A mechanism called a deployment/retraction assembly (DRA) which provides not only a stable, but a deployable platform for the high gain antenna system (HGAS) aboard the Solar Maximum Mission (SMM) spacecraft is described. The DRA also has the capability to retract the system upon command.


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    Titel :

    Deployment/retraction mechanism for solar maximum mission high gain antenna system


    Beteiligte:
    Bennett, N. (Autor:in) / Preiswerk, P. (Autor:in)


    Erscheinungsdatum :

    01.04.1979


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :




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