| Le Rhône 9C ✕ | |
|---|---|
| Aircraft Engine Manufacturer | Le Rhône |
| Aircraft Engine Type | Piston |
| Dry Weight (kg) | 121.5 |
| Diameter (mm) | 94.5 |
| Wikipedia Article (URL) | en.wikipedia.org/wiki/Le_Rh%C3%B4ne_9C |
| Oil System | Castor oil, total loss |
| Cylinders | 9 |
| Cylinders Disposition | rotary |
| Bore (mm) | 105 |
| Stroke (mm) | 140 |
| Displacement (L) | 10.89 |
| Compression Ratio | 4.5 |
| Valvetrain | Cam-operated single rocker for both inlet and exhaust valves |
| Cooling | Air-cooled |
| Maximum Takeoff Power (kW) | 68.6044 |