RADIO-CONTROLLED MISSILE Russian patent published in 2007 - IPC F42B15/00 

FIELD: armament.

SUBSTANCE: the radio-controlled missile has a sustainer stage detachable zero-stage engine with a fairing an the front end face, antenna device provided with a zero-stage branch in the form of antennas located in the fairing and coupled to the equipment by wave-guides passing through a base in the form of a tube firmly coupled to the engine and installed on the body of the sustainer stage. The zero-stage branch is made detachable in the rolling plane of the waveguides. The parts of the waveguides located inside and outside the body of the sustainer stage are provided with flanges located opposite the ports made in the, body of the sustainer stage. The outer parts of the zero-stage branch are installed on the base and compressed to the flanges of the inner parts of the waveguides through and insert, cavities are made in the front part of the fairing, in which covers of radio wave reflection material are installed, they are movably fastened on the outer surface of the sustainer stage and made with a provision of overlapping of the ports in the sustainer stage when, the covers are in the closed position.

EFFECT: reduced distances arising at a separation of the missile enhanced noise immunity of the missile.

2 cl, 2 dwg