| Kuznetsov NK-12 ✕ | |
|---|---|
| Aircraft Engine Manufacturer | Kuznetsov Design Bureau |
| Aircraft Engine Type | Turbopropulsor |
| Dry Weight (kg) | 2900 |
| Diameter (mm) | 1150 |
| Length (mm) | 6000 |
| Wikipedia Article (URL) | en.wikipedia.org/wiki/Kuznetsov_NK-12 |
| Fuel | Aviation kerosene such as JP-4 / Soviet spec. T-1 or T-2 |
| Combustion Chamber | 12 combustion chambers |
| Maximum Takeoff Power (kW) | 11185.5 |
| Power To Weight (kW/kg) | 3.7 |
| Specific Fuel Consumption (g/(kW·h)) | 219 |
| Compressor Description | 14-stage axial flow |
| Turbine Description | 5-stage axial turbine |