The McDonnell Douglas F-4 Phantom II[N 1] is a 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 first 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 an iconic combat aircraft of the Cold War.[4][5]
Specifications
General Characteristics
- Created On Windows
- Wingspan 24.9ft (7.6m)
- Length 28.7ft (8.8m)
- Height 11.6ft (3.5m)
- Empty Weight N/A
- Loaded Weight 4,602lbs (2,087kg)
Performance
- Power/Weight Ratio 14.649
- Wing Loading 21.4lbs/ft2 (104.3kg/m2)
- Wing Area 215.5ft2 (20.0m2)
- Drag Points 1285
Parts
- Number of Parts 66
- Control Surfaces 5
- Performance Cost 473