发明名称 MISSILE
摘要 FIELD: weapons and ammunition.SUBSTANCE: missile includes case in the form of connected separable joint units with pyrotechnical burst connection of sealed head compartment with a sequence of homing head, inertial control system, ammunition, active thermal protection system and independent fluid or paste fuel propeller containing fuel with oxidiser and liquid-propellant rocket engine set with longitudinal nozzle, four liquid-propellant rocket engines with transverse nozzles and four liquid-propellant rocket engines generating head compartment torque, and propeller compartment with aerodynamic rudders, rudder drives, double-pulse solid fuel propeller aggregate, second pulse timing unit, correction unit.EFFECT: efficient striking of high-altitude targets.3 cl, 4 dwg
申请公布号 RU2548957(C1) 申请公布日期 2015.04.20
申请号 RU20140119586 申请日期 2014.05.15
申请人 OTKRYTOE AKTSIONERNOE OBSHCHESTVO "GOSUDARSTVENNOE MASHINOSTROITEL'NOE KONSTRUKTORSKOE BJURO "VYMPEL" IM. I.I. TOROPOVA" 发明人 BOGATSKIJ VLADIMIR GRIGOR'EVICH;SMIRNOV ANATOLIJ GEORGIEVICH;ORELIOV GRIGORIJ RAFAILOVICH;MYNKIN VLADIMIR ALEKSANDROVICH
分类号 F42B15/00 主分类号 F42B15/00
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