FIELD: antiaircraft rocket weapon, in particular, for individual use.
SUBSTANCE: the device has a support installed on a carrier with components of conjugation and fastening of the launching tube and a clip for additional fastening of the rear part of the launching tube. The support is made of two components and its front component can be hinge-joined to the carrier for provision of its turn in the vertical and horizontal planes. The rear component of the support is adjustable in length, and it carries the guide support installed in which is the clip having the possibility of axial displacement in the support and fixation in the required position. The device is provided with a scanning drive installed on the carrier with the aid of a bracket that can adjust its position relative to the carrier in two mutually perpendicular directions. The outlet wheels of the scanning drive is provided with a self-aligning spherical bearing installed in which is the free end of the rear component of the support with an eccentricity relative to the outlet wheel axle.
EFFECT: enhanced operating characteristics of the launcher.
12 dwg
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Authors
Dates
2007-10-20—Published
2006-02-13—Filed