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A1-DASSAULT AVIATION Mirage-5F-NFM-000-r0
Mirage-5F / Nesher
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-5F-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-5F
Engine :SNECMA ATAR-9C
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•MILL Power
Aircraft : Mirage-5F
Engine :SNECMA ATAR-9C
A1-DASSAULT AVIATION Mirage-5F-NFM-000-r0
I – 1 - 3
Clean A/C
GW = 18,238 lbs
2 x AIM-9
GW = 18,724 lbs
IAS < 750 Kts SL-30,000ft
IAS < 700 Kts over 30,000ft
Mach number < 2.00
Clean A/C
GW = 18,238 lbs
2 x AIM-9
GW = 18,724 lbs
IAS < 750 Kts SL-30,000ft
IAS < 700 Kts over 30,000ft
Mach number < 2.00
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
A1-DASSAULT AVIATION Mirage-5F-NFM-000-r0
I – 1 - 4
Turn Rate – Summary
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : Mirage-5F
Engine :SNECMA ATAR-9C
CONFIGURATIONS :
•DRAG INDEX = 20 (2xAIM-9)
•GW=18,724lbs
A1-DASSAULT AVIATION Mirage-5F-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
Limitation by Maximum Lift,
not ADHEMAR red only
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
Load Factor – Summary
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : Mirage-5F
Engine :SNECMA ATAR-9C
CONFIGURATIONS :
•DRAG INDEX = 20 (2xAIM-9)
•GW=18,724lbs
A1-DASSAULT AVIATION Mirage-5F-NFM-000-r0
I - 1 - 6
Limitation by Maximum Lift,
not ADHEMAR red only
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-5F
Engine :SNECMA ATAR-9C
CONFIGURATIONS :
•DRAG INDEX = 20 (2xAIM-9)
•GW=18,724lbs
A1-DASSAULT AVIATION Mirage-5F-NFM-000-r0
I – 1 - 7
Max. Sustained Turn = 13.7 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 = 21.0 deg/s
Lim
ita
tio
n b
y M
axim
um
Lift,
no
t A
DH
EM
AR
re
d o
nly
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-5F
Engine :SNECMA ATAR-9C
CONFIGURATIONS :
•DRAG INDEX = 20 (2xAIM-9)
•GW=18,724lbs
A1-DASSAULT AVIATION Mirage-5F-NFM-000-r0
I – 1 - 8
+150
0
-150
-300
-450
+300
9G 8G 7G 6G 5G 4G 3G 2G
Quickest Turn = 19.5 deg/s
Max. Sustained Turn = 11.9 deg/s
MA
XIM
UM
AIR
SP
EE
D
+450
Lim
ita
tio
n b
y M
axim
um
Lift,
no
t A
DH
EM
AR
re
d o
nly
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-5F
Engine :SNECMA ATAR-9C
CONFIGURATIONS :
•DRAG INDEX = 20 (2xAIM-9)
•GW=18,724lbs
A1-DASSAULT AVIATION Mirage-5F-NFM-000-r0
I – 1 - 9
+150
0
-150
-300
-450
+300
9G 8G 7G 6G 5G 4G 3G 2G
Max. Sustained Turn = 10.2 deg/s
MA
XIM
UM
AIR
SP
EE
D
Quickest Turn = 18.0 deg/s
Lim
ita
tio
n b
y M
axim
um
Lift,
no
t A
DH
EM
AR
re
d o
nly
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-5F
Engine :SNECMA ATAR-9C
CONFIGURATIONS :
•DRAG INDEX = 20 (2xAIM-9)
•GW=18,724lbs
A1-DASSAULT AVIATION Mirage-5F-NFM-000-r0
I – 1 - 10
+150
0
-150
-300
-450
9G 8G 7G 6G 5G 4G 3G 2G
Max. Sustained Turn = 8.6 deg/s
MA
XIM
UM
AIR
SP
EE
D
+300
Quickest Turn = 16.3 deg/s
Lim
ita
tio
n b
y M
axim
um
Lift,
no
t A
DH
EM
AR
re
d o
nly
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-5F
Engine :SNECMA ATAR-9C
CONFIGURATIONS :
•DRAG INDEX = 20 (2xAIM-9)
•GW=18,724lbs
A1-DASSAULT AVIATION Mirage-5F-NFM-000-r0
I – 1 - 11
+150
0
-150
-300
-450
9G 8G 7G 6G 5G 4G 3G 2G
Quickest Turn = 14.8 deg/s
Max. Sustained Turn = 7.1 deg/s
MA
XIM
UM
AIR
SP
EE
D
Lim
ita
tio
n b
y M
axim
um
Lift,
no
t A
DH
EM
AR
re
d o
nly
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-5F
Engine :SNECMA ATAR-9C
CONFIGURATIONS :
•DRAG INDEX = 20 (2xAIM-9)
•GW=18,724lbs
A1-DASSAULT AVIATION Mirage-5F-NFM-000-r0
I – 1 - 12
+150
0
-150
-300
-450
9G 8G 7G 6G 5G 4G 3G 2G
Quickest Turn = 14.0 deg/s
Max. Sustained Turn = 6.0 deg/s
MA
XIM
UM
AIR
SP
EE
D
Lim
ita
tio
n b
y M
axim
um
Lift,
no
t A
DH
EM
AR
re
d o
nly
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-5F
Engine :SNECMA ATAR-9C
CONFIGURATIONS :
•DRAG INDEX = 20 (2xAIM-9)
•GW=18,724lbs
A1-DASSAULT AVIATION Mirage-5F-NFM-000-r0
I – 1 - 13
+150
0
-150
-300
-450
9G 8G 7G 6G 5G 4G 3G 2G
Max. Sustained Turn = 4.9 deg/s MA
XIM
UM
AIR
SP
EE
D
Quickest Turn = 13.2 deg/s
Lim
ita
tio
n b
y M
axim
um
Lift,
no
t A
DH
EM
AR
re
d o
nly
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-5F
Engine :SNECMA ATAR-9C
CONFIGURATIONS :
•DRAG INDEX = 20 (2xAIM-9)
•GW=18,724lbs
A1-DASSAULT AVIATION Mirage-5F-NFM-000-r0
I – 1 - 14
0
-150
-300
-450
9G 8G 7G 6G 5G 4G 3G 2G
Max. Sustained Turn = 4.1 deg/s
MA
XIM
UM
AIR
SP
EE
D
Quickest Turn = 12.3 deg/s
Lim
ita
tio
n b
y M
axim
um
Lift,
no
t A
DH
EM
AR
re
d o
nly
+150
Climb Performance
A1-DASSAULT AVIATION Mirage-5F-NFM-000-r0
I – 1 - 15
Aircraft : Mirage-5F
Engine :SNECMA ATAR-9C
CONFIGURATIONS :
•DRAG INDEX = 20 (2xAIM-9)
•50% internal fuel
•GW= 18,724 lbs / 8,482 Kg
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : Mirage-5F
Engine :SNECMA ATAR-9C
CONFIGURATIONS :
•DRAG INDEX = 20 (2xAIM-9)
•GW=18,724lbs
A1-DASSAULT AVIATION Mirage-5F-NFM-000-r0
I - 1 - 16
0
50
100
150
200
250
300
350
400
450
500
550
600
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-5F
Engine :SNECMA ATAR-9C
CONFIGURATIONS :
•DRAG INDEX = 20 (2xAIM-9)
•GW=18,724lbs
A1-DASSAULT AVIATION Mirage-5F-NFM-000-r0
I - 1 - 17
0
50
100
150
200
250
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-5F-NFM-000-r0
I – 1 - 18
Aircraft : Mirage-5F
Engine :SNECMA ATAR-9C
CONFIGURATIONS :
•DRAG INDEX = 20 (2xAIM-9)
•50% internal fuel
•GW= 18,724 lbs / 8,482 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
Tim
e (
s)
Mach
Acceleration (Max Thrust AB)
0 10,000 20,000
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 1.80 1.90 2.00 2.10 2.20
Tim
e (
s)
Mach
Acceleration (Max Thrust AB)
30,000 30,000 36,000
Acceleration Diagram
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : Mirage-5F
Engine :SNECMA ATAR-9C
CONFIGURATIONS :
•DRAG INDEX = 20 (2xAIM-9)
•GW=18,724lbs
Sea Level
10,000 ft
30,000 ft
36,000 ft
30,000 ft
A1-DASSAULT AVIATION Mirage-5F-NFM-000-r0
I – 1 - 19
20,000 ft
