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AIAA S-133-5

Space Plug-and-Play Architecture Standard 28V Power Service

Organization:
AIAA - American Institute of Aeronautics and Astronautics
Year: 2013

Abstract: This standard is applicable to systems operating under the Space Plug-and-Play Architecture.
The SPA 28V Power Service Standard establishes specifications regarding the quality of the power service such as voltage ripple, transients, and interruptions.
The scope of this document is limited to the interface between a SPA-equipped spacecraft and SPAcompliant device. This interface is implemented at a physical SPA endpoint connector, specified in AIAA S-133-4-2013 SPA Physical Interface Standard, which contains details of the connector type, pin assignments, and wiring harnesses. Details of the design of a specific spacecraft electrical power subsystem, including power sources such as solar arrays and power storage devices such as batteries, are not relevant to the SPA power interface described in this document.
URI: http://yse.yabesh.ir/std;jsery=autho4703177D081D20686159DD6EFDEC9FCD/handle/yse/22714
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    AIAA S-133-5

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contributor authorAIAA - American Institute of Aeronautics and Astronautics
date accessioned2017-09-04T15:22:33Z
date available2017-09-04T15:22:33Z
date copyright2013.01.01
date issued2013
identifier otherNCREGFAAAAAAAAAA.pdf
identifier urihttp://yse.yabesh.ir/std;jsery=autho4703177D081D20686159DD6EFDEC9FCD/handle/yse/22714
description abstractThis standard is applicable to systems operating under the Space Plug-and-Play Architecture.
The SPA 28V Power Service Standard establishes specifications regarding the quality of the power service such as voltage ripple, transients, and interruptions.
The scope of this document is limited to the interface between a SPA-equipped spacecraft and SPAcompliant device. This interface is implemented at a physical SPA endpoint connector, specified in AIAA S-133-4-2013 SPA Physical Interface Standard, which contains details of the connector type, pin assignments, and wiring harnesses. Details of the design of a specific spacecraft electrical power subsystem, including power sources such as solar arrays and power storage devices such as batteries, are not relevant to the SPA power interface described in this document.
languageEnglish
titleAIAA S-133-5num
titleSpace Plug-and-Play Architecture Standard 28V Power Serviceen
typestandard
page21
statusActive
treeAIAA - American Institute of Aeronautics and Astronautics:;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