| Walter M601 ✕ | |
|---|---|
| Aircraft Engine Manufacturer | Motorlet |
| Aircraft Engine Type | Turbopropulsor |
| Dry Weight (kg) | 197 |
| Diameter (mm) | 590 |
| Length (mm) | 1675 |
| Wikipedia Article (URL) | en.wikipedia.org/wiki/Walter_M601 |
| Combustion Chamber | annular |
| Maximum Takeoff Power (kW) | 544 |
| Specific Fuel Consumption (g/(kW·h)) | 229320.4 |
| Compressor Description | 2-stage axial compressor and 1-stage centrifugal compressor |
| Turbine Description | 1-stage high-pressure and 1-stage free |