FIELD: coastal aviation missile systems.
SUBSTANCE: invention relates to coastal aviation missile systems with unmanned convertible aircraft (UCAC). The UCAC contains a turbofan engine (TFE), a Y-tail (YT) and a bidirectional wing (BDW) mounted on top of the fuselage with bilateral symmetry/asymmetry in two positions, having in any of a number of positions different-sized in span greater (GW) and smaller (SW) wings. The BDW is integrated with the upper hinge of the wing, the servo drive of which provides, after launch, the unfolding of the SW and the subsequent clockwise rotation of the high-lying BDW.
EFFECT: reduction of dimensions in the transport and traveling configuration, increase in speed, flight range and target load.
2 cl, 3 dwg, 1 tbl
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