FIELD: the invention refers to rocket launchers precisely to arrangements for fastening rockets on launchers.
SUBSTANCE: the essence of the invention in that the body of the arrangement is fulfilled in the shape of a bushing. Its inner diameter exceeds the diameter of the tail part of the projectile. The limiter of axial movement of the body is fulfilled in the shape of the unit of a hold-down of the bushing's face to the breech face of the launcher. Besides mentioned unit has as minimum three locking units which locking devices have possibility of mounting on the guide and interaction with responsive elements on the outside surface of the bushing. Responsive elements are fulfilled in the shape of a flange.
EFFECT: the invention increases reliability of the work of the arrangement and the launcher as a whole.
3 cl, 2 dwg
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Authors
Dates
2005-07-10—Published
2004-02-24—Filed