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
