| 发明名称 |
LIQUID-PROPELLANT ROCKET ENGINE THRUST UNIT |
| 摘要 |
FIELD: transport.SUBSTANCE: invention relates to rocketry. Liquid-propellant rocket engine thrust unit comprises frame, combustion chamber with nozzle and thrust unit protection device with bottom shields. Said thrust unit protection device incorporates extra frame thermal protection device composed of combustion chamber wall cooler with channels communicating with channels feed one of fuel components to het chamber.EFFECT: higher reliability.1 dwg |
| 申请公布号 |
RU2502645(C2) |
申请公布日期 |
2013.12.27 |
| 申请号 |
RU20110145928 |
申请日期 |
2011.11.11 |
| 申请人 |
OTKRYTOE AKTSIONERNOE OBSHCHESTVO "URAL'SKIJ NAUCHNO-ISSLEDOVATEL'SKIJ INSTITUT KOMPOZITSIONNYKH MATERIALOV" |
发明人 |
NIKITIN VLADIMIR VIKTOROVICH;SHIRJAEV MIKHAIL IVANOVICH;UDINTSEV PETR GENNAD'EVICH;CHUNAEV VLADIMIR JUR'EVICH;MIRONOV VADIM VSEVOLODOVICH;KOSHLAKOV VLADIMIR VLADIMIROVICH;FEDOTOV JURIJ DMITRIEVICH |
| 分类号 |
B64G1/52;B64G1/40;F02K9/64 |
主分类号 |
B64G1/52 |
| 代理机构 |
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