The HJ40A is a turbine jet engine composed of a single-stage centrifugal compressor and an axial-flow turbine. It provides maximum integration with a control system and simplified installation, with all necessary peripheral systems integrated inside the engine's front casing. It is mainly started using an electric motor. Currently, it is primarily utilized in model aircraft and target drones.
Technical Specifications |
Model | HJ40A |
Type | Centrifugal compressor, axial-flow turbine |
Dimensions | ∅146mm×347mm |
Weight | ≯4kg |
Maximum Thrust | ≮400N |
Fuel Consumption Rate | ≯600ml/min |
Maximum Operating Altitude | 6000m |
Maximum Operating Speed | 0.6Ma |
Rated Exhaust Temperature | 750℃ |
Operating Temperature | -40℃~55℃ |
Operating Life | 25h |