The invention relates to the technical field of satellites, in particular to a stackable satellite protection device which comprises a satellite body and a solar wing, the solar wing is arranged on the side wall of the satellite body, a protection assembly is arranged on the solar wing and used for protecting the solar wing, and the protection assembly comprises a protection frame. The protection frames are connected to the peripheral side walls of the solar wings, the multiple protection frames are arranged corresponding to the solar wings, the multiple protection frames are connected with one another, and the protection frames can be arranged in a stacked mode. The problem that the solar wing is damaged by vibration in the lift-off process is solved.

    本申请涉及卫星的技术领域,尤其涉及一种可堆叠卫星防护装置,其包括卫星主体和太阳翼,所述太阳翼设置在所述卫星主体的侧壁上,所述太阳翼上设置有防护组件,所述防护组件用于对所述太阳翼进行防护,所述防护组件包括防护框架,所述防护框架连接在太阳翼的周侧壁上,所述防护框架对应所述太阳翼设置有多个,多个防护框架相互连接,所述防护框架可堆叠设置。本申请改善了在升空的过程中太阳翼受震动损坏的问题。


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    Titel :

    Stackable satellite protection device


    Weitere Titelangaben:

    一种可堆叠卫星防护装置


    Beteiligte:
    DING BEN (Autor:in) / SUN SHOUJIA (Autor:in) / CAI DAZHEN (Autor:in) / ZHU ZHENGXIAN (Autor:in) / XU ZHI (Autor:in)

    Erscheinungsdatum :

    05.12.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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