The invention provides a power supply and distribution system of a multi-stage carrier rocket. Two ends of the multi-stage carrier rocket are respectively powered by independent batteries. The systemis advantaged in that characteristics of multiple stages and long length of the multi-stage carrier rocket are combined, a two-end power supply mode is adopted, the weight of a power supply and distribution system is reduced, and the weight reduction amplitude is not smaller than 30%.

    本申请提供了一种多级运载火箭的供配电系统,多级运载火箭的两端分别采用独立的电池供电。本申请结合多级运载火箭级数多、长度长的特点,采用两端供电的方式,减轻供配电系统的重量,减重幅度不少于30%。


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    Titel :

    Power supply and distribution system of multistage carrier rocket


    Weitere Titelangaben:

    一种多级运载火箭的供配电系统


    Beteiligte:
    YU JICHAO (Autor:in) / ZHU YONGQUAN (Autor:in) / YANG YIQIANG (Autor:in) / XIN ZHEKUI (Autor:in) / WANG ZHI (Autor:in)

    Erscheinungsdatum :

    19.06.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS / H02J CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER , Schaltungsanordnungen oder Systeme für die Abgabe oder Verteilung elektrischer Leistung



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