KALAIGNAR KARUNANIDHI INSTITUTE OF TECHNOLOGY KANNAMPALAYAM, COIMBATORE‐641 402. Course plan Department
:
AERONAUTICAL ENGINEERING
Semester
:
VIII
Academic Year
:
2013 ‐ 2014
Subject
:
ROCKETS AND MISSILES
Faculty Name
:
Mr. O.MANIYARASU
F/TL/22
Objectives:
To introduce basic concepts of design of design and trajectory estimation of rocket of rocket and missiles.
UNIT
1
2
3
UNIT TITLE
ROCKETS SYSTEM
AERODYNAMICS OF ROCKETS AND MISSILES
ROCKET MOTION IN FREE SPACE AND GRAVITATIONAL FIELD
TOPICS
PERIODS FOR EACH TOPICS
Ignition System in rockets
1
Types of Igniters of Igniters Igniter Design Considerations Design Consideration of liquid of liquid Rocket Combustion Chamber Injector Propellant Feed Lines, Valves Propellant Tanks Outlet Helium Pressurized Turbine feed Systems Propellant Slash Propellant Hammer Elimination of Geysering of Geysering Effect in Missiles Combustion System of Solid of Solid Rockets.
2
ASSIGNMENT
VERIFICATION OF STUDENT’S CLASS NOTES
I
Once in a week
II
Once in a week
III
Once in a week
3 4 5 6 7 8 9 10 11 12
Airframe Components of Rockets of Rockets and Missiles Airframe Components of Rockets of Rockets and Missiles Forces Acting on a Missile While Passing Through Atmosphere Classification of Missiles of Missiles Classification of Missiles of Missiles Methods of Describing of Describing Aerodynamic Forces and Moments Methods of Describing of Describing Aerodynamic Forces and Moments Lateral Aerodynamic Moment Lateral Damping Moment Longitudinal Moment of a of a Rocket Lift and Drag Forces Drag Estimation Body Upwash and Downwash in Missiles Rocket Dispersion Numerical Problems Numerical Problems
13
One Dimensional rocket Motions in Free Space One Dimensional rocket Motions in Homogeneous Gravitational Fields Two Dimensional rocket Motions in Free Space Two Dimensional rocket Motions in Homogeneous Gravitational Fields Description of Vertical, of Vertical, Inclined and Gravity Turn Trajectories Description of Vertical, of Vertical, Inclined and Gravity Turn Trajectories Description of Vertical, of Vertical, Inclined and Gravity Turn Trajectories Determination of range of range Altitude Simple Altitude Simple
29
14 15 16 17 18 19 20 21 22 23 24 25 26 27 28
30 31 32 33 34 35 36 37 38
4
5
STAGING AND CONTROL OF ROCKETS AND MISSILES
MATERIALS FOR ROCKETS AND MISSILES
Approximations to Burnout Velocity Approximations to Burnout Velocity
39
Rocket Vector Control Methods Thrust determination SITVC Multistaging of rockets Vehicle Optimization Stage Separation Dynamics Separation Techniques
41
Selection of Materials Selection of Materials Selection of Materials Special Requirements of Materials to Perform under Adverse Conditions Special Requirements of Materials to Perform under Adverse Conditions Special Requirements of Materials to Perform under Adverse Conditions
49
40
42 43 44 45
IV
Once in a week
V
Once in a week
46 47 48
50 51 52 53 54
TEXT BOOKS 1. Sutton.G.P, “Rocket Propulsion Elements”, John Wiley & Sons Inc., New York, 1993. 2. Cornelisse, J.W., “Rocket Propulsion and Space Dynamics”, J.W., Freeman & Co. Ltd., London, 1982. REFERENCES 1. Mathur, M., and Sharma, R.P., “Gas Turbines and Jet and Rocket Propulsion”, Standard Publishers, New Delhi 1998. 2. Parket, E.R., “Materials for Missiles and Spacecraft”, McGraw‐Hill Book Co. Inc., 1982. 3. M.J.Zucrow, “Missile Propulsion”, John Wiley & sons. 4. H.S.Mukunda, “Understanding Aerospace Chemical Propulsion”, Interline Publishing Company Bangalore. 1.
Examination Topics
SL.No
Examination
1
Internal Examination – I
Topic
Marks
Unit ‐ I
50
Unit ‐ I & Unit ‐ III
50
Unit ‐ IV & Unit ‐ V
50
As per Anna University Chennai Schedule As per Anna University
2
Internal Examination – II
Chennai Schedule As per Anna University
3
2.
Date
Internal Examination – III
Chennai Schedule
Innovative work / Paper presentation 1. Students are asked to prepare a seminar on types of Rockets and Missiles.
3.
Evaluation system given by Anna University Chennai Marks
SL.No
Component Internal
1
Internal Examinations (I – III)
15
2
Attendance
5
3
University Examination
External
100 (Converted to 80 Marks)
4
Faculty
Total
100
HoD
Principal