发明名称 GUIDES MISSILE
摘要 FIELD: armament. ^ SUBSTANCE: the guide missile has a body with a blunt nose section of low lengthening, fin unit, control surfaces located on the body nose section. The missile body is made with a additional withdrawable nose section of a lower diameter. The ratio of the diameters of the with drawable nose section and the body makes up 0.4 to 0.7. The ratio of the summary length of the main nose section and the withdrawal one and the body diameter makes up 2.0 to 3.0. ^ EFFECT: enhanced efficiency of missile control. ^ 5 dwg
申请公布号 RU2302606(C1) 申请公布日期 2007.07.10
申请号 RU20050140896 申请日期 2005.12.26
申请人 GOSUDARSTVENNOE UNITARNOE PREDPRIJATIE "KONSTRUKTORSKOE BJURO PRIBOROSTROENIJA" 发明人 SHIPUNOV ARKADIJ GEORGIEVICH;STEPANICHEV IGOR' VENIAMINOVICH;MOROZOV VLADIMIR IVANOVICH;GOLOMIDOV BORIS ALEKSANDROVICH;GUSAROV NIKOLAJ IVANOVICH
分类号 F42B15/00 主分类号 F42B15/00
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