The methods employed by NASA to establish configuration control of nonmetallic materials on Apollo spacecraft are described. A five step procedure for examining contractor materials for suitability and compatibility is presented. The compatibility of the materials with the oxygen enriched environment of the spacecraft enclosures is emphasized.


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    Title :

    Nonmetallic-material configuration control in the Apollo spacecraft


    Contributors:


    Publication date :

    1971-01-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English





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