In prior studies of the current Shuttle Spacesuit (SSA), where basic fabric lay-ups were tested for shielding capabilities, it was found that the fabric portions of the suit give far less protection than previously estimated due to porosity and non-uniformity of fabric and LCVG components. In addition, overall material transmission properties were less than optimum. A number of alternate approaches are being tested to provide more uniform coverage and to use more efficient materials. We will discuss in this paper, recent testing of new material lay-ups/configurations for possible use in future spacesuit designs.


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    Title :

    Design and Testing of Improved Spacesuit Shielding Components


    Additional title:

    Sae Technical Papers


    Contributors:
    Zeitlin, C. J. (author) / de Angelis, G. (author) / Ferl, J. (author) / Tweed, J. (author) / Ware, J. (author) / Wilson, J. W. (author) / Clowdsley, M. S. (author)

    Conference:

    International Conference On Environmental Systems ; 2002



    Publication date :

    2002-07-15




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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