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Lessons Learned – Design Practice to Control Interference from Electrostatic Discharge (ESD)

contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T16:54:17Z
date available2017-09-04T16:54:17Z
date copyright04/11/2000
date issued2000
identifier otherWYCEQCAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/117749
description abstractPractice:
Minimize the adverse effects of electrostatic discharge (ESD) on spacecraft by implementing the following three design practices:
1. Make all external surfaces of the spacecraft electrically conductive and grounded to the main structure.
2. Provide all internal metallic elements and other conductive elements with an "ESD conductive" path to the main structure.
3. Enclose all sensitive circuitry in an electrically conductive enclosure-- a "Faraday cage".
languageEnglish
titleNASA-LLIS-0773num
titleLessons Learned – Design Practice to Control Interference from Electrostatic Discharge (ESD)en
typestandard
page4
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;2000
contenttypefulltext


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