A boxboard type lunar exploration micro-nano satellite supporting structure comprises two vertically and oppositely arranged main bearing structure frames, side plates vertically arranged outside the main bearing structure frames in four directions, a bottom plate and a top plate oppositely arranged outside the main bearing structure frames, and an adapter bracket arranged below the bottom plate, wherein the two main bearing structure frames are arranged oppositely by being connected and matched with the top plate and the bottom plate to form a main bearing structure of the boxboard type lunar exploration micro-nano satellite, the upper surface of the adapter bracket is connected with the satellite through the separation release mechanism, and the lower surface of the adapter bracket is mounted on the carrier in an insulated and heat-insulated manner; a plurality of reinforcing ribs are arranged on the inner wall of the main body bearing structure in the vertical horizontal direction and used for fixing the in-satellite comprehensive electronic stack module and/or reinforcing the whole structure. Through the adoption of the through type design, a sufficient internal space is provided on the premise of ensuring the structural stability of the whole satellite and the precision of external enveloping, the processing and the assembly are simple, the structure is reliable, the internal space is coherent, and the diversified layout of the satellite and the wide selection of functional components are convenient to meet.

    一种箱板式探月微纳卫星支撑结构,包括:两个竖直相对设置的主承力结构框架、四个方向上分别竖直设置于主承力结构框架外部的侧板、相对设置于主承力结构框架外部的底板和顶板、设置于底板下方的转接支架,其中:两个主承力结构框架通过与顶板和底板连接配合而相向布置,形成了箱板式探月微纳卫星的主体承力结构,转接支架的上表面通过分离释放机构与卫星连接,下表面与运载绝缘隔热安装,主体承力结构内壁竖直水平方向设有多根加强肋用于固定星内综合电子堆栈模块和/或加固整体结构。本发明采用贯穿式设计,在保证整星结构稳定与外部包络的精度前提下,提供了充分的内部空间,不仅加工装配简单,结构可靠,而且内部空间连贯,便于满足卫星的多样化布局和功能组件的广泛选择。


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    Titel :

    Box plate type lunar exploration micro-nano satellite supporting structure


    Weitere Titelangaben:

    箱板式探月微纳卫星支撑结构


    Beteiligte:
    WANG WEI (Autor:in) / MU ZHONGCHENG (Autor:in) / YI JIYUAN (Autor:in) / WU SHUFAN (Autor:in) / HUANG YIXIN (Autor:in) / MO QIANKUN (Autor:in) / WANG XIAOLIANG (Autor:in) / ZHOU HANG (Autor:in) / WU HANG (Autor:in) / CAO XIN (Autor:in)

    Erscheinungsdatum :

    25.10.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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