History:
The Lockheed F-104 Starfighter was the first operational interceptor capable of sustained speeds above Mach 2. Design work began in 1952 and the first test flights were flown in 1954. The F-104 was intended as a short-range point defense fighter with both single and two seat versions. The Starfighter was extensively exported and built under license in Canada, Europe, and Japan. The F-104D model is a two seat fully combat-capable trainer built for use by the U.S. Air Force’s Tactical Air Command between November 1958 and September 1959. A total of 21 were built. To make room for the second seat the F-104D gave up its internal gun but was given an enhanced ground strike capability and in-flight refueling.
Controls:
AG1 Tail hook
AG2 Switch sights
AG4 & 5 Jettison fuel tanks & weapons
AG6 Enable parachute
AG8 Lights
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Specifications
General Characteristics
- Predecessor Supersonic Challenge
- Created On Windows
- Wingspan 22.4ft (6.8m)
- Length 54.8ft (16.7m)
- Height 12.8ft (3.9m)
- Empty Weight 18,412lbs (8,352kg)
- Loaded Weight 18,412lbs (8,352kg)
Performance
- Power/Weight Ratio 0.846
- Wing Loading 73.2lbs/ft2 (357.3kg/m2)
- Wing Area 251.6ft2 (23.4m2)
- Drag Points 641
Parts
- Number of Parts 455
- Control Surfaces 0
- Performance Cost 2,166
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