Aircraft engine: Shvetsov ASh-21
USSR
radial engine
1948
Configuration | 7-cylinder radial | Cooling | air-cooled | Displacement | 20.6 l (1,257 cu in) | Compression ratio | 6.4 | Weight | 495 kg (1,091 lb) | Maximum power | 700 hp at 2,500 RPM | Climb power | 570 hp at 2,350 RPM |
A radial engine with direct fuel injection. Designed by a team led by A. Shvetsov. The engine was produced after the Second World War in the USSR and on licence in Czechoslovakia as M-21. It was the powerplant of the Yakovlev Yak-11 and Tupolev UTB training aircraft.
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