发明名称 METHOD OF GUIDED MISSLE LAUNCH
摘要 FIELD: weapon. ^ SUBSTANCE: invention relates to missile munitions. The method of guided missile launch includes targeting of the missile, increase of its length due to impulse boost and further inertial shift of its head and firing the missile. The head of the missile is made from telescopically shifted members. The length of the missile is shifted due to their sequential shifting, breaking and fixation with decrease of the total weight. ^ EFFECT: decrease of pre-launch indignations effected the missile and launcher with providing higher length of the missile. ^ 4 dwg
申请公布号 RU2358232(C2) 申请公布日期 2009.06.10
申请号 RU20070125318 申请日期 2007.07.04
申请人 GOSUDARSTVENNOE UNITARNOE PREDPRIJATIE "KONSTRUKTORSKOE BJURO PRIBOROSTROENIJA" 发明人 STEPANICHEV IGOR' VENIAMINOVICH;GUSEV ANDREJ VIKTOROVICH;FIMUSHKIN VALERIJ SERGEEVICH;OVCHELUPOV NIKOLAJ VASIL'EVICH;GALKIN VIKTOR NIKOLAEVICH
分类号 F42B15/00 主分类号 F42B15/00
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