METHOD FOR CONTROL OF MISSILE FLIGHT DIRECTION AND MISSILE Russian patent published in 2006 - IPC F42B15/01 F42B10/66 

FIELD: means for control of missile flight direction.

SUBSTANCE: the missile has a control system of missile flight direction, which includes a set of barrel assemblies from which the missiles are launched selectively. Each assembly of barrel; has a great number of missiles arranged in the axis in the barrel and linked with the respective propellant charges for movement of the mentioned missiles in succession in the barrel. Some of the barrels in the set of the barrel assemblies are oriented for provision of the direction of movement in the longitudinal axis of the missile for the respective missiles. In another modification some of the barrels in the set are arranged mainly behind the missile center of gravity for adjustment of the missile flight altitude and trajectory by a random launching of missiles.

EFFECT: enhanced missile maneuverability.

12 cl, 4 dwg