A1-DASSAULT AVIATION Mirage-5F-NFM-000-r0
PERFORMANCE ANALYSIS
Mirage-5F / Nesher DASSAULT AVIATION (SNECMA ATAR-9C)
CAUTION STATEMENT : This document is to be use only for simulation. Do not try to apply the procedures and or advices contained in it if you have the opportunity to fly this plane in real life. By the way, if you had (or still have) flew this aircraft, your comments, criticism and more are welcome LICENSE : This document has been created by J.M. LANGERON / TOPOLO, (http://topolo.free.fr/) all the values used to model the aircraft behavior have been computed by him, like all performance charts presented here. If you want to use these data, or part of it, please contact the author by personal message to TOPOLO on check-six forum: (http://www.checksix-forums.com/)
I–1-1
A1-DASSAULT AVIATION Mirage-5F-NFM-000-r0
Level Flight Envelope
I–1-2
A1-DASSAULT AVIATION Mirage-5F-NFM-000-r0
Level Flight Envelope DATA BASIS : ESTIMATED CONDITIONS: •Standard Day •Max AB
Aircraft : Mirage-5F Engine :SNECMA ATAR-9C Level Flight Enveloppe Full AB
65,000
Clean A/C GW = 18,238 lbs
60,000 55,000 50,000 45,000
2 x AIM-9 GW = 18,724 lbs
35,000 30,000 25,000 20,000
15,000
IAS < 750 Kts SL-30,000ft IAS < 700 Kts over 30,000ft Mach number < 2.00
10,000 5,000
0 0.00 0.10 0.20 0.30 0.40 0.50 0.60 0.70 0.80 0.90 1.00 1.10 1.20 1.30 1.40 1.50 1.60 1.70 1.80 1.90 2.00 2.10 2.20 2.30 2.40 Mach
DATA BASIS : ESTIMATED CONDITIONS: •Standard Day •MILL Power
Aircraft : Mirage-5F Engine :SNECMA ATAR-9C Level Flight Enveloppe MIL Power
65,000 60,000
Clean A/C GW = 18,238 lbs
55,000
50,000 45,000 40,000
Alt (ft)
Alt (ft)
40,000
35,000 30,000 25,000 20,000
2 x AIM-9 GW = 18,724 lbs
15,000
IAS < 750 Kts SL-30,000ft IAS < 700 Kts over 30,000ft Mach number < 2.00
10,000 5,000
0 0.00 0.10 0.20 0.30 0.40 0.50 0.60 0.70 0.80 0.90 1.00 1.10 1.20 1.30 1.40 1.50 1.60 1.70 1.80 1.90 2.00 2.10 2.20 2.30 2.40 Mach
I–1-3
A1-DASSAULT AVIATION Mirage-5F-NFM-000-r0
Turn Performance Aircraft : Mirage-5F Engine :SNECMA ATAR-9C CONFIGURATIONS : •DRAG INDEX = 20 (2xAIM-9) •50% internal fuel •GW= 18,724 lbs / 8,482 Kg
I–1-4
A1-DASSAULT AVIATION Mirage-5F-NFM-000-r0
Turn Rate – Summary DATA BASIS : ESTIMATED
Aircraft : Mirage-5F Engine :SNECMA ATAR-9C
CONDITIONS: •Standard Day •Max AB
CONFIGURATIONS : •DRAG INDEX = 20 (2xAIM-9) •GW=18,724lbs Maximum Available Turn Rate
25.00 0
10,000 20,000 30,000
Maximum instantaneous turn rate (deg/s)
20.00
40,000
Limitation by Maximum Lift, not ADHEMAR red only 15.00
10.00
5.00
0.00 0.00
0.20
0.40
0.60
0.80
1.00
1.20
1.40
1.60
1.80
2.00
2.20
2.40
Mach number
Maximum Sustained Turn rate (deg/s) 25.00 0 10,000 20,000 30,000
Sustained Turn rate (deg/s)
20.00
40,000
15.00
10.00
5.00
0.00 0.00
0.20
0.40
0.60
0.80
1.00
1.20
Mach number
I-1-5
1.40
1.60
1.80
2.00
2.20
2.40
A1-DASSAULT AVIATION Mirage-5F-NFM-000-r0
Load Factor – Summary DATA BASIS : ESTIMATED
Aircraft : Mirage-5F Engine :SNECMA ATAR-9C
CONDITIONS: •Standard Day •Max AB
CONFIGURATIONS : •DRAG INDEX = 20 (2xAIM-9) •GW=18,724lbs
Maximum Available Load Factor 10.00 0 10,000
9.00
20,000 30,000 40,000
7.00
6.00
5.00
Limitation by Maximum Lift, not ADHEMAR red only
4.00
3.00
2.00
1.00 0.00
0.20
0.40
0.60
0.80
1.00
1.20
1.40
1.60
1.80
2.00
2.20
2.40
Mach number
Maximum Sustained Load Factor (Ng) 10.00
0 10,000 9.00
20,000 30,000
8.00
Sustained Load Factor (Ng)
Maximum Available Load Factor (Ng)
8.00
40,000
7.00
6.00
5.00
4.00
3.00
2.00
1.00 0.00
0.20
0.40
0.60
0.80
1.00
1.20
Mach number
I-1-6
1.40
1.60
1.80
2.00
2.20
2.40
A1-DASSAULT AVIATION Mirage-5F-NFM-000-r0
Turn Performance – Sea Level DATA BASIS : ESTIMATED
Aircraft : Mirage-5F Engine :SNECMA ATAR-9C
CONDITIONS: •Standard Day •Max AB
CONFIGURATIONS : •DRAG INDEX = 20 (2xAIM-9) •GW=18,724lbs
24.00
2G
20.00
18.00
16.00
5G
6G
7G
8G
9G
Quickest Turn = 21.0 deg/s
-450 -300 -150
Max. Sustained Turn = 13.7 deg/s
14.00
0 12.00
+150 10.00
+300
MAXIMUM AIR SPEED
Turn Rate (degree per second)
4G
Limitation by Maximum Lift, not ADHEMAR red only
22.00
3G
8.00
6.00
+450 4.00
2.00
0.00 0
50
100
150
200
250
300
350
400
450
CAS (Kts)
I–1-7
500
550
600
650
700
750
800
A1-DASSAULT AVIATION Mirage-5F-NFM-000-r0
Turn Performance – 5,000 ft
24.00
DATA BASIS : ESTIMATED
Aircraft : Mirage-5F Engine :SNECMA ATAR-9C
CONDITIONS: •Standard Day •Max AB
CONFIGURATIONS : •DRAG INDEX = 20 (2xAIM-9) •GW=18,724lbs
2G
3G
4G
5G
6G
7G
8G
9G
Limitation by Maximum Lift, not ADHEMAR red only
22.00
20.00
18.00
14.00
-450 -300 -150 Max. Sustained Turn = 11.9 deg/s
12.00
0
10.00
+150
MAXIMUM AIR SPEED
Turn Rate (degree per second)
16.00
Quickest Turn = 19.5 deg/s
8.00
+300
6.00
4.00
+450 2.00
0.00 0
50
100
150
200
250
300
350
400
450
CAS (Kts)
I–1-8
500
550
600
650
700
750
800
A1-DASSAULT AVIATION Mirage-5F-NFM-000-r0
Turn Performance – 10,000 ft DATA BASIS : ESTIMATED
Aircraft : Mirage-5F Engine :SNECMA ATAR-9C
CONDITIONS: •Standard Day •Max AB
CONFIGURATIONS : •DRAG INDEX = 20 (2xAIM-9) •GW=18,724lbs
24.00
2G
3G
4G
5G
6G
7G
8G
9G
22.00
20.00
Limitation by Maximum Lift, not ADHEMAR red only
Quickest Turn = 18.0 deg/s 18.00
Turn Rate (degree per second)
16.00
14.00
12.00
-450 -300 -150
Max. Sustained Turn = 10.2 deg/s 10.00
0
MAXIMUM AIR SPEED
8.00
+150 6.00
+300
4.00
2.00
0.00 0
50
100
150
200
250
300
350
400
450
CAS (Kts)
I–1-9
500
550
600
650
700
750
800
A1-DASSAULT AVIATION Mirage-5F-NFM-000-r0
Turn Performance – 15,000 ft DATA BASIS : ESTIMATED
Aircraft : Mirage-5F Engine :SNECMA ATAR-9C
CONDITIONS: •Standard Day •Max AB
CONFIGURATIONS : •DRAG INDEX = 20 (2xAIM-9) •GW=18,724lbs
24.00
2G
3G 4G
5G
6G 7G
8G
9G
22.00
20.00
Limitation by Maximum Lift, not ADHEMAR red only
18.00
Turn Rate (degree per second)
16.00
14.00
12.00
Quickest Turn = 16.3 deg/s
-450 -300
10.00
-150 Max. Sustained Turn = 8.6 deg/s 0
8.00
MAXIMUM AIR SPEED
6.00
+150
4.00
+300
2.00
0.00 0
50
100
150
200
250
300
350
400
450
CAS (Kts)
I – 1 - 10
500
550
600
650
700
750
800
A1-DASSAULT AVIATION Mirage-5F-NFM-000-r0
Turn Performance – 20,000 ft DATA BASIS : ESTIMATED
Aircraft : Mirage-5F Engine :SNECMA ATAR-9C
CONDITIONS: •Standard Day •Max AB
CONFIGURATIONS : •DRAG INDEX = 20 (2xAIM-9) •GW=18,724lbs
24.00
2G
3G 4G 5G 6G 7G 8G
9G
22.00
20.00
Limitation by Maximum Lift, not ADHEMAR red only
18.00
Turn Rate (degree per second)
16.00
14.00
12.00
Quickest Turn = 14.8 deg/s
-450 10.00
-300 -150
8.00
Max. Sustained Turn = 7.1 deg/s 0
4.00
MAXIMUM AIR SPEED
6.00
+150
2.00
0.00 0
50
100
150
200
250
300
350
400
450
CAS (Kts)
I – 1 - 11
500
550
600
650
700
750
800
A1-DASSAULT AVIATION Mirage-5F-NFM-000-r0
Turn Performance – 25,000 ft DATA BASIS : ESTIMATED
Aircraft : Mirage-5F Engine :SNECMA ATAR-9C
CONDITIONS: •Standard Day •Max AB
CONFIGURATIONS : •DRAG INDEX = 20 (2xAIM-9) •GW=18,724lbs
24.00
2G
3G 4G 5G 6G 7G 8G
9G
22.00
20.00
Limitation by Maximum Lift, not ADHEMAR red only
18.00
Turn Rate (degree per second)
16.00
14.00
12.00
Quickest Turn = 14.0 deg/s
10.00
-450 -300 8.00
-150 Max. Sustained Turn = 6.0 deg/s
MAXIMUM AIR SPEED
6.00
0 4.00
+150 2.00
0.00 0
50
100
150
200
250
300
350
400
450
CAS (Kts)
I – 1 - 12
500
550
600
650
700
750
800
A1-DASSAULT AVIATION Mirage-5F-NFM-000-r0
Turn Performance – 30,000 ft DATA BASIS : ESTIMATED
Aircraft : Mirage-5F Engine :SNECMA ATAR-9C
CONDITIONS: •Standard Day •Max AB
CONFIGURATIONS : •DRAG INDEX = 20 (2xAIM-9) •GW=18,724lbs
24.00
2G
3G 4G 5G 6G 7G 8G 9G
22.00
20.00
Limitation by Maximum Lift, not ADHEMAR red only
18.00
Turn Rate (degree per second)
16.00
14.00
12.00
Quickest Turn = 13.2 deg/s
10.00
8.00
-450 -300 6.00
-150 MAXIMUM AIR SPEED
Max. Sustained Turn = 4.9 deg/s 0
4.00
2.00
+150 0.00 0
50
100
150
200
250
300
350
400
450
CAS (Kts)
I – 1 - 13
500
550
600
650
700
750
800
A1-DASSAULT AVIATION Mirage-5F-NFM-000-r0
Turn Performance – 35,000 ft DATA BASIS : ESTIMATED
Aircraft : Mirage-5F Engine :SNECMA ATAR-9C
CONDITIONS: •Standard Day •Max AB
CONFIGURATIONS : •DRAG INDEX = 20 (2xAIM-9) •GW=18,724lbs
24.00
2G 3G 4G 5G 6G 7G 8G
9G
22.00
20.00
Limitation by Maximum Lift, not ADHEMAR red only
18.00
Turn Rate (degree per second)
16.00
14.00
12.00
Quickest Turn = 12.3 deg/s
10.00
8.00
-450 -300
6.00
MAXIMUM AIR SPEED
-150 Max. Sustained Turn = 4.1 deg/s 4.00
0 2.00
+150 0.00 0
50
100
150
200
250
300
350
400
450
CAS (Kts)
I – 1 - 14
500
550
600
650
700
750
800
A1-DASSAULT AVIATION Mirage-5F-NFM-000-r0
Climb Performance Aircraft : Mirage-5F Engine :SNECMA ATAR-9C CONFIGURATIONS : •DRAG INDEX = 20 (2xAIM-9) •50% internal fuel •GW= 18,724 lbs / 8,482 Kg
I – 1 - 15
A1-DASSAULT AVIATION Mirage-5F-NFM-000-r0
DATA BASIS : ESTIMATED
Aircraft : Mirage-5F Engine :SNECMA ATAR-9C
CONDITIONS: •Standard Day •Max AB
CONFIGURATIONS : •DRAG INDEX = 20 (2xAIM-9) •GW=18,724lbs Instantaneous Constant Speed Climb Rate
600
550 500
450
Excess Specific Power (ft/s)
0
400
5,000 10,000
350
15,000 20,000
300
25,000 30,000
250
35,000 40,000
200
45,000
150 100 50 0 0.00 0.10 0.20 0.30 0.40 0.50 0.60 0.70 0.80 0.90 1.00 1.10 1.20 1.30 1.40 1.50 1.60 1.70 1.80 1.90 2.00 2.10 2.20 2.30 2.40 Mach
Constant Speed Climb Angle 90.00
80.00
70.00 0
60.00
Climb Angle (deg)
5,000 10,000
50.00
15,000 20,000
25,000
40.00
30,000 35,000
30.00
40,000
20.00
10.00
0.00 0.00 0.10 0.20 0.30 0.40 0.50 0.60 0.70 0.80 0.90 1.00 1.10 1.20 1.30 1.40 1.50 1.60 1.70 1.80 1.90 2.00 2.10 2.20 2.30 2.40 Mach
I - 1 - 16
A1-DASSAULT AVIATION Mirage-5F-NFM-000-r0
DATA BASIS : ESTIMATED
Aircraft : Mirage-5F Engine :SNECMA ATAR-9C
CONDITIONS: •Standard Day •MIL Power
CONFIGURATIONS : •DRAG INDEX = 20 (2xAIM-9) •GW=18,724lbs Instantaneous Constant Speed Climb Rate
250
200
Excess Specific Power (ft/s)
0 5,000 10,000
150
15,000 20,000 25,000 30,000
100
35,000 40,000 45,000
50
0 0.00 0.10 0.20 0.30 0.40 0.50 0.60 0.70 0.80 0.90 1.00 1.10 1.20 1.30 1.40 1.50 1.60 1.70 1.80 1.90 2.00 2.10 2.20 2.30 2.40 Mach
Constant Speed Climb Angle 90.00
80.00
70.00 0
60.00
Climb Angle (deg)
5,000 10,000
50.00
15,000 20,000
25,000
40.00
30,000 35,000
30.00
40,000
20.00
10.00
0.00 0.00 0.10 0.20 0.30 0.40 0.50 0.60 0.70 0.80 0.90 1.00 1.10 1.20 1.30 1.40 1.50 1.60 1.70 1.80 1.90 2.00 2.10 2.20 2.30 2.40 Mach
I - 1 - 17
A1-DASSAULT AVIATION Mirage-5F-NFM-000-r0
Acceleration Performances Aircraft : Mirage-5F Engine :SNECMA ATAR-9C CONFIGURATIONS : •DRAG INDEX = 20 (2xAIM-9) •50% internal fuel •GW= 18,724 lbs / 8,482 Kg
I – 1 - 18
A1-DASSAULT AVIATION Mirage-5F-NFM-000-r0
Acceleration Diagram
0
DATA BASIS : ESTIMATED
Aircraft : Mirage-5F Engine :SNECMA ATAR-9C
CONDITIONS: •Standard Day •Max10,000 AB
CONFIGURATIONS : •DRAG INDEX = 20 (2xAIM-9) •GW=18,724lbs
20,000
Acceleration (Max Thrust AB) 180 165 150
10,000 ft
135 120
20,000 ft
Time (s)
105 90 75 60 45 30
Sea Level
15 0 0.30
0.40
0.50
30,000
0.60
30,000
0.70
0.80
0.90
1.00
1.10
1.20
1.30
1.40
1.50
1.60
1.70
Mach
36,000
Acceleration (Max Thrust AB) 180 165 150 135
36,000 ft
120
30,000 ft
Time (s)
105 90
30,000 ft
75
60 45 30 15
0 0.30
0.40
0.50
0.60
0.70
0.80
0.90
1.00
1.10
1.20
1.30
Mach
I – 1 - 19
1.40
1.50
1.60
1.70
1.80
1.90
2.00
2.10
2.20
