| BMW 6012 ✕ | |
|---|---|
| Aircraft Engine Manufacturer | BMW |
| Aircraft Engine Type | Turboshaft |
| Dry Weight (kg) | 45 |
| Diameter (mm) | 380 |
| Length (mm) | 700 |
| Wikipedia Article (URL) | en.wikipedia.org/wiki/BMW_6012 |
| Fuel | Jet fuel |
| Combustion Chamber | Annular (disc shaped) |
| Maximum Takeoff Power (kW) | 74.57 |
| Compressor Description | Single-stage radial |
| Turbine Description | Single-stage radial |