发明名称 LIQUID PROPELLANT ROCKET
摘要 FIELD: engines and pumps.SUBSTANCE: invention relates to jet machinery. Liquid-propellant engine comprises engine chamber, turbine, fuel pump and jet pre-pump and differs from known designs in that jet pre-pump injection nozzle communicates with turbine inlet or outlet or with chamber cooling circuit.EFFECT: higher efficiency of jet pre-pumps.3 dwg
申请公布号 RU2506444(C1) 申请公布日期 2014.02.10
申请号 RU20120121131 申请日期 2012.05.22
申请人 EFIMOCHKIN ALEKSANDR FROLOVICH;VOVCHARENKO KONSTANTIN IVANOVICH;ELISEEV ALEKSANDR VLADIMIROVICH 发明人 EFIMOCHKIN ALEKSANDR FROLOVICH;VOVCHARENKO KONSTANTIN IVANOVICH;ELISEEV ALEKSANDR VLADIMIROVICH
分类号 F02K9/46 主分类号 F02K9/46
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