The invention provides a satellite structure for parallel launching of double satellites and a satellite carrier rocket. The satellite structure comprises a fairing and satellites, the satellites are arranged in the fairing, the number of the satellites is two, the satellites are arranged side by side, and the two satellites are symmetrically arranged relative to the center of the fairing; the side, close to the fairing, of the satellite is arranged to be an inclined face, and the position, where the satellite is installed, of the fairing is arranged to be conical and matched with the inclined face of the satellite. The planar antenna and the solar cell array provided by the invention do not need to design an expandable mechanism, so that the system complexity of the planar antenna and the solar cell array is reduced, and the reliability of a satellite is improved.

    本发明提供了一种用于双星并联发射的卫星结构及卫星运载火箭,包括:整流罩和卫星;所述卫星安置在所述整流罩内,所述卫星设置有两个并且并排放置,两个所述卫星关于所述整流罩中心对称放置;所述卫星靠近所述整流罩一侧设置为斜面,所述整流罩安装所述卫星处设置为锥形并与所述卫星斜面相适配。本发明提供的平板天线和太阳电池阵均无需设计可展开机构,降低了平板天线和太阳电池阵的系统复杂度,提升了卫星的可靠性。


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    Titel :

    Satellite structure for parallel launching of double satellites and satellite carrier rocket


    Weitere Titelangaben:

    用于双星并联发射的卫星结构及卫星运载火箭


    Beteiligte:
    CHEN TING (Autor:in) / CHEN GUOZHONG (Autor:in)

    Erscheinungsdatum :

    2022-10-11


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS / F42B EXPLOSIVE CHARGES, e.g. FOR BLASTING , Explosive Ladungen, z.B. für Sprengungen



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