The NASA large flexible solar array space shuttle flight experiment is described. The 32 x 4 m wing is deployed from the shuttle bay, and experiments in electrical output, multiple deployment, and structural dynamics are planned. Both 2 x 4 cm and 5.9 x 5.9 cm cell assemblies on the array blanket are evaluated. Safety/hazards provisions are described, including emergency jettison provisions. Ground testing and hardware fabrication are summarized.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    NASA solar array flight experiment


    Beteiligte:
    Turner, G. (Autor:in) / Hill, H. (Autor:in)


    Erscheinungsdatum :

    01.06.1982


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Solar Array Flight Experiment

    J. Slaby | NTIS | 1985


    Solar array flight dynamic experiment

    Schock, R. W. | NTRS | 1986


    Solar Array Flight Experiment (SAFE)

    Schock, R. W. | NTRS | 1982


    Solar Array Flight Dynamic Experiment

    R. W. Schock | NTIS | 1986


    Solar array flight dynamic experiment

    Schock, Richard W. | NTRS | 1987