| Aircraft Engine Manufacturer |
Junkers |
Klimov |
| Aircraft Engine Type |
Turbojet |
Turbojet |
| Dry Weight (kg) |
2000 |
872 |
| Diameter (mm) |
1064 |
1300 |
| Length (mm) |
4860 |
2600 |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Junkers_Jumo_012 |
en.wikipedia.org/wiki/Klimov_VK-1 |
| Geared Fan |
No |
No |
| Combustion Chamber |
8 chamber can-type |
Nine can combustion chambers |
| Afterburner |
No |
No |
| Streams |
1 |
1 |
| Maximum Takeoff Thrust (kN) |
27.3 |
26.5 |
| Thrust To Weight |
1.39 |
3.1 |
| Specific Fuel Consumption (g/(kN·s)) |
|
3090.257 |
| Compressor Description |
11-stage axial compressor |
Centrifugal compressor |
| Turbine Description |
2-stage |
single stage axial |