GUIDED MISSILE Russian patent published in 2001 - IPC

FIELD: jet ammunition. SUBSTANCE: the missile has a body, power unit with a yoke and thermoelectric batteries placed in its seats, and a gyroscope, whose electric pins are connected to the communication board installed in the joint of the power unit and body. The seats in the yoke of the power unit are made in the form of stepped through holes whose steps are located in the same plane, perpendicular to the missile axis. The ends of the thermoelectric batteries and gyroscope are fastened on the supporting steps of the yoke seats, and their electric pins are soldered in the contracts holes of flexible printed circuit boards, whose leads are bent and brought out through the edge of the communication board to its external surface facing the missile body, fastened to it and soldered to the electric pins installed on the board with the aid of the contact holes. The flexible printed circuit boards are fastened on the yoke with the aid of a shield through a soft insulating pad, and pads of an electric insulator with holes for the battery pins are positioned between the ends of the thermoelectric batteries and flexible printed circuit boards. EFFECT: reduced labor content of electric wiring due to simplified design, enhanced reliability of missile functioning. 5 dwg