McDonnell Douglas F-4 Phantom II Fighter-bomber The McDonnell Douglas F-4 Phantom II is a tandem two-seat, twin-engine, all-weather, long-range supersonic jet interceptor and fighter-bomber originally developed by McDonnell Aircraft for the United States Navy. Wikipedia Top speed: 2300 (mine can only go 1000) km/h Introduced: December 30, 1960 Range: 2,816 km Length: 19 m Engine type: General Electric J79 First flight: May 27, 1958 Manufacturers: McDonnell Douglas, McDonnell
Specifications
General Characteristics
- Created On Windows
- Wingspan 36.2ft (11.0m)
- Length 57.6ft (17.5m)
- Height 17.6ft (5.4m)
- Empty Weight 16,119lbs (7,311kg)
- Loaded Weight 24,334lbs (11,037kg)
Performance
- Power/Weight Ratio 2.77
- Wing Loading 61.1lbs/ft2 (298.2kg/m2)
- Wing Area 398.5ft2 (37.0m2)
- Drag Points 4643
Parts
- Number of Parts 63
- Control Surfaces 5
- Performance Cost 464
