GUIDING DEVICE FOR MISSILE LAUNCHING Russian patent published in 2005 - IPC

Abstract RU 2246679 C1

FIELD: armament, in particular, missile complexes.

SUBSTANCE: the guiding device has a launching tube, device for missile roll twist made in the form of lugs on the missile body engageable with the inner surface of the launching tube, and plate springs fastened in cantilever to the missile body generating line. A ring-shaped flange is installed on the rear end of the launching tube, it has a bore and grooves, in which the tops of the lugs are located with a stop at their end face surfaces, the lugs have sharpened edges turned relative to the missile longitudinal axis through the twist angle. The lugs are positioned in the center of the springs, and a ring with a stop at the end face surface of the lugs is installed in the bore.

EFFECT: expanded functional potentialities of the guiding device for missile launching, enhanced reliability of it.

3 dwg

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RU 2 246 679 C1

Authors

Kuznetsov V.M.

Zhukov V.P.

Rasskazov A.V.

Dates

2005-02-20Published

2004-01-19Filed