发明名称 |
JET PROJECTILE |
摘要 |
artillery ammunition. SUBSTANCE: the jet projectile has a nose section combined with the engine. The engine carries a fin with opening blades. The stabilizer casing is made in the form of a thin-walled cylinder consisting of spring blades rolled up in circumference and successively fastened to one another. Each blade is concave towards rolling-up, and the fin casing longitudinal axis is aligned with the projectile longitudinal axis. EFFECT: reduced passive weight of the projectile. 2 dwg
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申请公布号 |
RU2165584(C1) |
申请公布日期 |
2001.04.20 |
申请号 |
RU20000102771 |
申请日期 |
2000.02.03 |
申请人 |
GOSUDARSTVENNOE UNITARNOE PREDPRIJATIE "KONSTRUKTO;RSKOE BJURO PRIBOROSTROENIJA |
发明人 |
KUZNETSOV V.M.;KHRIPUNOV L.A.;DAVYDOV M.N.;MAKHONIN V.V.;KHEL'BERG F.M. |
分类号 |
F42B10/14;(IPC1-7):F42B10/14 |
主分类号 |
F42B10/14 |
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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