SPIN-STABILIZED MISSILE PACK HEAD Russian patent published in 1997 - IPC

FIELD: rocketry. SUBSTANCE: the pack head has a master controller, body, frame with war elements and separation assemblies. To reduce impact and vibratory overloads, the head is furnished with a separation and attitude control device. After actuation of this device the head is jettisoned and its stabilization is ensured due to the attitude control system. As a result of operation of the propelling charge of the pack head, the lock-on connection is actuated, which results in removal of the rigid mounting of the adapter ring to the frame front disk and body at minimum allowable overloads. After the frame comes out of the body the retarding device in turn generate pulses to the ignition charges of the separation engines. When the necessary pressure is attained in the engine chambers, the flexible bands in the zone of the engine nozzle openings get destructed, and the war elements are separated at the minimum vibratory and impact loads. On completion of operation of the separation engine impactless separation of the war element occurs due to the fact that one end of the wire rope is secured on the intermediate diaphragm, and the other end - on the separation engine. The war element positioned on the front disk is ejected from the frame due to the flexible members. Its ejection occurs after separation of the next war element, which holds the free plate with the retainer. EFFECT: improved design. 6 cl, 11 dwg