A heatpipe experiment for a long duration exposure facility is described. The design and configuration of the power system of the spacecraft is reported with emphasis placed on its solar array panels, 12-ampere hour 18-cell nickel battery, and its electronic controller.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    The LDEF heat pipe experiment power systems


    Contributors:


    Publication date :

    1980-04-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English