The HJ150B is a turbine jet engine composed of a single-stage centrifugal compressor and an axial-flow turbine. It uses an electric motor for starting, and all control system accessories are internally integrated. Currently, it is primarily applied in UAVs, target drones, and cruise missiles.
Technical Specifications |
Model | HJ80 |
Type | Centrifugal compressor, axial-flow turbine |
Dimensions | ∅264mm×636.5mm |
Weight | ≯26kg |
Maximum Thrust | ≮150daN |
Fuel Consumption Rate | ≯1.5kg/(daN.h) |
Maximum Operating Altitude | 10000m |
Maximum Operating Speed | 0.8Ma |
Rated Exhaust Temperature | 750℃ |
Operating Temperature | -40℃~55℃ |
Operating Life | 25h |