ChAI-12
The ChAI-12 Start ( Russian ХАИ-12 Старт ) was a Soviet project for a single-engine, single-seat sport aircraft . It was the Kharkiv Aviation Institute's first project after World War II . The aircraft was designed as a low wing aircraft with retractable tail wheel landing gear. The tailplane was attached halfway up. There were automatic slats on the outer wing parts . The project was worked out by D. Arsona, but the plan was never implemented. The plane was not built.
Project data
Parameter | Data |
---|---|
crew | 1 |
Wing area | 10.13 m² |
Empty mass | 653 kg |
Max. Takeoff mass | 830 kg |
Top speed | 340 km / h |
Range | 510 km |
Engine | 1 × Wedenejew M-14 , 265 kW |