| Aircraft Engine Manufacturer |
Walter Aircraft Engines |
| Aircraft Engine Type |
Turbopropulsor |
| Dry Weight (kg) |
570 |
| Diameter (mm) |
753 |
| Length (mm) |
2565 |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Walter_M602 |
| Fuel |
Aviation kerosene |
| Combustion Chamber |
Annular combustion chamber |
| Maximum Takeoff Power (kW) |
1360 |
| Power To Weight (kW/kg) |
602 |
| Compressor Description |
2-spool centrifugal compressor |
| Turbine Description |
1-stage HP axial turbine (with internally cooled blades), 1-stage axial IP compressor, 2-stage LP axial power turbine |