发明名称 |
SOLID-PROPELLANT ROCKET ENGINE |
摘要 |
FIELD: rocketry; solid-propellant engines. ^ SUBSTANCE: invention can be used at designing, developing and manufacturing of solid-propellant rocket engines. Proposed rocket engine contains body with fitted-in insert channel unrestricted burning charge and igniter arranged from side of charge front end face. Thin-walled diaphragm made of combustible material is installed behind rear end face of charge. Through cuts are made over periphery of diaphragm. ^ EFFECT: improved reliability of ignition of solid-propellant charge, and weight-and-dimension and performance characteristics of solid-propellant rocket engine. ^ 2 cl, 4 dwg
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申请公布号 |
RU2286475(C2) |
申请公布日期 |
2006.10.27 |
申请号 |
RU20050100546 |
申请日期 |
2005.01.11 |
申请人 |
FEDERAL'NOE GOSUDARSTVENNOE UNITARNOE PREDPRIJATIE "NAUCHNO-ISSLEDOVATEL'SKIJ INSTITUT POLIMERNYKH MATERIALOV" |
发明人 |
KOZ'JAKOV ALEKSEJ VASIL'EVICH;MOLCHANOV VLADIMIR FEDOROVICH;KOLESNIKOV VITALIJ IVANOVICH;NIKITIN VASILIJ TIKHONOVICH |
分类号 |
F02K9/32 |
主分类号 |
F02K9/32 |
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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