MCDONNELL DOUGLAS F-4 Phantom

Aircraft
Name: 
F-4 Phantom
Manufacturer: 
Body: 
Narrow
Wing: 
Fixed Wing
Position: 
Low wing
Tail: 
Regular tail (Anhedral)
WTC
M
APC
E
Type Code: 
L2J
Engine: 
Jet
Engine Count: 
Multi
Position: 
In fuselage
Landing gear: 
Tricycle retractable
Manufacturered as
MCDONNELL DOUGLAS F-4 Kurnass
MCDONNELL DOUGLAS F-4 Phantom 2
MCDONNELL DOUGLAS Kurnass
MCDONNELL DOUGLAS Phantom 2
MCDONNELL DOUGLAS QF-4 Phantom 2
MCDONNELL DOUGLAS RF-4 Kurnass
MCDONNELL DOUGLAS RF-4 Phantom 2
IAI F-4 Kurnass 2000
IAI F-4 Phantom 2000
IAI Kurnass 2000
IAI Phantom 2000
MCDONNELL C-12 Phantom 2
MCDONNELL CR-12 Phantom 2
MCDONNELL F-4 Phantom 2
MCDONNELL Phantom 2
MCDONNELL RF-4 Phantom 2
MITSUBISHI F-4 Phantom 2
MITSUBISHI Phantom 2
MITSUBISHI RF-4 Phantom 2

F4

Multi role fighter/tactical reconnaissance aircraft. In service since 1965 (F-4E since 1966, RF-4C since 1964). Developed in many versions, used by German, Greek, Spanish, Turkish and Middle East Air Forces.

Technical Data
Wing span: 
11.70 m
Length: 
17.80 m
Height: 
5.10 m
Powerplant: 

Variants:

Engine Model: 
General Electric J79, Rolls-Royce Spey
Indicative Performance Data
Take-Off
V2: 
150 kts
Distance: 
1500 m
MTOW: 
28000 kg
Initial Climb (to 5000 ft)
IAS: 
180 kts
ROC: 
4000 ft/min
Initial Climb (to FL150)
IAS: 
300 kts
ROC: 
7000
Initial Climb (to FL240)
IAS: 
300 kts
ROC: 
5000 ft/min
MACH Climb
MACH: 
0.80
ROC: 
3000 ft/min
Cruise
TAS: 
480 kts
MACH: 
0.86
Ceiling: 
590
Range: 
1200 NM
Initial Descent (to FL240)
MACH: 
0.85
ROD: 
10000 ft/min
Descent (to FL100)
IAS: 
350 kts
ROD: 
10000 ft/min
Descent (FL100 & below)
IAS: 
n/a
MCS: 
n/a
ROD: 
n/a
Approach
Vapp (IAS): 
175 kts
Distance: 
915 m

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