The NM-150P turbojet engine is a small turbojet engine composed of a single-stage centrifugal compressor and an axial flow turbine, with a maximum net thrust of 150daN. The engine runs stably and reliably, and can provide power for high-subsonic UAVs, unmanned target drones, small missiles and other aircraft, and is an ideal small aviation power device.
This turbojet engine has been equipped with a large number of troops.
Basic parameters
Diameter: 310mm
Length: 650mm
Weight: 42kg
Maximum thrust: 145daN
Fuel consumption rate: ≤1.3kg/(daN.h)
