Start | McDonnell Douglas | F-4A (F4H-1F) Phantom II

McDonnell Douglas F-4A


General information


ManufacturerMcDonnell Douglas
ModelF-4A (F4H-1F) Phantom II
ModificationF-4A
CountryUSA
Years1958
TypeFighter
Main rotor diameter-
Tail rotor diameter-
Wingspan11,2 m
Length17,68 m
Height4,95 m
Wing area49,20 m2
Zero fuel weight-
Empty weight13760 kg
Maximum takeoff weight26308 kg
Normal takeoff weight-
Flight duration-
Engine2 ТРДФ General Electric J79-GE-2, -2A
Power-
Thrust-
Maximum speed2390 km/h
Cruising speed-
Rate of climb-
Practical range2590 km
Service ceiling18700 m
Hovering ceiling-
Crew-