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The PROPULSION SYSTEM 2N is an innovative, efficient turbofan engine designed for small aircraft, manned and unmanned aerial vehicles, and vertical and horizontal takeoff and landing systems.
Technical data
Static thrust - 1700 N
Static thrust (max) - 2040 N
Specific fuel consumption - 1,497ˑ10-5 kg/N.sec
Power delivered into network - 1500 W
Weight of the engine - 19,5 kg
Weight of the engine including electronic control, switched source, ignition system, and cabling - 2,5 kg
Service life - 1000 h
Uninterrupted operation - 4 h
Scale
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