SYSTEM OF PAYLOAD DISENGAGEMENT Russian patent published in 2010 - IPC B64G1/10 

FIELD: aerospace engineering.

SUBSTANCE: proposed system comprises split retainer device with locks and pyrotechnical gadget arranged between bearing structure and payload, and pushers with spring-loaded rods for payload disengagement arranged in bearing structure. The system carries endless tensioned rope enveloping block-rollers arranged along periphery of bearing structure. Every pusher rod is articulated with aforesaid rope via bell crank fitted on pusher casing. Bell crank one arm is connected with the rope, the other one is coupled, via pinot link, with spring-loaded rod.

EFFECT: higher accuracy and reliability of disengagement.

2 cl, 6 dwg