An electrical power system may comprise a first energy source management converter (ESMC) configured to be connected in electronic communication with a first power source, a second ESMC configured to be connected in electronic communication with a second power source, and a multi-channel DC bus, wherein the first ESMC is configured to supply electric power to a first channel of the multi-channel DC bus, the second ESMC is configured to supply electric power to a second channel of the multi-channel DC bus, and the multi-channel DC bus is configured to supply electric power to a load.


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    Title :

    SOLAR POWERED SPACECRAFT POWER SYSTEM


    Contributors:

    Publication date :

    2018-05-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    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 / H02M APPARATUS FOR CONVERSION BETWEEN AC AND AC, BETWEEN AC AND DC, OR BETWEEN DC AND DC, AND FOR USE WITH MAINS OR SIMILAR POWER SUPPLY SYSTEMS , Anlagen zur Umformung von Wechselstrom in Wechselstrom, von Wechselstrom in Gleichstrom oder umgekehrt, oder von Gleichstrom in Gleichstrom und zur Verwendung in Netzen oder ähnlichen Stromversorgungssystemen



    Solar powered spacecraft power system

    ROZMAN GREGORY I / FUTRELL MICHAEL ANTHONY | European Patent Office | 2019

    Free access

    SOLAR POWERED SPACECRAFT POWER SYSTEM

    ROZMAN GREGORY I / MICHAEL ANTHONY FUTRELL | European Patent Office | 2018

    Free access