[PEA] McDonnell Douglas F-4 Phantom II
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The McDonnell Douglas F-4 Phantom II[N 1] is an American tandem two-seat, twin-engine, all-weather, long-range supersonic jet interceptor and fighter-bomber originally developed by McDonnell Aircraft for the United States Navy.[2] Proving highly adaptable, it entered service with the Navy in 1961[3] before it was adopted by the United States Marine Corps and the United States Air Force, and by the mid-1960s it had become a major part of their air arms.[4] Phantom production ran from 1958 to 1981 with a total of 5,195 aircraft built, making it the most produced American supersonic military aircraft in history, and cementing its position as a signature combat aircraft of the Cold War.[4][5]
Specifications
General Characteristics
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- Wingspan 41.1ft (12.5m)
- Length 52.4ft (16.0m)
- Height 13.7ft (4.2m)
- Empty Weight 16,897lbs (7,664kg)
- Loaded Weight 21,342lbs (9,680kg)
Performance
- Power/Weight Ratio 3.158
- Wing Loading 50.2lbs/ft2 (244.9kg/m2)
- Wing Area 425.5ft2 (39.5m2)
- Drag Points 5874
Parts
- Number of Parts 46
- Control Surfaces 7
- Performance Cost 400
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