GUIDED MISSILE Russian patent published in 2001 - IPC

Abstract RU 2164657 C1

FIELD: high-accuracy guided missile weaponry. SUBSTANCE: the guided missile has control and booster units. The control unit is made in the form of a nose module with a homing head and missile controls and a real module rigidly attached to the nose cone of the booster unit by the mounting seat. The modules are interconnected by a cylindrical hinge joint, whose axis of rotation coincides with the longitudinal axis of the booster unit. EFFECT: expanded field of combat employment of guided missiles up to destruction of movable targets. 6 cl, 3 dwg

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RU 2 164 657 C1

Authors

Efremov G.A.

Burganskij A.I.

Khomjakov M.A.

Lavrenov A.N.

Bol'Shakov M.V.

Dates

2001-03-27—Published

1999-10-06—Filed