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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. 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
- Successors 1 airplane(s)
- Created On Windows
- Wingspan 27.5ft (8.4m)
- Length 35.8ft (10.9m)
- Height 9.8ft (3.0m)
- Empty Weight 12,896lbs (5,849kg)
- Loaded Weight 17,672lbs (8,016kg)
Performance
- Power/Weight Ratio 4.577
- Wing Loading 106.0lbs/ft2 (517.3kg/m2)
- Wing Area 166.8ft2 (15.5m2)
- Drag Points 4800
Parts
- Number of Parts 99
- Control Surfaces 8
- Performance Cost 527
why is German it's usa BTW it looks good
@KnightPerformance they handle like boats