According to the one-rocket seventeen-star satellite layout configuration, a main load-bearing structure adopts a structural form of a supporting cabin and a cylinder section, the main load-bearing structure comprises an upper cylinder section, a lower cylinder section and a supporting cabin which are connected in sequence, and a supporting beam is installed on the upper end face of the upper cylinder section; the seventeen satellites comprise six microsatellites and eleven microsatellites; the six microsatellites are arranged on the outer side wall of the supporting cabin; among the eleven small satellites, five small satellites are arranged on the outer side wall of the lower cylinder section, five small satellites are arranged on the outer side wall of the upper cylinder section, and one small satellite is installed on the upper end face of the upper cylinder section through a supporting beam. The side wall space of the supporting cabin and the main load-bearing structure are fully utilized for satellite layout, and the structural weight is reduced; the satellites are circumferentially and uniformly distributed on the side wall, the satellite separation scheme is simple, and the safety is high; and by adopting the upper and lower cylinder section structure, the convenience of satellite-rocket combined operation is greatly improved, and the problems of heavy weight, complex separation scheme, poor satellite-rocket combined operability and the like of the existing multi-satellite layout structure are solved.

    本发明的一箭十七星卫星布局构型,主承力结构采用支承舱+筒段的结构形式,主承力结构包括依次连接的上筒段、下筒段和支承舱,在上筒段的上端面上安装有支承梁;十七星包括六颗微型卫星和十一颗小型卫星;六颗微型卫星布置在支承舱外侧壁上;十一颗小型卫星中,五颗小型卫星布置在下筒段外侧壁上,五颗小型卫星布置在上筒段外侧壁上,一颗小型卫星通过支承梁安装在上筒段的上端面上。本发明充分利用支承舱侧壁空间和主承力结构进行卫星布局,减少了结构重量;卫星采用侧壁周向均布,卫星分离方案简单、安全性高;采用上下筒段结构,大大提升了星箭联合操作的便利性,解决了现有多星布局结构重量重,分离方案复杂、星箭联合操作性差等问题。


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    Title :

    Satellite layout configuration with one arrow and seventeen satellites


    Additional title:

    一箭十七星卫星布局构型


    Contributors:
    ZHAO ZHIJIE (author) / ZENG YUQIN (author) / XIANG CHANGZHENG (author) / HU ZEZHONG (author) / LIU ZHENDONG (author) / DONG WENFENG (author) / WEI XIYANG (author) / YUAN XIURAO (author)

    Publication date :

    2023-03-21


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64G Raumfahrt , COSMONAUTICS