GUIDED MISSILE Russian patent published in 2005 - IPC

Abstract RU 2244896 C1

FIELD: armament, in particular, guided missiles.

SUBSTANCE: the guided missile has a control actuator in the nose cone, warhead and a control equipment positioned in the missile body and connected by lines of electric coupling made in the form of bundled conductors with connectors. The control actuator, warhead, control equipment are made in the form of a single unit provided with electric connectors on the outer surface. The lines of electric coupling are located inside the body along the unit outer surface. The missile body is fastened in the rear part of the control surface unit.

EFFECT: improved aerodynamic properties of the missile, simplified construction and manufacturing and assembly methods.

1 dwg

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RU 2 244 896 C1

Authors

Kuznetsov V.M.

Zhukov V.P.

Ermakov V.G.

Eremin S.N.

Dates

2005-01-20—Published

2004-01-08—Filed