TWP100E 100kg thrust turbojet engine is a low-cost, short-life, high thrust-to-weight ratio small turbojet engine independently developed by the Chinese Academy of Sciences.
The engine is mainly composed of a 1-stage high-pressure ratio centrifugal compressor, an annular evaporating tube combustion chamber, a 1-stage axial-flow turbine, a casing and a fuel conditioning system. The engine adopts a unique high-wheel-to-hub ratio compressor design. Through the built-in generator installation structure, the engine itself can obtain 800W of electricity.
Throttle characteristics of engine thrust and fuel consumption
Engine working envelope
ECU controller
Technical Parameters：
| 95 kgf Turbojet Engine | |
| Max. thrust (kgf) | 95 |
| Max. altitude (m) | 12000 |
| Max. speed (Ma) | 0.9 |
| Outside diameter(mm) | Φ230×535 |
| Thrust to weight ratio | 7.5 |
| Fuel consumption (kg/kgf·h) | 1.4 |
| Electrical power output (W) | 800 |
| Lifetime (h) | 30 |
