ARRESTING DEVICE OF MISSILE LAUNCHER GUIDE Russian patent published in 2005 - IPC

FIELD: rocketry, applicable in production of anti-hail missile complexes.

SUBSTANCE: the arresting device of the missile launcher guide has arresting components positioned on the cut of the breech end of the guide and side surface of the nozzle unit of the missile. The first arresting component has the front and rear stops, between a through duct is formed, in which an arresting pin is enclosed located on the side surface of the missile nozzle unit. The arresting pin fixes the missile in the duct of the guide and is cut off by the front stop at missile launching.

EFFECT: simplified design of the arresting device, reduced labor consumption in service, as well as enhanced reliability and efficiency in operation.

3 cl, 5 dwg