0 - 100kN turbojet / 0 - 100kg / for drones
TJ40-G1

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Characteristics

  • Thrust:

    0 - 100kN

  • Dry weight:

    0 - 100kg

  • Applications:

    for drones

Description

Jet Engine PBS TJ40-G1
The small PBS TJ40-G1 jet engine was developed for unmanned systems.
Compact design - all accessories incorporated in the engine (except for the fuel pump)
Excellent thrust-to-weight ratio, low power consumption in the given power category
Any engine position during start
Shortened start sequence under 25 seconds

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