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Lessons Learned - Solid Rocket Motor (SRM) O-ring Processing

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:44:32Z
date available2017-09-04T18:44:32Z
date copyright33900
date issued1992
identifier otherKEZCQCAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;jsessionid=3826AF679D40527318548F1EFDEC014A/handle/yse/225997
description abstractDescription of Driving Event:
During processing, employees failed to perform checks of the mandatory inspection points of the orings as specified in the acceptance criteria. However, a review of inspection records for the 51-L orings indicates there is a high probability that the 51-L o-rings were acceptable for launch
languageEnglish
titleNASA-LLIS-0178num
titleLessons Learned - Solid Rocket Motor (SRM) O-ring Processingen
typestandard
page2
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1992
contenttypefulltext
subject keywordsRisk Management/Assessment
subject keywordsTest & Verification


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