F104It is the second generation supersonic fighter developed by Lockheed in the mid-1950s.The design of F-104 fighter was contrary to the trend of large-scale and heavy-duty of the U.S. air force at that time, emphasizing lightness and simplicity. The F-104 is the world's first fighter with a speed up to twice the speed of sound, with a maximum usable overload of 7.33. It has long maintained the world record of climb rate and maximum lift limit in the 1960s [3].F-104g fighters are exported to Germany, Japan, Canada, Italy, the Netherlands and Denmark for mass production. The main types of F-104 are a, C, G, J, s, etc. A total of 2578 were produced
Specifications
General Characteristics
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- Wingspan 16.6ft (5.1m)
- Length 37.7ft (11.5m)
- Height 9.4ft (2.9m)
- Empty Weight N/A
- Loaded Weight 7,233lbs (3,280kg)
Performance
- Power/Weight Ratio 4.66
- Wing Loading 64.4lbs/ft2 (314.3kg/m2)
- Wing Area 112.3ft2 (10.4m2)
- Drag Points 3675
Parts
- Number of Parts 229
- Control Surfaces 6
- Performance Cost 1,028
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