| Tumansky R-25 ✕ | |
|---|---|
| Aircraft Engine Manufacturer | Tumansky |
| Aircraft Engine Type | Turbojet |
| Dry Weight (kg) | 1212 |
| Diameter (mm) | 1191 |
| Length (mm) | 4615 |
| Wikipedia Article (URL) | en.wikipedia.org/wiki/Tumansky_R-25 |
| Geared Fan | No |
| Combustion Chamber | Cannular 10 burners |
| Afterburner | Yes |
| Streams | 1 |
| Maximum Takeoff Thrust (kN) | 40.3 |
| Thrust To Weight | 5.6 |
| Afterburner Thrust (kN) | 69.6 |
| Compressor Description | Two-spool axial compressor 3 LP stages, 5 HP stages |
| Turbine Description | 1 HP stage, 1 LP stage |