The invention provides a flexible ball spacecraft inflation unfolding structure evaluation method, which can evaluate the rationality and reliability of the inflatable unfolding structure of the flexible ball spacecraft. The method relates to flexible ball spacecraft test conditions, installation bearing modes and flexible ball inflation unfolding process monitoring, the inflation unfolding function of the flexible ball spacecraft can be verified, and then the inflation unfolding structure of the flexible ball spacecraft is evaluated.

    本发明提供了一种柔性球航天器充气展开结构评估方法,能够评估柔性球航天器充气展开结构的合理性、可靠性。涉及柔性球航天器试验条件、安装承载方式以及柔性球充气展开过程监测,可以验证柔性球航天器的充气展开功能,进而对柔性球航天器充气展开结构进行评估。


    Access

    Download


    Export, share and cite



    Title :

    Flexible ball spacecraft inflation unfolding structure evaluation method


    Additional title:

    一种柔性球航天器充气展开结构评估方法


    Contributors:
    WANG HU (author) / ZHANG KAIFENG (author) / LI LIN (author) / ZUO HUAPING (author) / CAO SHENGZHU (author) / LI XUELEI (author) / HAO HONG (author) / LUO SHUILIAN (author) / GAO HENGJIAO (author) / WANG ZHIMIN (author)

    Publication date :

    2021-04-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS



    Flexible hinge unfolding mechanism for spacecraft solar array

    KE MIN / ZHANG BO / LUO ZHIHUI et al. | European Patent Office | 2023

    Free access

    Unfolding mechanism and spacecraft

    ZHENG HAO / JIN YAFANG / NI JIAWEI et al. | European Patent Office | 2025

    Free access

    Folding and unfolding method of inflatable reentry deceleration flexible unfolding structure

    LIAO HANG / CAO XU / WANG LIWU et al. | European Patent Office | 2020

    Free access

    Telescopic folding and unfolding mechanism for spacecraft and spacecraft

    MU MENGLIANG / GAO ENYU / KONG LINGBO et al. | European Patent Office | 2025

    Free access

    Space unfolding variable configuration mechanism and spacecraft

    ZHANG HE / SI XIANFENG / LIU FEI et al. | European Patent Office | 2023

    Free access