发明名称 |
CONTROLLED MISSILE |
摘要 |
FIELD: weapons and ammunition.SUBSTANCE: invention relates to missile engineering, namely to controlled missiles. A controlled missile includes a housing with the main control elements symmetrically arranged on it - aerodynamic surfaces and rudders, as well as a wire duct. The latter is arranged along the housing in the incline of rudders. An aerodynamic surface is additionally installed on the housing, on the side opposite to the wire duct.EFFECT: improvement of aerodynamics of missile flight and improvement of its target guidance accuracy.2 cl, 1 dwg |
申请公布号 |
RU2539709(C1) |
申请公布日期 |
2015.01.27 |
申请号 |
RU20140101679 |
申请日期 |
2014.01.22 |
申请人 |
OTKRYTOE AKTSIONERNOE OBSHCHESTVO "GOSUDARSTVENNOE MASHINOSTROITEL'NOE KONSTRUKTORSKOE BJURO "VYMPEL" IMENI I.I. TOROPOVA" |
发明人 |
BOGATSKIJ VLADIMIR GRIGOR'EVICH;KRAVCHUK ALEKSANDR PAVLOVICH;LEVISHCHEV OLEG NIKOLAEVICH;ORELIOV GRIGORIJ RAFAILOVICH;SMIRNOV ANATOLIJ GEORGIEVICH |
分类号 |
F42B15/00;F42B10/60;F42B10/62;F42B10/64;F42B15/01 |
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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