MECHANISM FOR RETENTION OF MISSILE IN LAUNCHING TRANSPORTING CONTAINER Russian patent published in 2015 - IPC F42B15/00 

FIELD: weapons and ammunition.

SUBSTANCE: invention relates to missile engineering and is intended to be used in rockets launched from a launching transporting container. The design of the retention mechanism assembly represents a bracket, on which a limit stop, a turnbuckle and a grip arranged on the rotation axis in the front part of the retention mechanism bracket are mounted. The grip design has an attachment axis of the turnbuckle serving as a fastening element of the grip design with a flag, by means of which the rear face of the rocket is held down to the limit stop of the retention mechanism. The flag design has a rotation axis fixed on the bracket. In the zone of the rotation axis in the flag there is a T-slot for fixation of the turnbuckle; on the opposite side there is a platform with holes for attachment of a fastening plate. The fastening plate attaches flags of two assemblies of the retention mechanism.

EFFECT: achievement of reliable fixation at transportation, and minimum disturbances at start-up at the moment of the plate burnout.

4 cl, 4 dwg