发明名称 |
ANTIAIRCRAFT GUIDED MISSILE |
摘要 |
FIELD: rocketry. SUBSTANCE: missile has interconnected zero and sustainer stages. The sustainer stage case is made in the form of a thin-walled envelope connected to the nose fairing. The functional units and live ammunition interconnected in axial direction are located inside the envelope. Part of the envelope around the live ammunition is made as an additional mass of warhead hitting components. EFFECT: enhanced stiffness of sustainer stage airframe, reduced overall dimensions and mass, improved aeroballistic characteristics of missile. 2 cl, 2 dwg
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申请公布号 |
RU2133446(C1) |
申请公布日期 |
1999.07.20 |
申请号 |
RU19980111140 |
申请日期 |
1998.06.09 |
申请人 |
SKOE BJURO PRIBOROSTROENIJA;G UNITARNOE PREDPRIJATIE KONST |
发明人 |
KUZNETSOV V.M.;EHNTIN A.P.;FERULENKOV A.V.;GORBUNOV B.A.;TRESHCHEV I.L.;MAKHONIN V.V. |
分类号 |
F42B15/10;(IPC1-7):F42B15/10 |
主分类号 |
F42B15/10 |
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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