Sichuan hongying power technology co., ltd.
Sichuan Hawk Power Technology Co., Ltd
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Turbojet EngineYour current location:Home >Turbojet Engine

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