FIELD: aviation.
SUBSTANCE: invention relates to the field of aviation, in particular to the structures of aircraft missile systems. The missile and aviation complex includes a heavy aircraft carrier (HACC) and more than one unmanned remotely controlled aircraft (URCAC), the fuselage of which is fixed on the underwing pylon (UWP) of the HACC and/or the intrafuselage pylon (IFP) of the bomb bay. URCAC has an asymmetric sweep wing (ASW), a Y-tail and a turbojet engine with side air intakes, providing flight at altitude in the configuration of a trans-/supersonic URCAC with its ASW deployed to attack the target and its ASW retracted inside the ASW influxes to receive it under the UWP and/or IFP HACC. The HACC is equipped with a flexible attachment system that releases a towing device with a cone on a cable, which docks with the URCAC retractable hook and leads it in flight under the docking/undocking nodes.
EFFECT: increase in the flight range of the missile defense system, the probability of hitting a surface or ground target located at a long range, docking of the URCAC with the carrier aircraft for returning to the home airfield.
3 cl, 1 tbl, 3 dwg
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Authors
Dates
2022-03-28—Published
2021-09-27—Filed