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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    Title :

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


    Contributors:
    J. C. Amieux (author) / C. Fournier (author) / R. Strittmatter (author) / M. Baier (author) / D. Schmitt (author)

    Publication date :

    1985


    Size :

    372 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English