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 for the United States Navy by McDonnell Aircraft. It first entered service in 1960 with the U.S. Navy. Proving highly adaptable, it was also adopted by the U.S. Marine Corps and the U.S. Air Force, and by the mid-1960s had become a major part of their air arms.
Specifications
General Characteristics
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- Wingspan 36.5ft (11.1m)
- Length 40.6ft (12.4m)
- Height 15.0ft (4.6m)
- Empty Weight 15,140lbs (6,867kg)
- Loaded Weight 22,969lbs (10,418kg)
Performance
- Power/Weight Ratio 2.935
- Wing Loading 69.9lbs/ft2 (341.1kg/m2)
- Wing Area 328.8ft2 (30.5m2)
- Drag Points 3815
Parts
- Number of Parts 67
- Control Surfaces 5
- Performance Cost 433
