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Lessons Learned - Thermal-Vacuum Versus Thermal-Atmospheric Tests of Electronic Assemblies

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:20:43Z
date available2017-09-04T15:20:43Z
date copyright04/14/2000
date issued2000
identifier otherMXCEQCAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/20641
description abstractPractice:
Perform all thermal environmental tests on electronic spaceflight hardware in a flight-like thermal vacuum environment (i.e., do not substitute an atmospheric pressure thermal test for the thermal/ vacuum test). Moreover, if a compromise is thought to be necessary for nontechnical reasons, then an analysis is required to quantify the reduction in test demonstrated reliability.
languageEnglish
titleNASA-LLIS-0781num
titleLessons Learned - Thermal-Vacuum Versus Thermal-Atmospheric Tests of Electronic Assembliesen
typestandard
page7
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;2000
contenttypefulltext


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