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Zdenek Liska
Zdenek Liska
Sales Manager

PBS TJ150 Turbojet Engine

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    PBS TJ150_turbojet engine

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    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.

Standard accessories included:

Control System (FADEC), Ignition, Connecting Cable

Optional accessories: 

Electromagnetic fuel valve, fuel Filter, Control Lever, Signalling Panel, Boost Pump, Reduction Valve, Converter CAN, Converter CAN-USB, User Software.

Main features

  • Neat Compact design
  • Excellent power thrust-to-weight ratio
  • Low fuel consumption
  • The built-in starter-generator ensures a reliable start, providing a power supply to the onboard systems, allowing engine cooling while on the ground. 
  • Possibility of customisied production in accordance with customer's requirements.  (adjustment of hinges, the length of the outlet nozzle, water landing capabilities etc..)

PBS INDIA brochures:
TURBINE ENGINES.pdf
Turbojet Engines for Target Drones.pdf
Turbojet Engines for UCAV.pdf

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