GUIDED MISSILE Russian patent published in 2007 - IPC F42B15/00 

FIELD: armament.

SUBSTANCE: the guided missile has successively positioned control compartment, acceleration-cruise engine, warhead, tail section with stabilizer cantilevers, on-board radiation source and a coil of the wire communication line. The quantity of supports corresponds to the number of the stabilizer cantilevers. Each support is fastened to the guided missile body in such a way that the support longitudinal axis forms an acute angle with the longitudinal axis of the guided missile. Two rectangular slots are made in the front and rear parts of the supports. Two straps are fastened in the lower base of each stabilizer cantilever, and two semicircular bulges are formed, they enter the support slots. The diametric height of the supports exceeds the outside diameter of the coil of the wire communication line. The length of the supports is commensurable with the length of the lower edge of the stabilizer cantilever.

EFFECT: enhanced accuracy of aiming of the guided missile on the target.

2 cl, 7 dwg