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Lessons Learned - Solid Rocket Motor (SRM) Processing and Inspection

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:42:39Z
date available2017-09-04T15:42:39Z
date copyright33926
date issued1992
identifier otherPJZCQCAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/44904
description abstractDescription of Driving Event:
All inventory SRM case o-rings were reinspected during the STS 51-L investigation. When reinspected using original inspection equipment (mechanical micrometer), very few out-of-tolerance conditions were identified. However, when reinspected with a laser micrometer with a 0.007-inch measuring beam, numerous small localized out-of-tolerance conditions were detected. All inventory o-rings were also x-rayed, indicating numerous o-ring inclusions. Although tests proved that these conditions did not affect the sealing capability, this does indicate a potential problem and a need for processing and inspection improvements. It was also learned during this investigation that the o-ring material manufacturer had changed material formulations and processing numerous times since starting to produce srm o-ring material. While all these formulations resulted in o-ring material that was in compliance with MIL-R-83248, this lack of standardization could possibly result in application problems and is unacceptable for such a critical item
languageEnglish
titleNASA-LLIS-0215num
titleLessons Learned - Solid Rocket Motor (SRM) Processing and Inspectionen
typestandard
page2
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1992
contenttypefulltext
subject keywordsLaunch Vehicle
subject keywordsParts Materials & Processes


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