发明名称 CONTROLLED MISSILE
摘要 FIELD: weapons and ammunition. ^ SUBSTANCE: missile comprises cruise solid propellant jet engine with side nozzles and combat part attached to it. Body of combat part is made of thin-walled aluminium shell with windows opposite to output sections of cruise engine nozzles. Nozzles of cruise engine are arranged within the limits of inner diametre of combat part body. L-shaped heat resistant pads are installed between end surface of nozzles and body of combat part. They interact by their one shelf with end surface of cruise engine nozzles, and by the other one - with external surface of combat part body. Width of pad is more than width of hole opposite to output sections of cruise engine nozzles. In shelf there are slots arranged, which interact with outer and inner surfaces of combat part body. L-shaped heat resistant pads are made of low-carbon structural steel. ^ EFFECT: improved reliability and manufacturability of controlled missile production due to provision of strong and manufacturable joint of cruise engine with side nozzles and combat part and elimination of combat part body overheating by gases. ^ 4 dwg, 2 cl
申请公布号 RU2393421(C1) 申请公布日期 2010.06.27
申请号 RU20080143773 申请日期 2008.11.05
申请人 GOSUDARSTVENNOE UNITARNOE PREDPRIJATIE "KONSTRUKTORSKOE BJURO PRIBOROSTROENIJA" 发明人 DRIZGALOVICH EVGENIJ MIKHAJLOVICH;ZAKHAROV LEV GRIGOR'EVICH;KOPYLOV JURIJ DMITRIEVICH;PARFENOV PAVEL PETROVICH
分类号 F42B15/00 主分类号 F42B15/00
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