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Lessons Learned - SEASAT Failure

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:28:35Z
date available2017-09-04T18:28:35Z
date copyright01/24/1995
date issued1995
identifier otherIRAEQCAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;jsery=autho146/handle/yse/210713
description abstractAbstract:
The SEASAT Spacecraft failed in orbit due to arcing between adjacent slip ring brush assemblies. It was discovered that the Agena bus had been substantially modified, but were treated as a heritage design not requiring requalification. Plans should be made early in the project to fully evaluate the heritage of previously used equipment. When conducting a FMECA on electrical components, electrical short failure modes should be considered.
languageEnglish
titleNASA-LLIS-0371num
titleLessons Learned - SEASAT Failureen
typestandard
page3
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1995
contenttypefulltext
subject keywordsHardware
subject keywordsInherited Equipment
subject keywordsSlip Rings


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