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TURBOJET ENGINE Small turbojet with designed for experimental aircrafts, powered gliders and UAV, UCAV systems.

Main parameters – performance (ISA SL) Max. thrust Min. specific fuel consumption Electrical power output Dimensions and weight Max. diameter Length Dry weight (with accessories) Operating range Flight envelope – altitude Flight envelope – speed Start envelope – altitude Start envelope – speed Start envelope – temperature Main features • Compact design, excellent thrust/weight ratio and low fuel consumption at its power category • Integrated starter-generator is enabling the reliable starting by battery 24 V, electricity supply to board net and engine cooling after stop • Classical...

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