An example of an apparatus includes a spacecraft body and a solar array that is attached to the spacecraft body. In addition, a solar array spring element is configured to provide a force between the solar array and one or more components of a neighboring spacecraft in a stack of spacecraft.


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    Titel :

    SOLAR ARRAY SPRING ELEMENTS FOR STACKING SPACECRAFT


    Beteiligte:
    YATES HARRY A (Autor:in) / BIENIEK RYAN (Autor:in) / SZETO ALAN J (Autor:in) / PSYK KATE (Autor:in) / BRIEND JONATHAN (Autor:in)

    Erscheinungsdatum :

    24.10.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



    SOLAR ARRAY SPRING ELEMENTS FOR STACKING SPACECRAFT

    YATES HARRY A / BIENIEK RYAN / SZETO ALAN J et al. | Europäisches Patentamt | 2024

    Freier Zugriff

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