An orbital satellite has a bus formed of a bus module and a payload module. Both the bus module and the payload modules may include a pair of panels integrally formed at an angle of for example 90° with respect to each other. Components and electronics supporting the satellite systems may be mounted on the panels of the bus and payload modules. Heat generated by the components and electronics are conducted between panels of the bus module and/or payload module. Sufficient heat transfer between panels occurs as a result of their being integrally formed with each other.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    THERMALLY EFFICIENT BUS HOUSING


    Beteiligte:
    GEORGIS DAVID (Autor:in) / OEY FREDERICK (Autor:in) / HELMER ROBERT (Autor:in)

    Erscheinungsdatum :

    2024-03-07


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



    A THERMALLY CONTROLLED HOUSING ASSEMBLY FOR ELECTRICAL CELLS

    CHOPARD FABRICE / FLORENTZ BERTRAND | Europäisches Patentamt | 2023

    Freier Zugriff

    THERMALLY EFFICIENT ROUTE SELECTION

    PERUMALLA SARASWATHI / RAKSHIT SARBAJIT / CHETTUPALLI SWETHA et al. | Europäisches Patentamt | 2022

    Freier Zugriff


    HyTEC Hybrid Thermally Efficient Core

    Anthony Nerone / James Kenyon / Ashlie Flegel et al. | NTRS