[R] F-4E
Control:
VTOL - Flaps
Trim - Trim
Ag1 - lights
Ag2 - parachute
Ag3 - aresting hook
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 that was developed by McDonnell Aircraft for the United States Navy. Proving highly adaptable, it entered service with the Navy in 1961 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.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.
Specifications
General Characteristics
- Predecessor F-4E
- Created On Windows
- Wingspan 40.5ft (12.4m)
- Length 66.7ft (20.3m)
- Height 17.1ft (5.2m)
- Empty Weight 29,611lbs (13,431kg)
- Loaded Weight 43,188lbs (19,589kg)
Performance
- Power/Weight Ratio 0.52
- Wing Loading 75.3lbs/ft2 (367.9kg/m2)
- Wing Area 573.2ft2 (53.3m2)
- Drag Points 7731
Parts
- Number of Parts 277
- Control Surfaces 5
- Performance Cost 1,527