GUIDED MISSILE Russian patent published in 1999 - IPC

Abstract RU 2127417 C1

FIELD: rocketry. SUBSTANCE: guided missile has the leading shaped charge and the main warhead with safety-and- actuating mechanisms, as well as the control actuator unit with coils of the polarized control electromagnet, and coil of two-wire communication line. The communication line coil is connected to the beginnings of the coils of the control electromagnet of the control actuator unit, and the ends of these coils are combined by a jumper and parallel- connected to the safety-and actuating mechanisms of the leasing shaped charge and the main warhead. EFFECT: enhanced reliability of the safety-and-actuating mechanisms and the missile on the whole. 2 dwg

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RU 2 127 417 C1

Authors

Shipunov A.G.

Tikhonov V.P.

Zakharov L.G.

Zybin I.M.

Boev I.V.

Dates

1999-03-10Published

1998-02-16Filed