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NASA-LLIS-1330

Lessons Learned – Space Charging of Composite Structures

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T18:18:11Z
date available2017-09-04T18:18:11Z
date copyright03/05/2003
date issued2003
identifier otherHQVEQCAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;jsery=autho162s7D8308/handle/yse/200901
description abstractAbstract:
Although graphite/polymer composites were thought to be immune to space plasma charging because the material is electrically conductive, it may actually retain a significant charge in places where the non-conductive resin pools.
Use a non-contact charge measuring device when testing the material's electrical resistance, and consider spacecraft designs that can accept worst-case electrical discharges.
languageEnglish
titleNASA-LLIS-1330num
titleLessons Learned – Space Charging of Composite Structuresen
typestandard
page3
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;2003
contenttypefulltext
subject keywordsbulk dielectric charging
subject keywordsconducted electromagnetic interference
subject keywordsconductive surfaces
subject keywordsdielectric materials
subject keywordsEnergy
subject keywordsEnvironment
subject keywordsFlight Equipment
subject keywordsFlight Operations
subject keywordsHardware
subject keywordsIESD
subject keywordsIndustrial Operations
subject keywordsinternal electrostatic discharge
subject keywordsParts Materials & Processes
subject keywordsPayloads
subject keywordsradiated electromagnetic interference
subject keywordsSafety & Mission Assurance
subject keywordsSpacecraft
subject keywordsspacecraft materials
subject keywordsTest & Verification


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