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Home >  Turbine & EDF Jet >  PBS Turbine Engine > PBS TJ40-G1NS Turbojet Engine for Manned Glider, Drone & RC Jet 425N/43Kg Thrust +150W Generator

PBS TJ40-G1NS Turbojet Engine for Manned Glider, Drone & RC Jet 425N/43Kg Thrust +150W Generator (Global Warehouse)

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      • Product Details
      • Manual
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      Our expert technicians at PBS have designed and developed the PBS TJ40-G1 turbojet engine within the small turbojet engine category for small aircraft such as gliders and some larger model aircraft. 

      It has an extremely compact design, with all accessories integrated within the engine body (excluding the fuel pump). It is also very a light weight of only 3.6 kg, and a maximum thrust of 425 N. The start-up sequence is advantageously short at less than 25 seconds and there is an easy and rapid kerosene starting system. The PBS TJ40-G1 can restart from the ground as well as in-flight and has unilimited starting position angles.

      The PBS TJ40-G1NS small turbojet 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. It is slightly more compact than the TJ40-G2, which is measures just 69 mm longer than the PBS TJ40-G1.

      Standard accessories: 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

      • ‘Plug & Play’ design
      • Salt water recovery
      • Integrated starter-generator
      • Compact design
      • EASA standards

      PBS TJ40-G1NS Engine Parameters

      Technical parameters SI Units Imperial Units
      Max. thrust 425 N  96 lbf
      Fuel consumption 0.147 kg/N/H 1.442 lb/lbf/hr
      Outer diameter 147 mm 5.79 in
      Length 304 mm 11.97 in
      Weight 3.6 kg 7.94 lb
      Max. altitude for operating envelope 9,000 m 29,528 ft
      Max. altitude for starting envelope 4,500 m 14,764 ft

      TJ40.jpg



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