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Lessons Learned - Solid Rocket Motor (SRM) Sealing Surfaces

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:49:45Z
date available2017-09-04T15:49:45Z
date copyright33900
date issued1992
identifier otherQEZCQCAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/52782
description abstractDescription of Driving Event:
A case dimensional change study performed as part of the 51-L failure analysis effort produced the diameter change results. The potential cause for this phenomenon is believed to be material related in three areas and their direct effect on the hydrostatic proof test pressure level chosen for acceptance testing prior to reuse.
languageEnglish
titleNASA-LLIS-0180num
titleLessons Learned - Solid Rocket Motor (SRM) Sealing Surfacesen
typestandard
page2
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1992
contenttypefulltext
subject keywordsHardware
subject keywordsParts Materials & Processes


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