| Lyulka TR-1 ✕ | |
|---|---|
| Aircraft Engine Manufacturer | Lyulka-Saturn |
| Aircraft Engine Type | Turbojet |
| Dry Weight (kg) | 885 |
| Wikipedia Article (URL) | en.wikipedia.org/wiki/Lyulka_TR-1 |
| Geared Fan | No |
| Afterburner | No |
| Streams | 1 |
| Maximum Takeoff Thrust (kN) | 12.8 |
| Thrust To Weight | 1.47 |
| Specific Fuel Consumption (g/(kN·s)) | 3653.925 |
| Compressor Description | eight-stage axial-flow |
| Turbine Description | single stage |