TJ 40-G2 Turbojet Engine
A small turbojet engine TJ 40 - G2 has been developed for UAVs, gliders and bigger modeller applications with a need of higher power supply up to 800 W.
Motor TJ 40 - G2 is a new development in out turbojet engine line.
TJ 40 - G2 turbojet engine is a single-shaft turbine engine with a single-stage radial compressor, annular combustion chamber, single-stage axial turbine and diffuser. The output of power generator is 800 W.
For more information, please contact PBS Aerospace