Manufacturer | McDonnell Douglas |
Model | F-4A (F4H-1F) Phantom II |
Modification | F-4A |
Country | USA |
Years | 1958 |
Type | Fighter |
Main rotor diameter | - |
Tail rotor diameter | - |
Wingspan | 11,2 m |
Length | 17,68 m |
Height | 4,95 m |
Wing area | 49,20 m2 |
Zero fuel weight | - |
Empty weight | 13760 kg |
Maximum takeoff weight | 26308 kg |
Normal takeoff weight | - |
Flight duration | - |
Engine | 2 ТРДФ General Electric J79-GE-2, -2A |
Power | - |
Thrust | - |
Maximum speed | 2390 km/h |
Cruising speed | - |
Rate of climb | - |
Practical range | 2590 km |
Service ceiling | 18700 m |
Hovering ceiling | - |
Crew | - |