FIELD: aviation.
SUBSTANCE: invention relates to aircraft engineering, particularly, to aircraft strike systems. Air strike missile system includes a group of shipborne or airborne vertical takeoff and landing vehicles, which include respectively one optionally piloted aircraft-helicopter (OPAH) with more than one remotely piloted aircraft-helicopter (RPAH). Each device is made with tandem sweep wings, has on pylon of fuselage two twin-bladed rotors (TBR) and in the stern nacelle free power turbine, leading TBR and the portable turbofan, creating lifting force and reactive cruise thrust with operating/autorotating coaxial TBR or fixed with their center of masses by their shutter sweep swept wings during horizontal flight in configuration of jet rotorcraft/gyroplane or triplane aircraft. Apparatuses are made as converted after landing in marching configuration by means of folding blades of TBR, wings and keels of V-shaped fins for shipborne and airborne location.
EFFECT: higher probability of destruction of surface, underwater and air targets located at long range, multiple applications.
5 cl, 1 dwg, 1 tbl
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Authors
Dates
2020-06-01—Published
2019-02-25—Filed