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A1-DASSAULT AVIATION Mirage-III CJ-NFM-000-r0
Mirage-III CJ (1973)
DASSAULT AVIATION
(SNECMA ATAR-9C)
PERFORMANCE ANALYSIS
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
I – 1 - 1
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/)
Level Flight Envelope
A1-DASSAULT AVIATION Mirage-III CJ-NFM-000-r0
I – 1 - 2
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
45,000
50,000
55,000
60,000
65,000
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
Alt
(ft
)
Mach
Level Flight EnveloppeMIL Power
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
45,000
50,000
55,000
60,000
65,000
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
Alt
(ft
)
Mach
Level Flight EnveloppeFull AB
Level Flight Envelope
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : Mirage-III CJ
Engine :SNECMA ATAR-9C
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•MILL Power
Aircraft : Mirage-III CJ
Engine :SNECMA ATAR-9C
A1-DASSAULT AVIATION Mirage-III CJ-NFM-000-r0
I – 1 - 3
Clean A/C
GW = 16,629 lbs
2 x AIM-9
GW = 17,353 lbs
IAS < 750 Kts SL-30,000ft
IAS < 700 Kts over 30,000ft
Mach number < 2.00
Clean A/C
GW = 16,629 lbs
2 x AIM-9
GW = 17,353 lbs
IAS < 750 Kts SL-30,000ft
IAS < 700 Kts over 30,000ft
Mach number < 2.00
Turn Performance
Aircraft : Mirage-III CJ
Engine :SNECMA ATAR-9C
CONFIGURATIONS :
•DRAG INDEX = 20 (2xAIM-9)
•50% internal fuel
•GW= 17,353 lbs / 7,860 Kg
A1-DASSAULT AVIATION Mirage-III CJ-NFM-000-r0
I – 1 - 4
Turn Rate – Summary
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : Mirage-III CJ
Engine :SNECMA ATAR-9C
CONFIGURATIONS :
•DRAG INDEX = 20 (2xAIM-9)
•GW=17,353lbs
A1-DASSAULT AVIATION Mirage-III CJ-NFM-000-r0
I - 1 - 5
0.00
5.00
10.00
15.00
20.00
25.00
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
Su
sta
ine
d T
urn
ra
te (d
eg
/s)
Mach number
Maximum Sustained Turn rate (deg/s)
0
10,000
20,000
30,000
40,000
0.00
5.00
10.00
15.00
20.00
25.00
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
Maxim
um
in
sta
nta
neo
us tu
rn r
ate
(d
eg
/s)
Mach number
Maximum Available Turn Rate
0
10,000
20,000
30,000
40,000
Load Factor – Summary
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : Mirage-III CJ
Engine :SNECMA ATAR-9C
CONFIGURATIONS :
•DRAG INDEX = 20 (2xAIM-9)
•GW=17,353lbs
A1-DASSAULT AVIATION Mirage-III CJ-NFM-000-r0
I - 1 - 6
1.00
2.00
3.00
4.00
5.00
6.00
7.00
8.00
9.00
10.00
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
Ma
xim
um
Av
aila
ble
Lo
ad
Fa
cto
r (N
g)
Mach number
Maximum Available Load Factor
0
10,000
20,000
30,000
40,000
1.00
2.00
3.00
4.00
5.00
6.00
7.00
8.00
9.00
10.00
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
Su
sta
ine
d L
oa
d F
ac
tor
(Ng
)
Mach number
Maximum Sustained Load Factor (Ng)
0
10,000
20,000
30,000
40,000
0.00
2.00
4.00
6.00
8.00
10.00
12.00
14.00
16.00
18.00
20.00
22.00
24.00
0 50 100 150 200 250 300 350 400 450 500 550 600 650 700 750 800
Tu
rn R
ate
(d
eg
ree p
er
seco
nd
)
CAS (Kts)
Turn Performance – Sea Level
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : Mirage-III CJ
Engine :SNECMA ATAR-9C
CONFIGURATIONS :
•DRAG INDEX = 20 (2xAIM-9)
•GW=17,353lbs
A1-DASSAULT AVIATION Mirage-III CJ-NFM-000-r0
I – 1 - 7
Max. Sustained Turn = 14.8 deg/s
+150
0
-150
-450
+300
9G 8G 7G 6G 5G 4G 3G 2G
MA
XIM
UM
AIR
SP
EE
D
-300
+450
Quickest Turn = 21.9 deg/s
0.00
2.00
4.00
6.00
8.00
10.00
12.00
14.00
16.00
18.00
20.00
22.00
24.00
0 50 100 150 200 250 300 350 400 450 500 550 600 650 700 750 800
Tu
rn R
ate
(d
eg
ree p
er
seco
nd
)
CAS (Kts)
Turn Performance – 5,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : Mirage-III CJ
Engine :SNECMA ATAR-9C
CONFIGURATIONS :
•DRAG INDEX = 20 (2xAIM-9)
•GW=17,353lbs
A1-DASSAULT AVIATION Mirage-III CJ-NFM-000-r0
I – 1 - 8
+150
0
-150
-300
-450
+300
9G 8G 7G 6G 5G 4G 3G 2G
Quickest Turn = 20.3 deg/s
Max. Sustained Turn = 12.9 deg/s
MA
XIM
UM
AIR
SP
EE
D
+450
0.00
2.00
4.00
6.00
8.00
10.00
12.00
14.00
16.00
18.00
20.00
22.00
24.00
0 50 100 150 200 250 300 350 400 450 500 550 600 650 700 750 800
Tu
rn R
ate
(d
eg
ree p
er
seco
nd
)
CAS (Kts)
Turn Performance – 10,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : Mirage-III CJ
Engine :SNECMA ATAR-9C
CONFIGURATIONS :
•DRAG INDEX = 20 (2xAIM-9)
•GW=17,353lbs
A1-DASSAULT AVIATION Mirage-III CJ-NFM-000-r0
I – 1 - 9
+150
0
-150
-300
-450
+300
9G 8G 7G 6G 5G 4G 3G 2G
Max. Sustained Turn = 11.1 deg/s
MA
XIM
UM
AIR
SP
EE
D
Quickest Turn = 18.7 deg/s
+450
0.00
2.00
4.00
6.00
8.00
10.00
12.00
14.00
16.00
18.00
20.00
22.00
24.00
0 50 100 150 200 250 300 350 400 450 500 550 600 650 700 750 800
Tu
rn R
ate
(d
eg
ree p
er
seco
nd
)
CAS (Kts)
Turn Performance – 15,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : Mirage-III CJ
Engine :SNECMA ATAR-9C
CONFIGURATIONS :
•DRAG INDEX = 20 (2xAIM-9)
•GW=17,353lbs
A1-DASSAULT AVIATION Mirage-III CJ-NFM-000-r0
I – 1 - 10
+150
0
-150
-300
-450
9G 8G 7G 6G 5G 4G 3G 2G
Max. Sustained Turn = 9.4 deg/s
MA
XIM
UM
AIR
SP
EE
D
+300
Quickest Turn = 17.0 deg/s
0.00
2.00
4.00
6.00
8.00
10.00
12.00
14.00
16.00
18.00
20.00
22.00
24.00
0 50 100 150 200 250 300 350 400 450 500 550 600 650 700 750 800
Tu
rn R
ate
(d
eg
ree p
er
seco
nd
)
CAS (Kts)
Turn Performance – 20,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : Mirage-III CJ
Engine :SNECMA ATAR-9C
CONFIGURATIONS :
•DRAG INDEX = 20 (2xAIM-9)
•GW=17,353lbs
A1-DASSAULT AVIATION Mirage-III CJ-NFM-000-r0
I – 1 - 11
+150
0
-150
-300
-450
9G 8G 7G 6G 5G 4G 3G 2G
Quickest Turn = 15.5 deg/s
Max. Sustained Turn = 7.7 deg/s
MA
XIM
UM
AIR
SP
EE
D
+300
0.00
2.00
4.00
6.00
8.00
10.00
12.00
14.00
16.00
18.00
20.00
22.00
24.00
0 50 100 150 200 250 300 350 400 450 500 550 600 650 700 750 800
Tu
rn R
ate
(d
eg
ree p
er
seco
nd
)
CAS (Kts)
Turn Performance – 25,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : Mirage-III CJ
Engine :SNECMA ATAR-9C
CONFIGURATIONS :
•DRAG INDEX = 20 (2xAIM-9)
•GW=17,353lbs
A1-DASSAULT AVIATION Mirage-III CJ-NFM-000-r0
I – 1 - 12
+150
0
-150
-300
-450
9G 8G 7G 6G 5G 4G 3G 2G
Quickest Turn = 14.3 deg/s
Max. Sustained Turn = 6.5 deg/s
MA
XIM
UM
AIR
SP
EE
D
0.00
2.00
4.00
6.00
8.00
10.00
12.00
14.00
16.00
18.00
20.00
22.00
24.00
0 50 100 150 200 250 300 350 400 450 500 550 600 650 700 750 800
Tu
rn R
ate
(d
eg
ree p
er
seco
nd
)
CAS (Kts)
Turn Performance – 30,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : Mirage-III CJ
Engine :SNECMA ATAR-9C
CONFIGURATIONS :
•DRAG INDEX = 20 (2xAIM-9)
•GW=17,353lbs
A1-DASSAULT AVIATION Mirage-III CJ-NFM-000-r0
I – 1 - 13
+150
0
-150
-300
-450
9G 8G 7G 6G 5G 4G 3G 2G
Max. Sustained Turn = 5.4 deg/s
MA
XIM
UM
AIR
SP
EE
D
Quickest Turn = 13.7 deg/s
0.00
2.00
4.00
6.00
8.00
10.00
12.00
14.00
16.00
18.00
20.00
22.00
24.00
0 50 100 150 200 250 300 350 400 450 500 550 600 650 700 750 800
Tu
rn R
ate
(d
eg
ree p
er
seco
nd
)
CAS (Kts)
Turn Performance – 35,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : Mirage-III CJ
Engine :SNECMA ATAR-9C
CONFIGURATIONS :
•DRAG INDEX = 20 (2xAIM-9)
•GW=17,353lbs
A1-DASSAULT AVIATION Mirage-III CJ-NFM-000-r0
I – 1 - 14
0
-150
-300
-450
9G 8G 7G 6G 5G 4G 3G 2G
Max. Sustained Turn = 4.5 deg/s
MA
XIM
UM
AIR
SP
EE
D
Quickest Turn = 12.7 deg/s
+150
Climb Performance
A1-DASSAULT AVIATION Mirage-III CJ-NFM-000-r0
I – 1 - 15
Aircraft : Mirage-III CJ
Engine :SNECMA ATAR-9C
CONFIGURATIONS :
•DRAG INDEX = 20 (2xAIM-9)
•50% internal fuel
•GW= 17,353 lbs / 7,860 Kg
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : Mirage-III CJ
Engine :SNECMA ATAR-9C
CONFIGURATIONS :
•DRAG INDEX = 20 (2xAIM-9)
•GW=17,353lbs
A1-DASSAULT AVIATION Mirage-III CJ-NFM-000-r0
I - 1 - 16
0
50
100
150
200
250
300
350
400
450
500
550
600
650
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
Excess S
pecif
ic P
ow
er
(ft/
s)
Mach
Instantaneous Constant Speed Climb Rate
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
45,000
0.00
10.00
20.00
30.00
40.00
50.00
60.00
70.00
80.00
90.00
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
Cli
mb
An
gle
(d
eg
)
Mach
Constant Speed Climb Angle
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•MIL Power
Aircraft : Mirage-III CJ
Engine :SNECMA ATAR-9C
CONFIGURATIONS :
•DRAG INDEX = 20 (2xAIM-9)
•GW=17,353lbs
A1-DASSAULT AVIATION Mirage-III CJ-NFM-000-r0
I - 1 - 17
0
50
100
150
200
250
300
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
Excess S
pecif
ic P
ow
er
(ft/
s)
Mach
Instantaneous Constant Speed Climb Rate
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
45,000
0.00
10.00
20.00
30.00
40.00
50.00
60.00
70.00
80.00
90.00
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
Cli
mb
An
gle
(d
eg
)
Mach
Constant Speed Climb Angle
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
Acceleration Performances
A1-DASSAULT AVIATION Mirage-III CJ-NFM-000-r0
I – 1 - 18
Aircraft : Mirage-III CJ
Engine :SNECMA ATAR-9C
CONFIGURATIONS :
•DRAG INDEX = 20 (2xAIM-9)
•50% internal fuel
•GW= 17,353 lbs / 7,860 Kg
0
15
30
45
60
75
90
105
120
135
150
165
180
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
Tim
e (
s)
Mach
Acceleration (Max Thrust AB)
30,000 30,000 36,000
0
15
30
45
60
75
90
105
120
135
150
165
180
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
Tim
e (
s)
Mach
Acceleration (Max Thrust AB)
0 10,000 20,000
Acceleration Diagram
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : Mirage-III CJ
Engine :SNECMA ATAR-9C
CONFIGURATIONS :
•DRAG INDEX = 20 (2xAIM-9)
•GW=17,353lbs
Sea Level
10,000 ft
30,000 ft
36,000 ft
30,000 ft
A1-DASSAULT AVIATION Mirage-III CJ-NFM-000-r0
I – 1 - 19
20,000 ft
