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Lessons Learned – Space Shuttle Program/Super Light Weight External Tank/Materials & Test and Verification Changes

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:10:11Z
date available2017-09-04T16:10:11Z
date copyright02/01/1997
date issued1997
identifier otherSIUEQCAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/73453
description abstractDescription of Driving Event:
Lower than Anticipated Fracture Toughness of the 2195 Aluminum-Lithium Alloy Used in the SLWT at Cryogenic Temperatures Causing Changes to Test & Verification Procedures.
languageEnglish
titleNASA-LLIS-1010num
titleLessons Learned – Space Shuttle Program/Super Light Weight External Tank/Materials & Test and Verification Changesen
typestandard
page3
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1997
contenttypefulltext
subject keywordsAerospace Safety Advisory Panel
subject keywordsCryogenic Systems
subject keywordsEnergetic Materials - Explosive/Propellant/Pyrotechnic
subject keywordsHardware
subject keywordsParts Materials & Processes
subject keywordsPolicy & Planning
subject keywordsRisk Management/Assessment
subject keywordsSpacecraft
subject keywordsStandard
subject keywordsTest & Verification


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