ROCKET LAUNCHER Russian patent published in 2004 - IPC

FIELD: armament, in particular, rocket launchers.

SUBSTANCE: the rocket launcher has a base, bank of launching tubes movable for orientation in elevation angle and azimuth, driving unit made in the form of two drive-hinges coupled by rotary links, their axes don't intersect and are positioned relative to each other at a right angle. The body of one of them is linked with the bank of launching tubes, and the body of the other - with the base of the launcher, and its is positioned in parallel with the base. The launching tubes are positioned in the form of a cone, whose axes converge in a fan-shaped manner in the center of the driving unit.

EFFECT: reduced impact momentary load on the driving unit.

6 dwg