GUIDED MISSILE Russian patent published in 2001 - IPC

FIELD: jet-propelled ammunition. SUBSTANCE: guided missile has a body, nose cone, homing head and control equipment that are electrically interconnected with the aid of contacts located in the sockets of the control equipment and pins of the homing head, fixed relative to one another by guide pins installed in parallel with the missile axis, and with their joint surfaces are positioned in the front hole of the nose cone. The control equipment is rigidly attached to the nose cone by means of screws and threaded ears made on the inner surface of the nose cone, and the homing head - by means of union nut and thread on its external surface. EFFECT: enhanced reliability of guided missile, simplified construction. 3 cl, 1 dwg