发明名称 |
SOLID-PROPELLANT ROCKET ENGINE |
摘要 |
FIELD: rocketry; solid-propellant rocket engines with inserted powder charges. ^ SUBSTANCE: proposed solid-propellant rocket engine has combustion chamber with front end plate and multi-nozzle unit, inserted powder charge unrestricted over outer surface and igniter with electric primer on front end plate of chamber. Igniter is located in prechamber formed by circular groove in front end plate of chamber and bearing plate with holes smoothly distributed over its edge. Electric primer is inserted into bush with splitter whose holes are directed to igniter. Nozzle end of charge is provided with chamfer. ^ EFFECT: reduced eccentricity of engine thrust due to smooth ignition of charge and efflux of gases from engine. ^ 2 dwg |
申请公布号 |
RU2297547(C1) |
申请公布日期 |
2007.04.20 |
申请号 |
RU20050126700 |
申请日期 |
2005.08.23 |
申请人 |
GOSUDARSTVENNOE UNITARNOE PREDPRIJATIE "KONSTRUKTORSKOE BJURO PRIBOROSTROENIJA" |
发明人 |
BOL'SHAKOV ANATOLIJ NIKOLAEVICH;KREJER KONSTANTIN VJACHESLAVOVICH;KHUDJAKOV VLADIMIR IVANOVICH;SHATROVA EHMILIJA ALEKSEEVNA |
分类号 |
F02K9/95 |
主分类号 |
F02K9/95 |
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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