Information from current and projected man bearing vehicles is used to estimate parameters such as size of cabin, number of crew, duration of flight, and possible heat loads for all stages of such journey; environmental requirements; main part of paper describes environmental engineering systems for small Earth-to-orbit vehicle, large space station, and lunar suit; possible emergencies and their countermeasures.


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    Title :

    High altitude chambers and pressure suits and their part in manned flight to moon


    Additional title:

    Brit Interplanetary Soc -- J


    Contributors:
    Still, E.W. (author)


    Publication date :

    1960


    Size :

    38 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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