The invention relates to a parallel-arranged storage tank satellite transverse centroid adjusting method. The method is characterized in that the filling weights of propellants in different storage tanks of the parallel storage tank satellite are designed, so that the adjustment of the transverse centroid of the whole satellite in the launching state of a spacecraft is realized without additionally adding a balancing weight while the propellant filling of the spacecraft is finished. A whole-satellite zero-counterweight transverse centroid adjustment strategy is realized, the load bearing capacity of the spacecraft can be effectively improved, and the method has relatively high engineering application value and prospect.

    一种并联布置贮箱卫星横向质心调整方法,通过设计并联贮箱卫星不同贮箱内推进剂的加注重量,在完成航天器推进剂加注的同时,无需额外增加配重块,实现航天器发射状态整星横向质心的调整,利用同种推进剂贮箱加注重量差,实现整星零配重横向质心调整策略,能够有效提高航天器的载荷承载能力,具有较强的工程应用价值和前景。


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    Titel :

    Parallel-arranged storage tank satellite transverse centroid adjusting method


    Weitere Titelangaben:

    一种并联布置贮箱卫星横向质心调整方法


    Beteiligte:
    LIU MIN (Autor:in) / PEI SHENGWEI (Autor:in) / LYU HONGJIAN (Autor:in) / SUN HENGCHAO (Autor:in) / HOU FENGLONG (Autor:in)

    Erscheinungsdatum :

    2020-12-25


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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