| Armstrong Siddeley Viper ✕ | |
|---|---|
| Aircraft Engine Manufacturer | Armstrong Siddeley |
| Aircraft Engine Type | Turbojet |
| Dry Weight (kg) | 249.0222 |
| Diameter (mm) | 623.57 |
| Length (mm) | 1625.6 |
| Wikipedia Article (URL) | en.wikipedia.org/wiki/Armstrong_Siddeley_Viper |
| Fuel | AVTUR, AVTAG |
| Geared Fan | No |
| Combustion Chamber | Annular, 24 burners |
| Afterburner | No |
| Streams | 1 |
| Maximum Takeoff Thrust (kN) | 12 |
| Thrust To Weight | 4.9 |
| Compressor Description | Seven stage axial |
| Turbine Description | Single stage |