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Lessons Learned – Cracks in the Body of Dual Inline Package (DIP) Components in the ASTROS Star Tracker Electronic Assembly

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T17:48:24Z
date available2017-09-04T17:48:24Z
date copyright07/07/1993
date issued1993
identifier otherEQZCQCAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std/handle/yse/171579
description abstractAbstract:
Functional testing of the ASTROS Star Tracker Electronic Assembly revealed a hairline crack that appeared to have been caused by lead bending tools used to form the part leads for installation. The tooling had been previously used successfully on this part type but a different lot number. Part types requiring mechanical lead forming should have approved procedures and qualified processes with adequate sample testing prior to forming component leads for installation into flight hardware.
languageEnglish
titleNASA-LLIS-0268num
titleLessons Learned – Cracks in the Body of Dual Inline Package (DIP) Components in the ASTROS Star Tracker Electronic Assemblyen
typestandard
page2
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1993
contenttypefulltext
subject keywordsCracked Components
subject keywordsParts Materials & Processes


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