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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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