AIAA S-133-5

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

contributor author	AIAA - American Institute of Aeronautics and Astronautics
date accessioned	2017-09-04T15:22:33Z
date available	2017-09-04T15:22:33Z
date copyright	2013.01.01
date issued	2013
identifier other	NCREGFAAAAAAAAAA.pdf
identifier uri	http://yse.yabesh.ir/std;jsery=autho4703177D081D20686159DD6EFDEC9FCD/handle/yse/22714
description 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.
language	English
title	AIAA S-133-5	num
title	Space Plug-and-Play Architecture Standard 28V Power Service	en
type	standard
page	21
status	Active
tree	AIAA - American Institute of Aeronautics and Astronautics:;2013
contenttype	fulltext