| Armstrong Siddeley Mamba ✕ | |
|---|---|
| Aircraft Engine Manufacturer | Armstrong Siddeley |
| Aircraft Engine Type | Turbopropulsor |
| Dry Weight (kg) | 385.5535 |
| Diameter (mm) | 838.2 |
| Length (mm) | 2291.08 |
| Wikipedia Article (URL) | en.wikipedia.org/wiki/Armstrong_Siddeley_Mamba |
| Fuel | Aviation Kerosene / JP-4 |
| Combustion Chamber | Annular combustion chamber with 24 vapourising burners |
| Maximum Takeoff Power (kW) | 1230.405 |
| Power To Weight (kW/kg) | 3.42 |
| Specific Fuel Consumption (g/(kW·h)) | 419.7 |
| Compressor Description | 11 stage axial flow |
| Turbine Description | 3 stage axial flow |