Vibroacoustic and thermal environment data gathered from the first three flights of the space shuttle are presented. The characterization of the particulate, gaseous, and electromagnetic emissions associated with the shuttle flight is emphasized. Measurements of vehicle glow light emissions and material effects (mass loss) due to the low Earth environment interactions with the shuttle vehicle are presented.


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    Title :

    Introductory comments


    Contributors:


    Publication date :

    1983-02-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




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