The invention discloses a 100V S4R circuit for a spacecraft, which belongs to the technical field of satellite power supply equipment, and is characterized by comprising a shunt tube, a protection tube, a charging tube, a BEA for controlling the working state of the charging tube, and an MEA for controlling the working state of the shunt tube, wherein the positive electrode of the solar cell array is connected with the positive electrode of the 100V bus through the first diode in sequence; the anode of the solar cell array is grounded through the shunt tube and the protection tube in sequence and is connected with the cathode of the solar cell array; the anode of the solar cell array is connected with the anode of the storage battery pack through a third diode and a charging switch in sequence; the protection tube is connected with a first driving circuit; the second driving circuit is connected with the shunt tube, the charging tube, the BEA and the MEA. According to the 100V main bus, the reliability requirement of a high-power satellite on the 100V main bus can be met, and a high-reliability and high-power 100V main bus is provided for a high-power satellite power supply system.

    本发明公开了一种航天器用100V电压的S4R电路,属于卫星供电设备技术领域,其特征在于,包括分流管、保护管、充电管、控制充电管工作状态的BEA,控制分流管工作状态的MEA;其中:太阳电池阵的正极依次通过第一二极管与100V母线正连接;太阳电池阵的正极依次通过分流管、保护管接地与太阳电池阵的负极连接;太阳电池阵的正极依次通过第三二极管、充电开关与蓄电池组的正极连接;所述保护管连接有第一驱动电路;第二驱动电路分别与分流管、充电管、BEA和MEA连接。本发明能够满足大功率卫星对100V主母线的可靠性需求,为大功率卫星电源系统提供一条高可靠、大功率的100V主母线。


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    Title :

    100V S4R circuit for spacecraft


    Additional title:

    一种航天器用100V电压的S4R电路


    Contributors:
    YANG ZHE (author) / BAI HAO (author) / HUANG XIAO (author) / CHEN XINGNA (author) / WANG YAOQING (author)

    Publication date :

    2023-10-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    H02J CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER , Schaltungsanordnungen oder Systeme für die Abgabe oder Verteilung elektrischer Leistung / B64G Raumfahrt , COSMONAUTICS / H02S GENERATION OF ELECTRIC POWER BY CONVERSION OF INFRA-RED RADIATION, VISIBLE LIGHT OR ULTRAVIOLET LIGHT, E.G. USING PHOTOVOLTAIC [PV] MODULES , Erzeugung elektrischer Energie durch Umwandlung von Infrarot-Strahlung, sichtbarem Licht oder ultraviolettem Licht, z.B. unter Verwendung von Photovoltaik [PV]-Modulen



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