| Aircraft Engine Manufacturer |
Armstrong Siddeley |
IL |
| Aircraft Engine Type |
Turbojet |
Turbojet |
| Dry Weight (kg) |
249.0222 |
321 |
| Diameter (mm) |
623.57 |
707 |
| Length (mm) |
1625.6 |
2157 |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Armstrong_Siddeley_Viper |
en.wikipedia.org/wiki/PZL_Rzesz%C3%B3w_SO-3 |
| Fuel |
AVTUR, AVTAG |
|
| Geared Fan |
No |
No |
| Combustion Chamber |
Annular, 24 burners |
Annular with 24 combustors |
| Afterburner |
No |
No |
| Streams |
1 |
1 |
| Maximum Takeoff Thrust (kN) |
12 |
10.8 |
| Thrust To Weight |
4.9 |
3.4 |
| Compressor Description |
Seven stage axial |
Seven-stage all-steel axial compressor |
| Turbine Description |
Single stage |
Single-stage axial flow |