On International Aviation and Space Show (MAKS) 2017 our company presented the prototype of a micro turbojet D200 engine. The engine is designed according to the classical scheme for this type of engines: a single-stage centrifugal compressor with a channel diffuser, an annular combustion chamber with an evaporative fuel supply system, a single-stage axial turbine. Control is provided by digital control system with all necessary tools located beneath the body.
This engine is able to reach the thrust of up to 21kgf. The engine is intended to be utilized of local market UAV manufacturers