发明名称 CLUSTER NOSE CONE OF SPIN-STABILIZED MISSILE IN LOADING WITH LIQUID FILLER
摘要 military equipment, in particular missiles, may be used in development of spin-stabilized missiles, jet projectiles of salvo-fire systems inclusive. SUBSTANCE: in the cluster nose cone of the spin-stabilized missile, having a body accommodating the war components with gas vents assembly for moving apart the war components and a master unit, the war components are loaded with a liquid filler, have cylindrical diameters equal to the inside diameter of the nose cone body, are interconnected in a spaceless relation by split U-section rings having a diameter equal to the diameter of the war components, and cavities communicating with the gas vents are made on the ends. The assembly for moving apart the war components is provided with a boost and bursting charges located in the nose and bottom compartments of the nose cone body respectively, the boost charge is electrically coupled to the master unit, and the elongation of the war component is selected with due account made for the nose cone caliber and viscosity of the liquid filler. EFFECT: enhanced efficiency of target hit by 3-4 times, enhanced accuracy of fire by 20 to 30%. 2 dwg
申请公布号 RU2179298(C1) 申请公布日期 2002.02.10
申请号 RU20010104474 申请日期 2001.02.20
申请人 GOSUDARSTVENNOE UNITARNOE PREDPRIJATIE "GOSUDARSTV";GOSUDARSTVENNOE UNITARNOE PREDPRIJATIE ZAVOD "EHLASTIK";GUP ZD EHLASTIK 发明人 AKEL'EV A.I.;BELOBRAGIN B.A.;BEZNOSOV V.I.;GRIGOROV S.I.;DENEZHKIN G.A.;DMITRIEV B.A.;MAKAROVETS N.A.;MALAKHOV A.N.;OBOZOV L.I.;ROMANOVTSEV B.M.;KHOMITSEVICH A.M.
分类号 F42B12/44;(IPC1-7):F42B12/44 主分类号 F42B12/44
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