A solar panel assembly for a spacecraft includes a bracket and first and second booms each having a first end secured to the bracket and a second end extending away from the bracket. Each boom is formed from a plurality of tubes that telescope between a stowed condition nested within one another and a deployed condition aligned end-to-end with one another. A solar panel is secured to the first and second booms for receiving solar energy and converting the solar energy to electrical power. The solar panel has a stowed condition collapsed between the first and second booms and a deployed condition extending in a plane between the first and second booms.


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    Titel :

    DEPLOYABLE SOLAR PANEL ARRAY FOR SPACECRAFT


    Weitere Titelangaben:

    ENTFALTBARE SOLARPANEELANORDNUNG FÜR RAUMFAHRZEUG
    RÉSEAU DE PANNEAUX SOLAIRES DÉPLOYABLES POUR ENGIN SPATIAL


    Beteiligte:

    Erscheinungsdatum :

    18.10.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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