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McDonnell F-4 Phantom II

McDonnell F-4F © Karsten Palt
Photo ©: Karsten Palt

F-4 Phantom II

Fighter / Fighter Bomber

The McDonnell F-4 Phantom II is a twin-engined two-seat jet fighter and fighter bomber aircraft produced by the US-American manufacturer McDonnell Aircraft Corporation, later McDonnell Douglas Corporation.

Crew2
 
Propulsion2 Turbojet Engines
Engine ModelGeneral Electric J79-GE-17
Engine Power (each)
dry/with Afterburner
52,8 / 79,6 kN11870 lbf
 
Speed2389 km/h1290 kts
  1485 mph
Service Ceiling18.288 m60.000 ft
Range1.300 km702 NM
808 mi.
 
Empty Weight13.770 kg30.358 lbs
max. Takeoff Weight27.965 kg61.652 lbs
 
Wing Span11,68 m38,3 ft
Wing Area49,2 m²530 ft²
Length19,20 m63,0 ft
Height5,03 m16,5 ft
 
First Flight27.08.1958
Production Statusout of production
Production Range1958-1979
Total Production5197
 
Data for (Version)McDonnell F-4E
VariantsF-4A, F-4B, F-4C, F-4D, F-4E, F-4EJ, F-4F, F-4G Wild Weasel V, F-4J, F-4K, F-4M, F-4N, F-4S, RF-4B, RF-4C, RF-4E

Remarks
The F-4 Phantom II was also operated from aircraft carriers. It was also licence-built by Mitsubishi in Japan (138 aircraft).


WeblinksExtras
The Boeing Company, official website

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