GUIDED MISSILE Russian patent published in 1999 - IPC

FIELD: military rocketry. SUBSTANCE: guided missile has a body with guide bands and obturator, electronic control equipment and a power unit with control program selector switches. Control program selector switches with an angle of turn of the change-over cocks equal to 90 deg are assembled with the aid of a strip and bases into a single unit and rigidly fastened to the body in front of its guide band. On the strip, in place of its joint with the body, a recess is made, which is filled with flexibly tightened sealing material and limited by a clamp on the contour of the strip. The strip and the body have aligned holes, which accommodate the tail pieces of the change-over cocks, furnished with flats on their lateral surfaces for turning by a tool, and with location marks on the external end faces parallel to the flats. The flats and location marks are oriented relative to the missile in the extreme positions of the change-over cocks either along, or perpendicularly to the missile longitudinal axis. EFFECT: enhanced reliability and combat readiness of missile, simplified design. 4 dwg