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Auto Credit Based on Jackrei's Simple Su-9 1946
Before the prototype was finished, Sukhoi was ordered to use the Lyulka TR-1 turbojets originally intended for the Su-9. This aircraft was designated the Su-11 and was called Samolyet KL by the OKB. Each TR-1 developed only 12.7 kN (2,865 lbf) thrust each, rather than the 15 kN (3300 lbf) required. The aircraft made its first flight on 28 May 1947 and also participated in the flypast at Tushino in August. It had a maximum speed of 940 km/h (580 mph) at sea level
Specifications
General Characteristics
- Predecessor Simple Su-9 1946
- Created On Android
- Wingspan 46.2ft (14.1m)
- Length 43.1ft (13.1m)
- Height 17.5ft (5.3m)
- Empty Weight 20,944lbs (9,500kg)
- Loaded Weight 27,403lbs (12,429kg)
Performance
- Power/Weight Ratio 0.893
- Wing Loading 69.8lbs/ft2 (340.9kg/m2)
- Wing Area 392.4ft2 (36.5m2)
- Drag Points 2425
Parts
- Number of Parts 317
- Control Surfaces 7
- Performance Cost 1,152
