FIELD: military equipment.
SUBSTANCE: invention refers to devices ensuring effective work of combat vehicle of multiple artillery rocket systems. Electromechanic locking device for rocket missiles includes two plate locks connected by regulation bolt and nut. The body of breech end of the guiding pipe to the left and right of plate locks we locate additionally two electric magnets spring loaded pits of which block plate locks in the initial position preventing their unclamping by pin of rocket missile. The command to pits to be pressed and plate locks to be released when the rocket missile reaches necessary start effort is sent to electromagnets from board network from the sensor measuring this effort. The sensor is located at one of the plate locks.
EFFECT: increased effectiveness of use of combat vehicle of multiple artillery rocket systems.
1 dwg, 1 dwg
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