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The McDonnell Douglas F-4 Phantom II[N 1] 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.[1] 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.
Specifications
General Characteristics
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- Wingspan 33.2ft (10.1m)
- Length 36.9ft (11.3m)
- Height 11.4ft (3.5m)
- Empty Weight 7,145lbs (3,240kg)
- Loaded Weight 15,415lbs (6,992kg)
Performance
- Power/Weight Ratio 1.457
- Wing Loading 45.4lbs/ft2 (221.8kg/m2)
- Wing Area 339.3ft2 (31.5m2)
- Drag Points 5094
Parts
- Number of Parts 100
- Control Surfaces 7
- Performance Cost 377
