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.
Nonmetallic-material configuration control in the Apollo spacecraft
1971-01-01
Conference paper
No indication
English
Apollo spacecraft nonmetallic materials applications
NTRS | 1971
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