First entering service in 1960, the McDonnel Douglas F-4 Phantom II is a two-seat, twin engine supersonic interceptor/bomber developed by the United States. With most deployed during the Vietnam War, the F-4 was eventually retired by the U.S. in 1996, and by the U.K. in 1992.
Specifications
Spotlights
- YTho 7.7 years ago
General Characteristics
- Created On Windows
- Wingspan 34.6ft (10.6m)
- Length 38.3ft (11.7m)
- Height 12.2ft (3.7m)
- Empty Weight 13,766lbs (6,244kg)
- Loaded Weight 23,260lbs (10,550kg)
Performance
- Power/Weight Ratio 2.898
- Wing Loading 101.3lbs/ft2 (494.8kg/m2)
- Wing Area 229.5ft2 (21.3m2)
- Drag Points 2972
Parts
- Number of Parts 69
- Control Surfaces 5
- Performance Cost 444
