| 摘要 |
FIELD: antiaircraft rocket armament. SUBSTANCE: facility to load launcher with rocket in launching tube has fixing pin, rotary lever of pricking mechanism with index pin, socket of electric connector assembly mounted on launching tube and cradles with clamps and locks, plug of electric connector assembly with socket to accommodate fixing pin, mechanism turning lever of launching tube, air-powered motor with extendible rod mounted on frame of launcher. Rod of air-powered motor is hinged to end of crank, the other end of it is put on shaft uniaxially with axle of rotary lever. Moving girder with upper and lower flanges embracing rotary lever and profile protrusion and rest in its upper part is fixed on this shaft. Plug with knife-like shut- off on cheek bordering on moving girder is attached to frame. EFFECT: decreased time for loading of launcher thanks to reduced number of manual operations. 1 cl, 11 dwg
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