This is a closed form solution for the longitudinal oscillation of the Solar Array Flight Experiment (SAFE) blanket for all phases of deployment. The frequency response shows that the blanket frequency increases shortly before full deployment. That fact causes a coupling between the mast and the blanket frequency but, because of the relatively high speed of deployment, a buildup of resonance is unlikely.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Solar Array Flight Experiment


    Beteiligte:
    J. Slaby (Autor:in)

    Erscheinungsdatum :

    1985


    Format / Umfang :

    17 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    NASA solar array flight experiment

    Turner, G. / Hill, H. | NTRS | 1982


    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, R. W. | NTRS | 1986


    Solar array flight dynamic experiment

    Schock, Richard W. | NTRS | 1987