| Aircraft Engine Manufacturer |
Lyulka-Saturn |
Heinkel-Hirth |
| Aircraft Engine Type |
Turbojet |
Turbojet |
| Dry Weight (kg) |
885 |
950 |
| Diameter (mm) |
|
875 |
| Length (mm) |
|
3405 |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Lyulka_TR-1 |
en.wikipedia.org/wiki/Heinkel_HeS_011 |
| Geared Fan |
No |
No |
| Combustion Chamber |
|
16 chamber annular |
| Afterburner |
No |
No |
| Streams |
1 |
1 |
| Maximum Takeoff Thrust (kN) |
12.8 |
12.7 |
| Thrust To Weight |
1.47 |
1.38 |
| Specific Fuel Consumption (g/(kN·s)) |
3653.925 |
|
| Compressor Description |
eight-stage axial-flow |
Diagonal + 3-stage axial |
| Turbine Description |
single stage |
2-stage axial |