The McDonnell Douglas F-4 Phantom II is a two-seat, twin-engine, all-weather, long-range supersonic jet interceptor aircraft/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 respective air wings. This is the clean version (no ordinance or pylons).
Specifications
General Characteristics
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- Wingspan 24.3ft (7.4m)
- Length 24.3ft (7.4m)
- Height 9.7ft (3.0m)
- Empty Weight 6,437lbs (2,920kg)
- Loaded Weight 14,171lbs (6,428kg)
Performance
- Power/Weight Ratio 1.585
- Wing Loading 88.6lbs/ft2 (432.4kg/m2)
- Wing Area 160.0ft2 (14.9m2)
- Drag Points 1565
Parts
- Number of Parts 47
- Control Surfaces 7
- Performance Cost 232
