MISSILE Russian patent published in 2006 - IPC F42B15/00 

Abstract RU 2284458 C1

FIELD: armament.

SUBSTANCE: the missile has a stabilizer unit in the form of a body with hinge-fastened blades, spring locks installed for engagement with the blade bases. The locks are made in the form of spring beams with the bearing surfaces at the ends, they are fastened to the body between the bearing surfaces. In the points of engagement with the locks the blade bases are made in the form of cylinders, whose axes are the folding axes of the blades. The rear part of the missile body behind the stabilizer blades is made in the form of a tapered skirt, whose vertex faces the missile nose. Besides, the rear part is provided with a cylindrical surface equal to the diameter of the missile outer body.

EFFECT: enhanced operating characteristics of the missile.

7 dwg

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RU 2 284 458 C1

Authors

Kuznetsov Vladimir Markovich

Zhukov Vladimir Petrovich

Korneichev Aleksandr Vjacheslavovich

Dates

2006-09-27Published

2005-02-17Filed