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TJ-40-G2-Turbojet-Engine - 2 Pages

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TJ-40-G2-Turbojet-Engine
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Catalog excerpts

TURBOJET ENGINE New development for UAV's, gliders and bigger modeller applications.

 Open the catalog to page 1

Examples of possible TJ 40 applications Technical parameters: Thrust: take-off (max 5 min) Dimensions and weight Outside diameter Length Weight of the engine Weight of the accessories Other data Fuel consumption max. Max. EGT Suction amount of air Revolutions max. Lubrication Fuel Generator power output 1230 ml/min 780 °C 0,78 kg/sec 98 000 RPM 3% oil in fuel kerosine/diesel 800 W Brushless starting generator 1st. radial compressor Toroidal combustion chamber Kerosine starting system 1st. axial turbine Ceramic bearings 3 electrovalves Sensor EGT Engine electronics AC-DC changer Accessories includes:...

 Open the catalog to page 2

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