The HJ50 is a turbine jet engine composed of a single-stage centrifugal compressor and an axial-flow turbine. It is started using an electric motor, and the control system is integrated into the engine. Currently, it is primarily applied in UAVs, target drones, and target missiles.
Technical Specifications |
Model | HJ50 |
Type | Centrifugal compressor, axial-flow turbine |
Dimensions | ∅177mm×460mm |
Weight | ≯5.5kg |
Maximum Thrust | ≮50daN |
Fuel Consumption Rate | ≯1.5kg/(daN.h) |
Maximum Operating Altitude | 10000m |
Maximum Operating Speed | 0.8Ma |
Operating Temperature | -40℃~55℃ |
Operating Life | 25h |
.png?x-oss-process=style/png_small)
Sichuan hongying power technology co., ltd.
