| Aircraft Engine Manufacturer |
Allison |
| Aircraft Engine Type |
Turbopropulsor |
| Dry Weight (kg) |
555.6507 |
| Diameter (mm) |
713.74 |
| Length (mm) |
2133.6 |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Allison_T38 |
| Fuel |
MIL-F-5572 100/130 Octane Gasoline |
| Combustion Chamber |
8 tubular inter-connected stainless steel combustion chambers |
| Maximum Takeoff Power (kW) |
1901.535 |
| Power To Weight (kW/kg) |
3.737 |
| Specific Fuel Consumption (g/(kW·h)) |
383.2 |
| Compressor Description |
17-stage axial |
| Turbine Description |
4-stage axial discs of Timken 16-25-4 alloy with special alloy blades |