Phenomena, design concepts, and design problems related to emergency repressurization systems for 2 large-space simulation chambers designed to test Apollo vehicle and to train astronauts; repressurization systems protect astronauts from effects of sudden loss of space suit pressure and of breathing oxygen while chambers are under high vacuum; engineering problems encountered involving thermodynamics, transient heat transfer, high velocity gas flow, and acoustics; analyses and calculations indicate that present system design eliminated problems.


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    Title :

    Emergency repressurization of large space simulation chambers


    Additional title:

    SAE -- Paper


    Contributors:
    Kuo, C.S. (author) / Heisler, S.I. (author) / Nayak, P.N. (author)

    Conference:

    SAE Meeting ; 1964 Simulators



    Publication date :

    1964


    Size :

    8 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :