Turbine Solution Group
TJ100 Turbojet Engine
TJ100 was designed for propulsion of
manned and unmanned aircraft. Development began in 2002 and a prototype
was developed and successfully tested in a pressure chamber. The test
where positive and the engine went into production.
There are over 150 engines currently flying in various different
configurations. The TJ100 engine is also flying in the U.S.A. on a manned
Salto sailplane that premiered in EAA AirVenture 2009.
The current engine has these specifications.
TJ100 Engine Parameters:
*SFC - Standard atmospheric conditions
Intake air is compressed by radial compressor. The passes through radial and axial diffusers into the combustion chamber. Fuel nozzles spray fuel and the expanded gases pass thru the single stage axial turbine. They are then expelled from the exhaust nozzle.
Mobil Jet Oil II or Aeroshell Turbine Oil 390
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