Aircraft engine: Renault 6Q-11
France
inline engine
1932
Configuration | 6-cylinder inline inverted |
Cooling | air-cooled |
Compression ratio | 6.4 |
Weight | 225 kg (496 lb) |
Maximum power | 240 hp at 2,625 RPM |
Climb power | 220 hp at 2,500 RPM |
An engine designed and built by the Société Anonyme des Moteurs Renault company in Billancourt. It was used in the Caudron-Renault C.445 Goeland and Caudron-Renault C.635 Simoun aircraft.
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