40kg Thrust Turbojet NM-40
SKU: MD-P00476·Spare Parts & Components·受注生産
概要
The NM-40 turbojet engine is a single-shaft small jet engine with a centrifugal compressor and a centripetal turbine, with a maximum static thrust of 40kg. The engine adopts a mixed fuel system design, and the engine control unit (ECU) adopts a digital fuel adjustment design, which can monitor and protect the working state of the engine, and is easy and reliable to operate. The engine can provide power for small unmanned aerial vehicles and target drones, and is an ideal small aviation turbojet power. This NM-40 turbojet engine has been widely used in target drones. Maximum thrust: 40daN (standard atmosphere at sea level) Fuel consumption rate: 1.45kg/daN.h Exhaust temperature: 600 ℃ Operating temperature: -40℃~+50℃ Use ceiling: 8000 meters (altitude)
技術仕様
Specifications. 主な仕様： Maximum diameter 154mm、Length 420mm、Total weight 7kg、Maximum speed 91000rpm、Maximum thrust 40daN (standard atmosphere at sea level)、Pressure ratio 3.75、Air flow 0. 75kg/s、Fuel consumption rate 1.45kg/daN. h、Generating power 1000W、Exhaust temperature 600 ℃、Operating temperature -40℃~+50℃、Use ceiling 8000 meters (altitude)、Service life 20H。
技術仕様 — 1 groups
主な仕様： Maximum diameter 154mm、Length 420mm、Total weight 7kg、Maximum speed 91000rpm、Maximum thrust 40daN (standard atmosphere at sea level)、Pressure ratio 3.75、Air flow 0. 75kg/s、Fuel consumption rate 1.45kg/daN. h、Generating power 1000W、Exhaust temperature 600 ℃、Operating temperature -40℃~+50℃、Use ceiling 8000 meters (altitude)、Service life 20H。
技術仕様
Specifications
- Maximum diameter
- 154mm
- Length
- 420mm
- Total weight
- 7kg
- Maximum speed
- 91000rpm
- Maximum thrust
- 40daN (standard atmosphere at sea level)
- Pressure ratio
- 3.75
- Air flow
- 0. 75kg/s
- Fuel consumption rate
- 1.45kg/daN. h
- Generating power
- 1000W
- Exhaust temperature
- 600 ℃
- Operating temperature
- -40℃~+50℃
- Use ceiling
- 8000 meters (altitude)
- Service life
- 20H
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。