The Su-124 Was One of the first Soviet Aircraft featuring Thrust vectoring. Its Intended Role is Close air Support / Interceptor. Its First Prototype was Made in 1976, It entered Production in 1979, Due to it's unreliability Production Stopped in 1985. All of the Su-124s were Retired By late 1990.
Specifications
General Characteristics
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- Wingspan 33.4ft (10.2m)
- Length 37.8ft (11.5m)
- Height 9.5ft (2.9m)
- Empty Weight 23,472lbs (10,646kg)
- Loaded Weight 33,672lbs (15,273kg)
Performance
- Power/Weight Ratio 2.002
- Wing Loading 104.3lbs/ft2 (509.1kg/m2)
- Wing Area 322.9ft2 (30.0m2)
- Drag Points 4596
Parts
- Number of Parts 61
- Control Surfaces 6
- Performance Cost 619
