发明名称 MISSILE HAVING DEPLOYMENT MECHANISM OF RETRACTABLE STABILIZERS
摘要 FIELD: missile armament, in particular, stabilizers deployed after lauding of the missile. ^ SUBSTANCE: the deployment mechanism automatically turns, about the hinge and deploys the stabilizer from the stowed position to the deployed position. The mechanism has a spring that produces a shifting force making the stabilizer to change the stowed position to the deployed position. ^ EFFECT: simplified consumption and enhanced reliability of the deployment mechanism and fixing of the stabilizers. ^ 10 cl, 15 dwg
申请公布号 RU2320952(C2) 申请公布日期 2008.03.27
申请号 RU20040130842 申请日期 2003.03.14
申请人 REHJTEON KOMPANI 发明人 AJZENTRAUT RUDOL'F ADOL'F;KEBSHULL MARTIN ALLEN;PARIN DZHON KRISTOFER
分类号 F42B10/14;F42B10/60 主分类号 F42B10/14
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