发明名称 GUIDING DEVICE FOR MISSILE LAUNCHING
摘要 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
申请公布号 RU2246679(C1) 申请公布日期 2005.02.20
申请号 RU20040101454 申请日期 2004.01.19
申请人 发明人 KUZNETSOV V.M.;ZHUKOV V.P.;RASSKAZOV A.V.
分类号 F41F3/04 主分类号 F41F3/04
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