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

FIELD: armament.

SUBSTANCE: the guided missile has a body with a warhead fastened to its front end, control equipment module fastened in the rear end of the missile body, and an electric wire bundle with a compensator of longitudinal motions. The warhead has a telescope joint to the control equipment module by means of a cylindrical bush that is fastened to the control equipment module by radial pins. The bush and the warhead are fixed to each other by a cut component, whose breaking force is less than the cutting force of the pins. The length of the telescope fit of the cylindrical bush exceeds the linear elongation of the missile body at a kinetic heating.

EFFECT: enhanced maneuverability of the missile.

2 dwg