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NASA-HDBK-4006

LOW EARTH ORBIT SPACECRAFT CHARGING DESIGN HANDBOOK - Revalidation Date: 06-06-2013

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 2013

Abstract: The information in this handbook presents an overview of the current understanding of the various plasma interactions that can result when a high-voltage system is operated in the Earth's ionosphere, references common design practices that have exacerbated plasma interactions in the past, and recommends standard practices to eliminate or mitigate such reactions.
Purpose
The purpose of this handbook is to provide design guidance referenced in NASA-STD-4005, Low Earth Orbit Spacecraft Charging Design Standard, for high-voltage space power systems (>55 volts) that operate in the plasma environment associated with LEO (altitude from 200 and 1000 km and latitude between -50 and +50 degrees). Such power systems, particularly solar arrays, are the proximate cause of spacecraft charging in LEO, and these systems can interact with this environment in a number of ways that are potentially destructive to themselves as well as to the platform or vehicle that has deployed them.
Applicability
This handbook is applicable to high-voltage space power systems that operate in the plasma environment associated with LEO (see NASA-STD-4005).
This handbook may be referenced in contract, program, and other Agency documents for guidance.
URI: https://yse.yabesh.ir/std/handle/yse/18816
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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:19:04Z
date available2017-09-04T15:19:04Z
date copyright06/03/2007 (R 2013)
date issued2013
identifier otherMSFKCCAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/18816
description abstractThe information in this handbook presents an overview of the current understanding of the various plasma interactions that can result when a high-voltage system is operated in the Earth's ionosphere, references common design practices that have exacerbated plasma interactions in the past, and recommends standard practices to eliminate or mitigate such reactions.
Purpose
The purpose of this handbook is to provide design guidance referenced in NASA-STD-4005, Low Earth Orbit Spacecraft Charging Design Standard, for high-voltage space power systems (>55 volts) that operate in the plasma environment associated with LEO (altitude from 200 and 1000 km and latitude between -50 and +50 degrees). Such power systems, particularly solar arrays, are the proximate cause of spacecraft charging in LEO, and these systems can interact with this environment in a number of ways that are potentially destructive to themselves as well as to the platform or vehicle that has deployed them.
Applicability
This handbook is applicable to high-voltage space power systems that operate in the plasma environment associated with LEO (see NASA-STD-4005).
This handbook may be referenced in contract, program, and other Agency documents for guidance.
languageEnglish
titleNASA-HDBK-4006num
titleLOW EARTH ORBIT SPACECRAFT CHARGING DESIGN HANDBOOK - Revalidation Date: 06-06-2013en
typestandard
page63
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;2013
contenttypefulltext
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DSpace software copyright © 2017-2020  DuraSpace
نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
yabeshDSpacePersian