TJ 40-G2 Turbojet Engine

TJ 40-G2
TJ 40-G2 Front View
TJ 40-G2 Top View
TJ 40-G2 Side View

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