• 文中报告了特种发动机燃烧室压力混合推进剂温度喷注结构燃烧过程影响计算分析结果

    The results of the calculation and the analysis of effects of combustion chamber pressure, mixture ratio, propellant injection temperature and injector type on the combustion processes are reported.

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  • 固体推进剂发动机系统的可调性基本上液体混合的要差。

    Solid propellant engine systems are basically less flexible in operation than liquid or hybrid propellant systems.

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  • 固体推进剂发动机系统的可调性基本上液体混合的要差。

    Solid propellant engine systems are basically less flexible in operation than liquid or hybrid propellant systems.

    youdao

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