DocumentCode
2179362
Title
Reliability considerations of ULP scaled CMOS in spacecraft systems
Author
White, M. ; MacNeal, K. ; Cooper, M.
Author_Institution
Electr. Parts Eng. & Reliability, Jet Propulsion Lab. .Pasadena, Pasadena, CA, USA
fYear
2013
fDate
28-31 Jan. 2013
Firstpage
1
Lastpage
6
Abstract
NASA, the aerospace community, and other high reliability (hi-rel) users of advanced microelectronic products face many challenges as technology continues to scale into the deep sub-micron region. Decreasing the feature size of CMOS devices not only allows more components to be placed on a single chip, but it increases performance by allowing faster switching (or clock) speeds with reduced power compared to larger scaled devices. Higher performance, and lower operating and stand-by power characteristics of Ultra-Low Power (ULP) microelectronics are not only desirable, but also necessary to meet low power consumption design goals of critical spacecraft systems. The integration of these components in such systems, however, must be balanced with the overall risk tolerance of the project.
Keywords
CMOS integrated circuits; power consumption; semiconductor device reliability; space vehicle electronics; ULP scaled CMOS; advanced microelectronic products; aerospace community; deep submicron region; reliability consideration; risk tolerance; single chip; spacecraft systems; ultra-low power microelectronics; CMOS integrated circuits; Circuit faults; Microelectronics; Power demand; Random access memory; Reliability; Space vehicles; Reliability; scaled CMOS; spacecraft systems; ultra-low power;
fLanguage
English
Publisher
ieee
Conference_Titel
Reliability and Maintainability Symposium (RAMS), 2013 Proceedings - Annual
Conference_Location
Orlando, FL
ISSN
0149-144X
Print_ISBN
978-1-4673-4709-9
Type
conf
DOI
10.1109/RAMS.2013.6517720
Filename
6517720
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