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The McDonnell Douglas F-4 Phantom II is a tandem two-seat, twin-engine, all-weather, long-range supersonic jet interceptor aircraft/fighter-bomber originally developed for the United States Navy by McDonnell Aircraft.
Specifications
General Characteristics
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- Wingspan 36.3ft (11.1m)
- Length 48.9ft (14.9m)
- Height 13.8ft (4.2m)
- Empty Weight 13,503lbs (6,125kg)
- Loaded Weight 31,344lbs (14,217kg)
Performance
- Power/Weight Ratio 2.15
- Wing Loading 83.1lbs/ft2 (406.0kg/m2)
- Wing Area 377.0ft2 (35.0m2)
- Drag Points 3906
Parts
- Number of Parts 74
- Control Surfaces 5
- Performance Cost 470
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