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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    Title :

    Power supply and distribution system of multistage carrier rocket


    Additional title:

    一种多级运载火箭的供配电系统


    Contributors:
    YU JICHAO (author) / ZHU YONGQUAN (author) / YANG YIQIANG (author) / XIN ZHEKUI (author) / WANG ZHI (author)

    Publication date :

    2020-06-19


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    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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