FIELD: aviation.
SUBSTANCE: invention relates to aircraft engineering, particularly, to designs and methods of using unmanned aerial vehicles to combat sea targets. Unmanned convertiplane rocket carrier (UCRC) comprises fuselage, bearing wing with tail unit, engine, onboard control system providing autonomous (AC) and remote control from command post, on-board power supply. UCRC is equipped with two-rotary transverse bearing system (TBS), including two single-blade rotors (SBR) with shaped counterweights mounted on the ends of the sweep of forward swept wing (FSW) and providing creation of vertical thrust only at vertical and short take-off/landing or in transition modes of flight. UCRC is also equipped with two turbojets in common stern nacelle. Air intake inlet device has controlled different-sized flaps arranged under the lower or above the upper inclined channel of the air duct so that the greater one of them deflects into the channel and the smaller one deviates into the outside of the fuselage. depending on flight speed.
EFFECT: higher probability of destruction of surface or underwater targets located at long range.
5 cl, 4 dwg, 1 tbl
