100kg Thrust Turbojet Engine TWP100E （Low cost, high performance）
SKU: MD-P00472·Spare Parts & Components·受注生産
概要
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
技術仕様
Specifications. 主な仕様： 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。
技術仕様 — 1 groups
主な仕様： 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。
技術仕様
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
対応機体
この部品は以下のプラットフォームに対応します。
適合データの準備中です。機体の型番をお知らせください。