GUIDED MISSILE IN LAUNCHING PACK Russian patent published in 2005 - IPC

FIELD: armament.

SUBSTANCE: the guided missile in a transport-launching pack has control surfaces installed in the horizontal plane, booster and propulsion engines, stabilizer unit consisting of flexible cantilevers combined around the body, a flare installed in the plane passing through the axis of the pack and the longitudinal axis of the flare and shifted from the vertical plane of symmetry. The angles of displacement of the planes of installation of the flare and control surfaces from the vertical plane of symmetry on the side of the missile trailing edge assembly are within 50 to 70 degrees in the counter-clockwise direction, and within 30 to 60 degrees in the clockwise direction respectively. The flare mass makes up 0.0075 to 0.015 of the missile mass.

EFFECT: enhanced probability of introduction of the guided missile in the field of vision of the guided missile instrument in the initial leg of the flight.

9 dwg