TM TJ-200 Turbojet

The TJ-200 is a single spool turbojet engine capable of providing up to 200 lbf of thrust. A very economical and lightweight propulsion system for small cruise missiles, military UAVs and air target drones. The breakthrough technology of this engine is its small axial compressor.

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GENERAL CHARACTERISTICS

  • Type: Single spool turbojet

  • Length: 520 mm

  • Diameter: 180 mm

  • Dry weight: 10 kg

  • Maximum uninstalled thrust: 1 kN @SSL (200 lbf)

  • Specific fuel consumption: 1.26 kg/Kgf/h


COMPONENTS

  • Compressor: 4 axial stages

  • Combustor: Annular

  • Turbine: Single axial stage

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TM TJ-200 Tech Specification