| Turbomeca Orédon (1947) ✕ | |
|---|---|
| Aircraft Engine Manufacturer | Turbomeca |
| Aircraft Engine Type | Turboshaft |
| Dry Weight (kg) | 81 |
| Length (mm) | 870 |
| Height (mm) | 520 |
| Width (mm) | 408 |
| Wikipedia Article (URL) | en.wikipedia.org/wiki/Turbomeca_Or%C3%A9don_%281947%29 |
| Fuel | kerosene |
| Combustion Chamber | single annular combustion chamber with rotary disc fuel injector |
| Maximum Takeoff Power (kW) | 119.312 |
| Specific Fuel Consumption (g/(kW·h)) | 590 |
| Compressor Description | 1-stage centrifugal |
| Turbine Description | 2-stage axial |