100kg Thrust Turbojet Engine TWP100E （Low cost, high performance）

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