The engine is designed for subsonic unmanned aerial vehicles of different purpose.


Main advantages of the engine:

  • high reliability;
  • high fuel efficiency;
  • low thrust-to-weight ratio;
  • long period of operation and storage in aircraft and insignificant scope of maintenance operations;
  • quick and reliable starting within wide range of environmental conditions as well as altitudes and airspeed;
  • resistance to instability of engine inlet air pressure and temperature;
  • capability of inadvertent surge recovery;
  • compact and simple single-shaft design;
  • built-in electric generator providing power supply to aircraft systems;
  • electronic-and-hydraulic automatic control system which does not need adjustment during storage and operation;
  • feasibility of air bleeds for aircraft needs.

Basic specifications: