PBS TJ150_turbojet engine
PBS TJ150_3D visualization
The PBS TJ150 jet engine was designed and developed for unmanned vehicles (UAV’s), training targets and missiles. It is main advantages are its compact design, light weight with a power thrust of up to 1,500 N, and its low fuel consumption, while the generator output is 750 W. In addition, one version of the PBS TJ150 turboshaft engine has the capability of landing on water. This engine is a single-shaft jet engine consisting of a radial compressor, radial and axial diffuser, annular combustion chamber, axial turbine and a fixed outlet nozzle.
Control System (FADEC), Ignition, Connecting Cable
Electromagnetic fuel valve, fuel Filter, Control Lever, Signalling Panel, Boost Pump, Reduction Valve, Converter CAN, Converter CAN-USB, User Software.