TJ-100 Turbojet Engine
This small turbojet engine has been developed for light air vehicles, such as light and ultralight sports planes, sailplanes equipped with auxiliary engine, piloted vehicles of EXPERIMENTAL class and various unmanned air vehicles.
TJ 100 is currently sold in several variants. Since 2008 over 1200 units have been delivered. TJ 100 is a completely newly developed power unit with excellent weight/thrust ratio. The TJ 100 features the latest technologies including FADEC. In the category of small turbojet engines, TJ 100 with thrust up to 1250 N ranks among the best in the world.
Single-stage radial compressor, radial and axial diffuser, annular combustion chamber, and single-stage axial turbine. Rotor bearings are lubricated by internal recirculating oil system. The engine is controlled by an electronic FADEC system. Starter/generator and all accessories are electric and controlled by the FADEC unit. Power supply is ensured by integral generator and DC-DC converter. Ignition is a true spark system (not glow plug).