FIELD: weapons; aviation.
SUBSTANCE: invention relates to military modular hardware. Aviation reconnaissance-damaging system (ARDS) comprises an unmanned aerial vehicle having a fuselage with a detachable guided missile, a wing with its control elements, engine of power plant, on-board control system providing for telemechanical control from command post of carrier vehicle. ARDS containing optionally and remotely piloted convertible aircraft of integral configuration, including flying wing, having variable and saw-like sweep along front and rear edges and on its cantilevers two combined engines with free power turbines, leading two pairs of transverse lifting fans (LF) and/or in annular fairings front fans, lifting and/or propulsive thrust with vertical or short take-off/landing (VTL and STL) with operating or fixed LF at automatically open/closed upper longitudinal shutters and lower transverse louvres of wing annular fairings in configuration of jet airplanes when performing VTL, STL/horizontal flight, having in the fuselage airframes of controlled missiles and folding external sections of wing after their landing on deck of aircraft carrier (AC).
EFFECT: increased weight and combat load, increased speed and range of flight, increased probability of destruction of surface, underwater and air targets located at long range.
4 cl, 1 tbl, 1 dwg
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Authors
Dates
2020-07-02—Published
2019-05-07—Filed