GUIDED MISSILE Russian patent published in 1999 - IPC

Abstract RU 2125230 C1

FIELD: missile armament. SUBSTANCE: guided missile has a leading shaped charge and the main shaped-charge warhead. A control actuator unit and an engine with a central tube are located between them; the central tube accommodates a distributor with control electromagnet. The distance between the front end of the shaped-charge funnel of the main warhead and rear end of the engine equals to 1.3 to 2.8 of the diameter of the shaped-charge funnel of the main warhead. The engine frame serves as a protective partition, and its optimum arrangement prevents destruction of the shaped-charge funnel of the main warhead at operation of the leading shaped-charge. EFFECT: enhanced armour-piercing of targets fitted with dynamic protection. 1 dwg

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RU 2 125 230 C1

Authors

Shipunov A.G.

Zakharov L.G.

Zybin I.M.

Filimonov G.D.

Dates

1999-01-20Published

1998-01-27Filed