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NASA-LLIS-0708

Lessons Learned – Plasma Noise in EMI Design

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 2000

Abstract: Practice:
Missions with payloads that can interact strongly with the ambient plasma, such as a high power electron beam, a high power RF source, or an ion engine, may require a structural current test for conducted susceptibility and higher radiated susceptibility test levels. The practice is to perform an analysis early in such a program to estimate the amplitude of plasma noise induced electromagnetic interference (EMI). This may identify potential adverse effects on operational reliability.
URI: https://yse.yabesh.ir/std/handle/yse/22158
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    NASA-LLIS-0708

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:22:08Z
date available2017-09-04T15:22:08Z
date copyright03/16/2000
date issued2000
identifier otherNBDEQCAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/22158
description abstractPractice:
Missions with payloads that can interact strongly with the ambient plasma, such as a high power electron beam, a high power RF source, or an ion engine, may require a structural current test for conducted susceptibility and higher radiated susceptibility test levels. The practice is to perform an analysis early in such a program to estimate the amplitude of plasma noise induced electromagnetic interference (EMI). This may identify potential adverse effects on operational reliability.
languageEnglish
titleNASA-LLIS-0708num
titleLessons Learned – Plasma Noise in EMI Designen
typestandard
page4
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;2000
contenttypefulltext
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