| Tumansky RD-9 ✕ | |
|---|---|
| Aircraft Engine Manufacturer | Shenyang |
| Aircraft Engine Type | Turbojet |
| Dry Weight (kg) | 725 |
| Diameter (mm) | 668 |
| Length (mm) | 5560 |
| Wikipedia Article (URL) | en.wikipedia.org/wiki/Tumansky_RD-9 |
| Geared Fan | No |
| Afterburner | Yes |
| Streams | 1 |
| Maximum Takeoff Thrust (kN) | 29 |
| Thrust To Weight | 5.2 |
| Afterburner Thrust (kN) | 37 |
| Compressor Description | Single-spool 9-stage Axial compressor |
| Turbine Description | axial flow |