FIELD: aviation.
SUBSTANCE: invention relates to military modular hardware. Stealthy missile-aviation system (SMAS) with an unmanned aerial vehicle having a fuselage, a launching device with a guided missile, a wing with its control elements, engine of power plant, onboard control system providing for telemechanical control from command post of aircraft-carrying ship (ACS). SMAS is equipped with a group of optional and remotely piloted aircraft-helicopters, which are a flying closed wing of a rhomboid-shaped plan with two over-wing nacelles, having combined gas turbine engines with free power turbines, leading two pusher twin-bladed rotors (TBR) in fairings of all-turning inter-gondagonal wing and/or in annular fairings external fans, creating at vertical take-off and/or horizontal flight propulsive thrust directed horizontally backwards with working transverse TBR/inclined autorotating or folded blades from vane position along and outside the cowlings of the TBR with their horizontal fixation in the course of translational flight in the configuration of the rotorcraft/gyroplane or the jet aircraft transformed after landing on the ship deck into the traveling configuration with the wing ends folded upwards for transportation in the hangar, fueling and loading with ammunition.
EFFECT: higher weight output and combat load, higher speed and range of flight, higher probability of destruction of surface, underwater and air targets.
5 cl, 1 tbl, 1 dwg
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Authors
Dates
2020-06-02—Published
2019-07-11—Filed