Heat balance was established between metabolic heat generated by suited subject and heat transferred to his environment in space chamber at Republic Aviation Corp; mass flow rates of constituents of ventilation stream into and out of suit were calculated from partial pressure data monitored by mass spectrometer; suited subjects, biomedically instrumented, performed work on bicycle ergometer at simulated altitude of 35,000 ft; results obtained are summarized.


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    Title :

    Manned chamber testing of Apollo prototype space suit


    Additional title:

    AIAA -- Tech Papers


    Contributors:
    Frankel, G. (author) / Albright, G. (author) / Axelrod, I. (author)

    Conference:

    AIAA -- Space Simulation Testing Conference ; 1964 Life support systems



    Publication date :

    1964


    Size :

    7 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :


    MANNED CHAMBER TESTING OF THE APOLLO PROTOTYPE SPACE SUIT

    ALBRIGHT, M. / AXELROD, I. / FRANKEL, G. | AIAA | 1964


    Manned chamber testing of the apollo prototype space suit

    ALBRIGHT, G. / AXELROD, I. / FRANKEL, G. | AIAA | 1965


    Manned Space Flight Network Testing for Apollo

    Carl O Roberts, Jr. | NTRS | 1966


    Apollo Space-Suit Materials

    Frederic S. Dawn / Ralph L. Jarboe | NTRS | 1971


    Manned space flight -- Beyond Apollo

    Engineering Index Backfile | 1965