Small aircraft turbojet engine with trust 1000 - 1200 N (225 - 247 lbf) for UAV, powered gliders,...
Newly developed jet engine intended for powered gliders, various UAV applications and experimental aircrafts.
Turbojet engine TJ 100 has single-stage radial compressor, radial and axial diffuser, annular combustion chamber and single stage axial turbine. Rotor seat is lubricated by autonomous oil system. Control is provided by digital electronic system. Starting is electric like fuel and oil pump. Power supply is provided by integrated generator and DC-DC converter. Ignition system is low-voltage, high-up power.
The extensive experience from various APU designs has been used in design and production of this engine ...
|Thrust max.||110 daN (247 lbf)|
|Length||625 mm (24.6 in)|
|Outside diameter||272 mm (10.7 in)|
|Total weight||20,6 kg (45.4 lb)|
|Electrical power output||750 W; 28 V|
|Fuel||JET A-1, JP5, JP8|
|Specific fuel consumption min.||1,09 kg/daN/h|
|Oil||3 cST / 5 cST|
|Altitude||0 - 8000 m|
(0 - 26000 ft)
|Speed||< Mach 0,8|
|Altitude||0 - 4000 m|
(0 - 13000 ft)
|Speed||< Mach 0,4|
|Temperatures||-30 ~ +50 °C|
(-22 ~ +122 °F)