Page 1
A1-Mc Donnell Douglas F-4E Blk.50-T.O.566 -NFM-000-r1
Mc Donnell Douglas
F-4E Blk.50 - Phantom II
(J79-GE-17) & (T.O.566 - Slated)
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/)
Page 2
Level Flight Envelope
A1-Mc Donnell Douglas F-4E Blk.50-T.O.566 -NFM-000-r1
I – 1 - 2
Page 3
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 : F-4E Blk.50 - T.O.566
Engine :J79-GE-17
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•MILL Power
Aircraft : F-4E Blk.50 - T.O.566
Engine :J79-GE-17
Clean
GW = 39,587 lbs
A1-Mc Donnell Douglas F-4E Blk.50-T.O.566 -NFM-000-r1
I – 1 - 3
4xAIM-7E +
2xAIM-9D + ALQ-71
GW = 42,628 lbs
750 Kts (IAS) from SL to 30,000ft
700Kts over
Clean
GW = 39,587 lbs
4xAIM-7E +
2xAIM-9D + ALQ-71
GW = 42,628 lbs
750 Kts (IAS) from SL to 30,000ft
700Kts over
Page 4
Turn Performance
Aircraft : F-4E Blk.50 - T.O.566
Engine : J79-GE-17
CONFIGURATIONS :
•4xAIM-7E + 2xAIM-9D + ALQ-71
•50% internal fuel
•GW= 42,628 lbs
Load Factor limited to 5.47G
(AIM-9 under LAU-7A/A on station 2)
IAS limited to 750Kts under 25,000ft,
650Kts over 40,000ft
(ALQ-71/QRC-160-1 on station 9)
A1-Mc Donnell Douglas F-4E Blk.50-T.O.566 -NFM-000-r1
I – 1 - 4
Page 5
Turn Rate – Summary
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : F-4E Blk.50 - T.O.566
Engine :J79-GE-17
CONFIGURATIONS :
•4xAIM-7E + 2xAIM-9D + ALQ-71
•GW=42,628 lbs
A1-Mc Donnell Douglas F-4E Blk.50-T.O.566 -NFM-000-r1
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
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
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
Page 6
Load Factor – Summary
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : F-4E Blk.50 - T.O.566
Engine :J79-GE-17
CONFIGURATIONS :
•4xAIM-7E + 2xAIM-9D + ALQ-71
•GW=42,628 lbs
A1-Mc Donnell Douglas F-4E Blk.50-T.O.566 -NFM-000-r1
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
Page 7
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)
Max. Sustained Turn Rate = 14.1 deg/s
+200
0 -200
-600
+400
9G 8G 7G 6G 5G 4G 3G 2G
Turn Performance – Sea Level
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Max. Instantaneous Turn Rate = 18.7 deg/s
MA
XIM
UM
AIR
SP
EE
D
Aircraft : F-4E Blk.50 - T.O.566
Engine :J79-GE-17
CONFIGURATIONS :
•4xAIM-7E + 2xAIM-9D + ALQ-71
•GW=42,628 lbs
-400
A1-Mc Donnell Douglas F-4E Blk.50-T.O.566 -NFM-000-r1
I – 1 - 7
Page 8
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)
+200
0
-200
-400
-600
+400
Turn Performance – 5,000 ft
Max. Instantaneous Turn Rate = 17.2 deg/s
Max. Sustained Turn Rate = 12.7 deg/s
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : F-4E Blk.50 - T.O.566
Engine :J79-GE-17
CONFIGURATIONS :
•4xAIM-7E + 2xAIM-9D + ALQ-71
•GW=42,628 lbs
A1-Mc Donnell Douglas F-4E Blk.50-T.O.566 -NFM-000-r1
I – 1 - 8
MA
XIM
UM
AIR
SP
EE
D
9G 8G 7G 6G 5G 4G 3G 2G
Page 9
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 : F-4E Blk.50 - T.O.566
Engine :J79-GE-17
CONFIGURATIONS :
•4xAIM-7E + 2xAIM-9D + ALQ-71
•GW=42,628 lbs
A1-Mc Donnell Douglas F-4E Blk.50-T.O.566 -NFM-000-r1
I – 1 - 9
+200
0
-200
-400
-600
+400
9G 8G 7G 6G 5G 4G 3G 2G
Max. Sustained Turn Rate = 11.4 deg/s
Max. Instantaneous Turn Rate = 15.9 deg/s
MA
XIM
UM
AIR
SP
EE
D
Page 10
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 : F-4E Blk.50 - T.O.566
Engine :J79-GE-17
CONFIGURATIONS :
•4xAIM-7E + 2xAIM-9D + ALQ-71
•GW=42,628 lbs
A1-Mc Donnell Douglas F-4E Blk.50-T.O.566 -NFM-000-r1
I – 1 - 10
+200
0
-200
-400
-600
9G 8G 7G 6G 5G 4G 3G 2G
Max. Sustained Turn Rate = 10.0 deg/s
+400
Max. Instantaneous Turn Rate = 14.6 deg/s
MA
XIM
UM
AIR
SP
EE
D
Page 11
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 : F-4E Blk.50 - T.O.566
Engine :J79-GE-17
CONFIGURATIONS :
•4xAIM-7E + 2xAIM-9D + ALQ-71
•GW=42,628 lbs
A1-Mc Donnell Douglas F-4E Blk.50-T.O.566 -NFM-000-r1
I – 1 - 11
+200
0
-200
-400
-600
9G 8G 7G 6G 5G 4G 3G 2G
Max. Instantaneous Turn Rate = 13.3 deg/s
Max. Sustained Turn Rate = 8.5 deg/s
MA
XIM
UM
AIR
SP
EE
D
Page 12
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 : F-4E Blk.50 - T.O.566
Engine :J79-GE-17
CONFIGURATIONS :
•4xAIM-7E + 2xAIM-9D + ALQ-71
•GW=42,628 lbs
A1-Mc Donnell Douglas F-4E Blk.50-T.O.566 -NFM-000-r1
I – 1 - 12
+200
0
-200
-400
-600
9G 8G 7G 6G 5G 4G 3G 2G
Max. Instantaneous Turn Rate = 12.2 deg/s
Max. Sustained Turn Rate = 7.5 deg/s
MA
XIM
UM
AIR
SP
EE
D
Page 13
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 : F-4E Blk.50 - T.O.566
Engine :J79-GE-17
CONFIGURATIONS :
•4xAIM-7E + 2xAIM-9D + ALQ-71
•GW=42,628 lbs
A1-Mc Donnell Douglas F-4E Blk.50-T.O.566 -NFM-000-r1
I – 1 - 13
0
-200
9G 8G 7G 6G 5G 4G 3G 2G
Max. Instantaneous Turn Rate = 11.2 deg/s
Max. Sustained Turn Rate = 6.4 deg/s
MA
XIM
UM
AIR
SP
EE
D
-400 -600
+200
Page 14
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 : F-4E Blk.50 - T.O.566
Engine :J79-GE-17
CONFIGURATIONS :
•4xAIM-7E + 2xAIM-9D + ALQ-71
•GW=42,628 lbs
A1-Mc Donnell Douglas F-4E Blk.50-T.O.566 -NFM-000-r1
I – 1 - 14
0
-200
-400
-600
9G 8G 7G 6G 5G 4G 3G 2G
Max. Sustained Turn Rate = 4.5 deg/s
MA
XIM
UM
AIR
SP
EE
D
Max. Instantaneous Turn Rate = 10.2 deg/s
Page 15
Climb Performance
A1-Mc Donnell Douglas F-4E Blk.50-T.O.566 -NFM-000-r1
I – 1 - 15
Aircraft : F-4E Blk.50 - T.O.566
Engine :J79-GE-17
CONFIGURATIONS :
•4xAIM-7E + 2xAIM-9D + ALQ-71
•50% internal fuel
•GW= 42,628 lbs
Page 16
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : F-4E Blk.50 - T.O.566
Engine :J79-GE-17
CONFIGURATIONS :
•4xAIM-7E + 2xAIM-9D + ALQ-71
•GW=42,628 lbs
A1-Mc Donnell Douglas F-4E Blk.50-T.O.566 -NFM-000-r1
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
Page 17
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•MIL Power
Aircraft : F-4E Blk.50 - T.O.566
Engine :J79-GE-17
CONFIGURATIONS :
•4xAIM-7E + 2xAIM-9D + ALQ-71
•GW=42,628 lbs
A1-Mc Donnell Douglas F-4E Blk.50-T.O.566 -NFM-000-r1
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
Page 18
Acceleration Performances
A1-Mc Donnell Douglas F-4E Blk.50-T.O.566 -NFM-000-r1
I – 1 - 18
Aircraft : F-4E Blk.50 - T.O.566
Engine :J79-GE-17
CONFIGURATIONS :
•4xAIM-7E + 2xAIM-9D + ALQ-71
•50% internal fuel
•GW= 42,628 lbs
Page 19
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 : F-4E Blk.50 - T.O.566
Engine :J79-GE-17
CONFIGURATIONS :
•4xAIM-7E + 2xAIM-9D + ALQ-71
•GW=42,628 lbs
Sea Level
30,000 ft
30,000 ft
36,000 ft
A1-Mc Donnell Douglas F-4E Blk.50-T.O.566 -NFM-000-r1
I – 1 - 19
20,000 ft
10,000 ft
Page 20
Turn Performance
Aircraft : F-4E Blk.50 - T.O.566
Engine : J79-GE-17
CONFIGURATIONS :
•4xAIM-7E
•50% internal fuel
•GW= 41,407lbs
A1-Mc Donnell Douglas F-4E Blk.50-T.O.566 -NFM-000-r1
I – 1 - 20
Page 21
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
Turn Rate – Summary
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : F-4E Blk.50 - T.O.566
Engine :J79-GE-17
CONFIGURATIONS :
•4xAIM-7E
•GW=41,407 lbs
A1-Mc Donnell Douglas F-4E Blk.50-T.O.566 -NFM-000-r1
I - 1 - 21
Maximum reached without AoA limit
(Stall speed)
Ng < 7.93 for mach number < 0.72
Ng < 6.06 for mach number > 1.05
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
Page 22
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 : F-4E Blk.50 - T.O.566
Engine :J79-GE-17
CONFIGURATIONS :
•4xAIM-7E
•GW=41,407 lbs
A1-Mc Donnell Douglas F-4E Blk.50-T.O.566 -NFM-000-r1
I - 1 - 22
Maximum reached without AoA limit
(Stall speed)
Ng < 7.93 for mach number < 0.72
Ng < 6.06 for mach number > 1.05
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
Page 23
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)
Max. Sustained Turn Rate = 14.9 deg/s
+200
0
-200
-600
+400
9G 8G 7G 6G 5G 4G 3G 2G
Turn Performance – Sea Level
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Max. Instantaneous Turn Rate = 22.6 deg/s
MA
XIM
UM
AIR
SP
EE
D
Aircraft : F-4E Blk.50 - T.O.566
Engine :J79-GE-17
CONFIGURATIONS :
•4xAIM-7E
•GW=41,407 lbs
-400
A1-Mc Donnell Douglas F-4E Blk.50-T.O.566 -NFM-000-r1
I – 1 - 23
+600
Page 24
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)
+200
0
-200
-400
-600
+400
Turn Performance – 5,000 ft
Max. Instantaneous Turn Rate = 20.9 deg/s
Max. Sustained Turn Rate = 13.3 deg/s
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : F-4E Blk.50 - T.O.566
Engine :J79-GE-17
CONFIGURATIONS :
•4xAIM-7E
•GW=41,407 lbs
A1-Mc Donnell Douglas F-4E Blk.50-T.O.566 -NFM-000-r1
I – 1 - 24
MA
XIM
UM
AIR
SP
EE
D
9G 8G 7G 6G 5G 4G 3G 2G
Page 25
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 : F-4E Blk.50 - T.O.566
Engine :J79-GE-17
CONFIGURATIONS :
•4xAIM-7E
•GW=41,407 lbs
A1-Mc Donnell Douglas F-4E Blk.50-T.O.566 -NFM-000-r1
I – 1 - 25
+200
0
-200
-400
-600
+400
9G 8G 7G 6G 5G 4G 3G 2G
Max. Sustained Turn Rate = 12.0 deg/s
Max. Instantaneous Turn Rate = 19.2 deg/s
MA
XIM
UM
AIR
SP
EE
D
Page 26
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 : F-4E Blk.50 - T.O.566
Engine :J79-GE-17
CONFIGURATIONS :
•4xAIM-7E
•GW=41,407 lbs
A1-Mc Donnell Douglas F-4E Blk.50-T.O.566 -NFM-000-r1
I – 1 - 26
+200
0
-200
-400
-600
9G 8G 7G 6G 5G 4G 3G 2G
Max. Sustained Turn Rate = 10.4
deg/s
+400
Max. Instantaneous Turn Rate = 17.5 deg/s
MA
XIM
UM
AIR
SP
EE
D
Page 27
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 : F-4E Blk.50 - T.O.566
Engine :J79-GE-17
CONFIGURATIONS :
•4xAIM-7E
•GW=41,407 lbs
A1-Mc Donnell Douglas F-4E Blk.50-T.O.566 -NFM-000-r1
I – 1 - 27
+200
0
-200
-400
-600
9G 8G 7G 6G 5G 4G 3G 2G
Max. Instantaneous Turn Rate = 15.8 deg/s
Max. Sustained Turn Rate = 8.9 deg/s
MA
XIM
UM
AIR
SP
EE
D
+400
Page 28
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 : F-4E Blk.50 - T.O.566
Engine :J79-GE-17
CONFIGURATIONS :
•4xAIM-7E
•GW=41,407 lbs
A1-Mc Donnell Douglas F-4E Blk.50-T.O.566 -NFM-000-r1
I – 1 - 28
+200
0
-200
-400
-600
9G 8G 7G 6G 5G 4G 3G 2G
Max. Instantaneous Turn Rate = 14.1 deg/s
Max. Sustained Turn Rate = 7.8 deg/s
MA
XIM
UM
AIR
SP
EE
D
Page 29
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 : F-4E Blk.50 - T.O.566
Engine :J79-GE-17
CONFIGURATIONS :
•4xAIM-7E
•GW=41,407 lbs
A1-Mc Donnell Douglas F-4E Blk.50-T.O.566 -NFM-000-r1
I – 1 - 29
0
-200
9G 8G 7G 6G 5G 4G 3G 2G
Max. Instantaneous Turn Rate = 11.5 deg/s
Max. Sustained Turn Rate = 6.6 deg/s
MA
XIM
UM
AIR
SP
EE
D
-400 -600
+200
Page 30
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 : F-4E Blk.50 - T.O.566
Engine :J79-GE-17
CONFIGURATIONS :
•4xAIM-7E
•GW=41,407 lbs
A1-Mc Donnell Douglas F-4E Blk.50-T.O.566 -NFM-000-r1
I – 1 - 30
0
-200
-400
-600
9G 8G 7G 6G 5G 4G 3G 2G
Max. Sustained Turn Rate = 4.7 deg/s
+200
MA
XIM
UM
AIR
SP
EE
D
Max. Instantaneous Turn Rate = 10.9 deg/s
Page 31
Climb Performance
A1-Mc Donnell Douglas F-4E Blk.50-T.O.566 -NFM-000-r1
I – 1 - 31
Aircraft : F-4E Blk.50 - T.O.566
Engine : J79-GE-17
CONFIGURATIONS :
•4xAIM-7E
•50% internal fuel
•GW= 41,407 lbs
Page 32
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : F-4E Blk.50 - T.O.566
Engine :J79-GE-17
CONFIGURATIONS :
•4xAIM-7E
•GW=41,407 lbs
A1-Mc Donnell Douglas F-4E Blk.50-T.O.566 -NFM-000-r1
I - 1 - 32
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
Page 33
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•MIL Power
Aircraft : F-4E Blk.50 - T.O.566
Engine :J79-GE-17
CONFIGURATIONS :
•4xAIM-7E
•GW=41,407 lbs
A1-Mc Donnell Douglas F-4E Blk.50-T.O.566 -NFM-000-r1
I - 1 - 33
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
Page 34
Acceleration Performances
A1-Mc Donnell Douglas F-4E Blk.50-T.O.566 -NFM-000-r1
I – 1 - 34
Aircraft : F-4E Blk.50 - T.O.566
Engine : J79-GE-17
CONFIGURATIONS :
•4xAIM-7E
•50% internal fuel
•GW= 41,407 lbs
Page 35
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 : F-4E Blk.50 - T.O.566
Engine :J79-GE-17
CONFIGURATIONS :
•4xAIM-7E
•GW=41,407 lbs
Sea Level
30,000 ft
30,000 ft
36,000 ft
A1-Mc Donnell Douglas F-4E Blk.50-T.O.566 -NFM-000-r1
I – 1 - 35
20,000 ft
10,000 ft
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