GUIDED ANTI-AIRCRAFT MISSILE Russian patent published in 2001 - IPC

Abstract RU 2167389 C1

FIELD: rocketry. SUBSTANCE: guided anti- aircraft missile has zero and sustainer stages. The sustainer stage body accommodates the warhead and the functional units. Made on the inner surface of the sustainer stage body, over the warhead, are annular grooves, installed in one of which is a spring nut, and in other - a key in the form of a spring ring with a profile of a rectangular trapezoid. The key rests on the annular groove on the warhead body, which obliquely changes into a groove of a smaller diameter with an undercutting in the form of tooth. The acute angle of the undercutting corresponds to the acute angle of the key profile. The spring nut is installed for engagement with the threaded bush pressing the end of the warhead. EFFECT: prevented motion of the warhead and functional units in the sustainer stage body in service of the missile. 4 dwg

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RU 2 167 389 C1

Authors

Kuznetsov V.M.

Kapustin A.S.

Ferulenkov A.V.

Gorbunov B.A.

Ehntin A.P.

Makhonin V.V.

Dates

2001-05-20—Published

2000-03-06—Filed