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A1-Mc Donnell Douglas F-4D Blk.37-NFM-000-r1
Mc Donnell Douglas
F-4D Blk.37 Phantom II
(J79-GE-15)
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/)
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Level Flight Envelope
A1-Mc Donnell Douglas F-4D Blk.37-NFM-000-r1
I – 1 - 2
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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
A l t ( f t )
Mach
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
A l t ( f t )
Mach
Level Flight Envelope
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : F-4D Blk.37
Engine :J79-GE-15
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•MILL Power
Aircraft : F-4D Blk.37
Engine :J79-GE-15
Clean
GW = 36,135 lbs
A1-Mc Donnell Douglas F-4D Blk.37-NFM-000-r1
I – 1 - 3
4xAIM-7E +
SUU-23
GW = 39,816 lbs
750 Kts (IAS) from SL to 30,000ft
700Kts over
Clean
GW = 36,135 lbs
4xAIM-7E +
SUU-23GW = 39,816 lbs
750 Kts (IAS) from SL to 30,000ft
700Kts over
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Turn Performance
Aircraft : F-4D Blk.37
Engine : J79-GE-15
CONFIGURATIONS :
•4xAIM-7E + SUU-23/A
•50% internal fuel
•GW= 39,816 lbs
A1-Mc Donnell Douglas F-4D Blk.37-NFM-000-r1
I – 1 - 4
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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
M a x i m u m i n
s t a n t a n e o u s
t u r n r a t e ( d e g / 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-4D Blk.37
Engine :J79-GE-15
CONFIGURATIONS :
•4xAIM-7E + SUU-23/A
•GW=39,816 lbs
A1-Mc Donnell Douglas F-4D Blk.37-NFM-000-r1
I - 1 - 5
Maximum reached without AoA limit
(Stall speed)
Ng < 8.16 for mach number < 0.72Ng < 6.24 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
S u s t a i n e d T u r n r a t e ( d e g / s )
Mach number
Maximum Sustained Turn rate (deg/s)
0
10,000
20,000
30,000
40,000
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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
M a x i m u m A
v a i l a b l e L
o a d F a c t o 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-4D Blk.37
Engine :J79-GE-15
CONFIGURATIONS :
•4xAIM-7E + SUU-23/A
•GW=39,816 lbs
A1-Mc Donnell Douglas F-4D Blk.37-NFM-000-r1
I - 1 - 6
Maximum reached without AoA limit
(Stall speed)
Ng < 8.16 for mach number < 0.72
Ng < 6.24 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
S u s t a i n e d L o a d F a c t o r ( N g )
Mach number
Maximum Sustained Load Factor (Ng)
0
10,000
20,000
30,000
40,000
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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
T u r n R a t e
( d e g r e e
p e r s e c
o n d )
CAS (Kts)
Max. Sustained Turn = 13.7 deg/s
+200
0
-200
-600
+400
9G8G7G6G5G4G3G2G
Turn Performance – Sea Level
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Max. Instantaneous Turn Rate = 21.6 deg/s
MAX I M UM AI R
S P E E D
Aircraft : F-4D Blk.37
Engine :J79-GE-15
CONFIGURATIONS :
•4xAIM-7E + SUU-23/A
•GW=39,816 lbs
-400
A1-Mc Donnell Douglas F-4D Blk.37-NFM-000-r1
I – 1 - 7
+600
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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
T u r n R a t e
( d e g r e e
p e r s e c
o n d )
CAS (Kts)
+200
0
-200
-400-600
+400
Turn Performance – 5,000 ft
Max. Instantaneous Turn Rate = 19.9 deg/s
Max. Sustained Turn = 12.0 deg/s
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : F-4D Blk.37
Engine :J79-GE-15
CONFIGURATIONS :
•4xAIM-7E + SUU-23/A
•GW=39,816 lbs
A1-Mc Donnell Douglas F-4D Blk.37-NFM-000-r1
I – 1 - 8
MAX I M UM AI R
S P E E D
9G8G7G6G5G4G3G2G
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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
T u r n R a t e
( d e g r e e
p e r s e c
o n d )
CAS (Kts)
Turn Performance – 10,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : F-4D Blk.37
Engine :J79-GE-15
CONFIGURATIONS :
•4xAIM-7E + SUU-23/A
•GW=39,816 lbs
A1-Mc Donnell Douglas F-4D Blk.37-NFM-000-r1
I – 1 - 9
+200
0
-200
-400-600
+400
9G8G7G6G5G4G3G2G
Max. Sustained Turn = 10.3 deg/s
Max. Instantaneous Turn Rate = 18.1 deg/s
MAX I M UM AI R
S P E E D
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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
T u r n R a t e
( d e g r e e
p e r s e c
o n d )
CAS (Kts)
Turn Performance – 15,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : F-4D Blk.37
Engine :J79-GE-15
CONFIGURATIONS :
•4xAIM-7E + SUU-23/A
•GW=39,816 lbs
A1-Mc Donnell Douglas F-4D Blk.37-NFM-000-r1
I – 1 - 10
+200
0
-200
-400
-600
9G8G7G6G5G4G3G2G
Max. Sustained Turn = 8.8 deg/s
+400
Max. Instantaneous Turn Rate = 16.3 deg/s
MAX I M UM AI R
S P E E
D
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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
T u r n R a t e
( d e g r e e
p e r s e c
o n d )
CAS (Kts)
Turn Performance – 20,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : F-4D Blk.37
Engine :J79-GE-15
CONFIGURATIONS :
•4xAIM-7E + SUU-23/A
•GW=39,816 lbs
A1-Mc Donnell Douglas F-4D Blk.37-NFM-000-r1
I – 1 - 11
+200
0
-200
-400
-600
9G8G7G6G5G4G3G2G
Max. Instantaneous Turn Rate = 14.6 deg/s
Max. Sustained Turn = 7.4 deg/s
MAX I M UM AI R
S P E E D
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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
T u r n R a t e
( d e g r e e
p e r s e c
o n d )
CAS (Kts)
Turn Performance – 25,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : F-4D Blk.37
Engine :J79-GE-15
CONFIGURATIONS :
•4xAIM-7E + SUU-23/A
•GW=39,816 lbs
A1-Mc Donnell Douglas F-4D Blk.37-NFM-000-r1
I – 1 - 12
+200
0-200
-400
-600
9G8G7G6G5G4G3G2G
Max. Instantaneous Turn Rate = 13.1 deg/s
Max. Sustained Turn = 6.2 deg/s MAX I M UM AI R
S P E E
D
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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
T u r n R a t e
( d e g r e e
p e r s e c
o n d )
CAS (Kts)
Turn Performance – 30,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : F-4D Blk.37
Engine :J79-GE-15
CONFIGURATIONS :
•4xAIM-7E + SUU-23/A
•GW=39,816 lbs
A1-Mc Donnell Douglas F-4D Blk.37-NFM-000-r1
I – 1 - 13
+200
0 -200
9G8G7G6G5G4G3G2G
Max. Instantaneous Turn Rate = 11.5 deg/s
Max. Sustained Turn = 5.2 deg/sMAX I M UM AI R
S P E E D
-400-600
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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
T u r n R a t e
( d e g r e e
p e r s e c
o n d )
CAS (Kts)
Turn Performance – 35,000 ft
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : F-4D Blk.37
Engine :J79-GE-15
CONFIGURATIONS :
•4xAIM-7E + SUU-23/A
•GW=39,816 lbs
A1-Mc Donnell Douglas F-4D Blk.37-NFM-000-r1
I – 1 - 14
0
-200
-400
-600
9G8G7G6G5G4G3G2G
Max. Sustained Turn = 3.8 deg/s
+200
MAX I M UM AI R
S P E E D
Max. Instantaneous Turn Rate = 10.3 deg/s
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Climb Performance
A1-Mc Donnell Douglas F-4D Blk.37-NFM-000-r1
I – 1 - 15
Aircraft : F-4D Blk.37
Engine :J79-GE-15
CONFIGURATIONS :
•
4xAIM-7E + SUU-23/A•50% internal fuel
•GW= 39,816 lbs
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DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : F-4D Blk.37
Engine :J79-GE-15
CONFIGURATIONS :
•4xAIM-7E + SUU-23/A
•GW=39,816 lbs
A1-Mc Donnell Douglas F-4D Blk.37-NFM-000-r1
I - 1 - 16
0
50
100
150
200
250
300
350
400
450
500
550
600
650
700
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
E x c e s s S p e c i f i c P o
w e r ( f t / 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
C l i m b A n g l e ( d e g )
Mach
Constant Speed Climb Angle
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
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DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•MIL Power
Aircraft : F-4D Blk.37
Engine :J79-GE-15
CONFIGURATIONS :
•4xAIM-7E + SUU-23/A
•GW=39,816 lbs
A1-Mc Donnell Douglas F-4D Blk.37-NFM-000-r1
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
E x c e s s S p e c i f i c P o
w e r ( f t / 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
C l i m b A n g l e ( d e g )
Mach
Constant Speed Climb Angle
0
5,000
10,000
15,000
20,000
25,000
30,000
35,000
40,000
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Acceleration Performances
A1-Mc Donnell Douglas F-4D Blk.37-NFM-000-r1
I – 1 - 18
Aircraft : F-4D Blk.37
Engine :J79-GE-15
CONFIGURATIONS :
•4xAIM-7E + SUU-23/A
•50% internal fuel•GW= 39,816 lbs
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0
15
30
45
60
75
90
105
120
135
150
165
180
Time(s)
Acceleration (Max Thrust AB)
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
Time(s)
Mach
Acceleration (Max Thrust AB)
Acceleration Diagram
DATA BASIS : ESTIMATED
CONDITIONS:
•Standard Day
•Max AB
Aircraft : F-4D Blk.37
Engine :J79-GE-15
CONFIGURATIONS :
•4xAIM-7E + SUU-23/A
•GW=39,816 lbs
Sea Level
30,000 ft
30,000 ft
36,000 ft
A1-Mc Donnell Douglas F-4D Blk.37-NFM-000-r1
20,000 ft
10,000 ft
