Save & Arming Fuse Semi-Active Laser Surface-to-Air Missile Semi-Armor Piercing High Explosive Incendiary Synthetic Aperture Radar Special Application Sniper Rifle Semi-Automatic Sniper System Squad Automatic Weapon Sustainment Block Smart Bomb Rack Assembly Smart Bomb Release Controller Shortened Control Actuation Section Newer Short Cord Small Diameter Bomb System Development and Demonstration Switchable Data Links Suppress Enemy Air Defense Modified ECBM for 1760 Scramjet Engine Demonstrator Sensor Fuzed Weapon Shaft Horse Power Standoff Intelligence Detection Signal Intelligence System Integration Test Standoff Land Attack Missile-Expanded Response Saboted Light Armor Penetrator Saboted Light Armor Penetrator Training Service Life Extension Program Sub-munition Stores Management Overlay Sustainment Management Office Stores Management Operational Flight Program Stores Management Processor Special Operations Forces Standoff Outside Point Defense Self Propelled Shots Per Minute System Program Office Super Quick System Ready Review Short Range Training Ammunition Shop Replaceable Unit

B-16

FOUO

SSD SSW STOVL SU SU SWING SWIR T2KU TA TALD TAMIDS TBD TBP TC TACMS TACOM TAD SADARM TCDL TCP TCTS TD TDD TDFA TDS TENA TER TERCOM TF TH3 TIC TJS TLAM TLE TM TMD TMR TNT TO TP TPI TPSs TPT TRANSCOM TRL TSAR

Safe Separation Device Small Smart Weapon Short Takeoff Vertical Landing Stores Suspension and Release Stores Release Unit or Suspension Unit (Munitions Dispenser) Smart Weapon Integration Next Generation Short-Wave Infrared TACMS 2000 Unitary Target Area Tactical Aircraft Tactical Air-Launched Decoy Target Acquisition Minefield Detection System To Be Determined To Be Published Training Cartridge Tactical Missile System Tank and Automotive Command Towed Artillery Digitization Sense and Destroy Armor Tactical Command Data Transformation Campaign Plan Tactical Combat Training System Target Detector Technology Demonstration Target Detection Device Time Delay Fuze Assembly Threat Detection System Test and Training Enabling Architecture Triple Ejection Rack Terrain-Contour Matching Terrain Following Thermite Mixture Troops in Contact Tactical Jamming System Tomahawk Land Attack Missile Target Location Error Miscellaneous Tanks Tactical Munition Dispenser Total Munitions Requirements Trinitrotoluene Technical Order Targeting Pod Target Practice Targeting Pod Integration Test Program Sets Target Practice Tracer Transportation Command Technology Readiness Level Tactical Synthetic Aperture Radar

B-17

FOUO

TSPI TT TTP TV TVGS UAI UALS UAS UAV UBL UCAV UDL UHF UMR UMT UNIX UNR UNS UPC UPCO US USAF USMC USN USSOCOM USSTRATCOM UUT VHF VL VME VRP VSM V/STOL VT VUIT-2 WAF WAFFAR WASM WAU WCMD WCMD-ER WCU WD WDU WGU WIA WP WPT WSO

Time, Space, Position Information Test Items Tactics, Techniques, and Procedures Television Television Guided Section Universal Armament Interface Universal Ammunition Loading System Unmanned Aerial System Unmanned Aerial Vehicle Unit Basic Load Uninhabited Combat Air Vehicles Universal Delinker Loader Ultra High Frequency Urgent Material Release Universal Munitions Trailer Universal Network Information Exchange Urgent Need Request Urgent Need Statement Universal Project Code Universal Propulsion company United States United States Air Force United States Marine Corps United States Navy United States Special Operations Command United States Strategic Command Units Under Test Very High Frequency Visible Light Versa Module Eurocard Vortex Ring Parachute Very Small Missile Vertical/Short Take-Off or Landing Proximity Fuze Video from UAS for Interoperability Teaming - Level 2 Weapons Attribute File Wrap-Around Folding Fin Aircraft Rocket Wide Area Search Munition Weapons Section Unit Wind Corrected Munitions Dispenser WCMD Extended Range Weapons Control Unit Warheads Weapons Delivery of Dispenser Unit Weapons Guidance Unit Weapon Impact Assessment White Phosphorus Weapons Preload Tester Weapon System Operator

B-18

FOUO

WT WUN WWP ZRF

Training Warheads Warfighter Urgent Need Wing Weapons Pylon Zero Retention Force

B-19

FOUO

INTENTIONALLY LEFT BLANK

B-20

FOUO