Environmental acceptance testing was used extensively to screen selected spacecraft hardware for workmanship defects and manufacturing flaws. The minimum acceptance levels and durations and methods for their establishment are described. Component selection and test monitoring, as well as test implementation requirements, are included. Apollo spacecraft environmental acceptance test results are summarized, and recommendations for future programs are presented.


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    Title :

    Apollo experience report environmental acceptance testing


    Contributors:

    Publication date :

    1976-06-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English