| 发明名称 |
SPINNING MISSILE |
| 摘要 |
FIELD: weapons and ammunition. ^ SUBSTANCE: spinning missile comprises warhead with a cylindrical case containing a fluid filler and an air chamber and a rod being arranged on the spinning missile symmetry axis. The missile also comprises a missile aerodynamic stabilizer with canted fins and a gas-dynamic angular stabilization system with nozzles. The air chamber volume is from 0.2 to 0.05 of the cylindrical body volume, and the distance between the centre of mass of the spinning missile and the centre of mass of the warhead does not exceed a value determined by the given mathematical expression. ^ EFFECT: enhancement of fire engagement. ^ 1 dwg |
| 申请公布号 |
RU2325612(C1) |
申请公布日期 |
2008.05.27 |
| 申请号 |
RU20060131766 |
申请日期 |
2006.09.04 |
| 申请人 |
FEDERAL'NOE GOSUDARSTVENNOE UNITARNOE PREDPRIJATIE "GOSUDARSTVENNOE NAUCHNO-PROIZVODSTVENNOE PREDPRIJATIE "SPLAV" |
发明人 |
MAKAROVETS NIKOLAJ ALEKSANDROVICH;DENEZHKIN GENNADIJ ALEKSEEVICH;SEMILET VIKTOR VASIL'EVICH;KALJUZHNYJ GENNADIJ VASIL'EVICH;BELOBRAGIN BORIS ANDREEVICH;SHIROKOV VLADIMIR VASIL'EVICH;TEREKHOV BOGDAN NIKOLAEVICH;VARENYKH NIKOLAJ MIKHAJLOVICH;SPORYKHIN ALEKSANDR IVANOVICH |
| 分类号 |
F42B15/00;F42B10/02;F42B12/02 |
主分类号 |
F42B15/00 |
| 代理机构 |
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