TJ 40-G1 Turbojet Engine

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The TJ 40-G1 is a turbojet engine designed for UAV systems, such as target drones and decoy drones, in order to confuse enemy air defenses and small reconnaissance drones. Its advantage is its low weight of 3.3 kg and thrust of 395 N. The PBS TJ40-G1 jet engine is a single-shaft engine with a one-stage radial compressor, radial and axial diffuser, annular combustion chamber, one-stage axial turbine and outlet nozzle. The output of the generator is 150 W.

Standard accessories - included: fuel pump and filter, engine control unit (ECU), connecting cables, fuel hose, data terminal, battery (4s Li-Fe - 2,5 Ah), CAN connector  

Main  features
  • Compact design – all accessories integrated within the engine body (excl. fuel pump).
  • Excellent thrust-to-weight ratio and low fuel consumption for its power category.
  • Kerosene starting.
  • Integrated starter-generator.
  • Recipient of a prestigious journalistic award at the IDET 2015 exhibition.
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