Manufacturer | McDonnell Douglas |
Model | F-4B (F4H-1) Phantom II |
Modification | F-4B |
Country | USA |
Years | 1961 |
Type | Fighter |
Main rotor diameter | - |
Tail rotor diameter | - |
Wingspan | 11,70 m |
Length | 17,78 m |
Height | 4,95 m |
Wing area | 49,23 m2 |
Zero fuel weight | - |
Empty weight | 12701 kg |
Maximum takeoff weight | 20231 kg |
Normal takeoff weight | - |
Flight duration | - |
Engine | 2 ТРДФ General Electric J79-GE-8 |
Power | - |
Thrust | - |
Maximum speed | 2390 km/h |
Cruising speed | - |
Rate of climb | - |
Practical range | - |
Service ceiling | 18898 m |
Hovering ceiling | - |
Crew | - |