| General Electric TF39 ✕ | |
|---|---|
| Aircraft Engine Manufacturer | General Electric Company |
| Aircraft Engine Type | Turbofan |
| Dry Weight (kg) | 3628.739 |
| Diameter (mm) | 2463.8 |
| Length (mm) | 7924.8 |
| Wikipedia Article (URL) | en.wikipedia.org/wiki/General_Electric_TF39 |
| Geared Fan | No |
| Combustion Chamber | Annular |
| Afterburner | No |
| Streams | 2 |
| Maximum Takeoff Thrust (kN) | 193 |
| Thrust To Weight | 5.4 |
| Compressor Description | Axial, low pressure compressor, comprising single stage booster and a single stage fan, 16-stage high-pressure compressor |
| Turbine Description | Axial, 2-stage high-pressure turbine, 6-stage low-pressure turbine |