| Aircraft Engine Manufacturer |
Armstrong Siddeley |
Lyulka-Saturn |
| Aircraft Engine Type |
Turbojet |
Turbojet |
| Dry Weight (kg) |
249.0222 |
885 |
| Diameter (mm) |
623.57 |
|
| Length (mm) |
1625.6 |
|
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Armstrong_Siddeley_Viper |
en.wikipedia.org/wiki/Lyulka_TR-1 |
| Fuel |
AVTUR, AVTAG |
|
| Geared Fan |
No |
No |
| Combustion Chamber |
Annular, 24 burners |
|
| Afterburner |
No |
No |
| Streams |
1 |
1 |
| Maximum Takeoff Thrust (kN) |
12 |
12.8 |
| Thrust To Weight |
4.9 |
1.47 |
| Specific Fuel Consumption (g/(kN·s)) |
|
3653.925 |
| Compressor Description |
Seven stage axial |
eight-stage axial-flow |
| Turbine Description |
Single stage |
single stage |