100kg Thrust Turbojet Engine TWP100E （Low cost, high performance）
SKU: MD-P00472·Spare Parts & Components·Made to Order
Overview
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
Technical specification
Specifications. Key specifications: Max. thrust (kgf) 95, Max. altitude (m) 12000, Max. speed (Ma) 0.9, Outside diameter(mm) 230 535, Thrust to weight ratio 7.5, Fuel consumption (kg/kgf h) 1.4, Electrical power output (W) 800, Lifetime (h) 30.
Technical specification — 1 groups
Key specifications: Max. thrust (kgf) 95, Max. altitude (m) 12000, Max. speed (Ma) 0.9, Outside diameter(mm) 230 535, Thrust to weight ratio 7.5, Fuel consumption (kg/kgf h) 1.4, Electrical power output (W) 800, Lifetime (h) 30.
Technical specifications
Specifications
- Max. thrust (kgf)
- 95
- Max. altitude (m)
- 12000
- Max. speed (Ma)
- 0.9
- Outside diameter(mm)
- 230 535
- Thrust to weight ratio
- 7.5
- Fuel consumption (kg/kgf h)
- 1.4
- Electrical power output (W)
- 800
- Lifetime (h)
- 30
Compatible aircraft
This part fits the following platforms.
Fitment data pending — contact us with your aircraft model.