The HJ150 is a turbine jet engine composed of a single-stage centrifugal compressor and an axial-flow turbine. It is capable of external power generation and internally integrates an oil pump, electromagnetic valve, and temperature sensor. It features electric and pyrotechnic starting capabilities. Currently, it is primarily applied in UAVs, target drones, and cruise missiles.
Technical Specifications: |
Model | HJ150 |
Type | Centrifugal compressor, axial-flow turbine |
Dimensions | ∅250mm×735mm |
Weight | ≯24kg |
Maximum Thrust | ≮150daN |
Fuel Consumption Rate | ≯1.3kg/(daN.h) |
Maximum Operating Altitude | 12000m |
Maximum Operating Speed | 0.8Ma |
Rated Exhaust Temperature | 750℃ |
Operating Temperature | -40℃~55℃ |
Operating Life | 25h |
External Power Generation | 2000W |