Function of environmental control system for initial lunar Apollo mission is to maintain temperature of Command Module at between 70 and 80 F with maximum of 90 F during re-entry, and humidity between 40 and 70%; atmosphere is 100% oxygen at 5 psia; block II life-support system differs from previous systems, such as those used in Gemini and Mercury, in several ways, which are pointed out; oxygen supply, cooling system and water supply are also described. (Technology Week including)


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    Titel :

    Apollo lunar flight package readied


    Weitere Titelangaben:

    Missiles Rockets


    Beteiligte:
    David, H.M. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1966


    Format / Umfang :

    3 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :