Considerable progress has been made in understanding the basic transmission properties of the spacesuit fabric as it is now used in the space program. Some improved details for the physical model for the cooling tube are still required. It is desirable to also study the electron transmission properties to insure that a consistent picture of the spacesuit fabric is obtained. The basic fabric model as outlined is being integrated into a spacesuit model for estimates of astronaut exposures during future missions.


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    Title :

    Shuttle Spacesuit: Fabric/LCVG Model Validation


    Contributors:
    J. W. Wilson (author) / J. Tweed (author) / C. Zeitlin (author) / M. H. Y. Kim (author) / B. M. Anderson (author)

    Publication date :

    2004


    Size :

    10 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Shuttle Spacesuit: Fabric/LCVG Model Validation

    Wilson, J. W. / Tweed, J. / Zeitflin, C. et al. | NTRS | 2001


    Shuttle Spacesuit: Fabric/LCVG Model Validation

    Persans, A.E. / Anderson, B. M. / Zeitlin, C. et al. | SAE Technical Papers | 2001


    Shuttle Spacesuit: Fabric/LCVG Model Validation

    Wilson, J. W. / Tweed, J. / Zeitlin, C. et al. | NTRS | 2001


    Shuttle Spacesuit: Fabric/LCVG Model Validation

    Wilson, J. W. / Tweed, J. / Zeitlin, C. et al. | British Library Conference Proceedings | 2001


    Shuttle Spacesuit (Radiation) Model Development

    Persans, A. E. / Anderson, Brooke M. / Cucinotta, F. A. et al. | SAE Technical Papers | 2001