Vibration generation and propagation in orbital platforms, including Spacelab and EURECA, were analyzed. Attitude and orbit control subsystem vibration generators; vibrations induced by thermal control subsystems; measurement techniques and experimental aspects for a microgravity environment; vibration induced by microgravity-oriented payloads; and vibration reduction techniques were studied. Dynamic synthesis of a microgravity platform is discussed.


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    Titel :

    Key Design Parameters for a Very Low Gravity in-Orbit Facility


    Beteiligte:
    J. C. Amieux (Autor:in) / C. Fournier (Autor:in) / R. Strittmatter (Autor:in) / M. Baier (Autor:in) / D. Schmitt (Autor:in)

    Erscheinungsdatum :

    1985


    Format / Umfang :

    372 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch