• Both the structure and the use of solid rocket motor case skirts are presented. The advantages of the composite skirts are introduced.

    介绍了固体火箭发动机壳体结构用途及采用复合材料裙体优点

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  • The burst pressure of filament wound pressure vessels which is applied to solid rocket motor case and gas tank in industry is an important design parameter.

    用于固体火箭发动机壳体工业贮罐纤维缠绕压力容器爆破压强重要设计参数

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  • The liner is a polymeric elastomer coating between propellant and insulation layer or case. The liner-forming is a special step in production of solid rocket motor.

    推进剂绝热层壳体之间高分子弹性体涂层,衬层成型是固体火箭发动机生产中的一种特种工序

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  • The effect of radial vibration of the chamber structure composed of propellant grain and case on the internal ballistic property of solid rocket motor (SRM) was investigated.

    研究推进剂药壳体组成燃烧室结构径向振动对发动机弹道性能影响

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  • This paper deals with the study of the external thermal insulation coating for a solid rocket motor (SRM) case.

    介绍固体发动机壳体外防涂层研究情况

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  • This paper deals with the study of the external thermal insulation coating for a solid rocket motor (SRM) case.

    介绍固体发动机壳体外防涂层研究情况

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