GUIDED MISSILE SYSTEM Russian patent published in 2009 - IPC F41F3/00 

FIELD: weapons.

SUBSTANCE: present invention pertains to military technology, particularly to antitank missile systems. The guided missile system has a launching stand, in the front and rear guides of which there are grooves for linkage with ledges of front and rear guides of the cradle, a shock absorber and container with discharge, electrically connected to the launch control equipment. The container has a front pile ring and a rear pile ring with an electrical connector, which is fitted in the groove of the rear guide of the launching stand. In the front guide of the launching stand there are parallel grooves, symmetrically arranged relative each other, into which fit ledges of the front guides of the cradle and the front pile ring of the container. The latter are fastened together with provision for axial displacement when the missile is launched. The shock absorber is fitted in the cradle, lying between two supports, fixed on the launching stand, and its axis coincides with the axis of the pile ring of the discharge container.

EFFECT: increase in efficiency of the missile system, its reliability and cutting on time for changing over from travelling position to firing position, and provision for possibility of installing the missile system on self-powered carriers.

2 cl, 10 dwg