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Reliability Considerations of ULP Scaled CMOS in Spacecraft SystemsNASA, 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.
Document ID
20150005510
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
White, Mark
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
MacNeal, Kristen
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Cooper, Mark
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
April 10, 2015
Publication Date
January 28, 2012
Subject Category
Electronics And Electrical Engineering
Quality Assurance And Reliability
Meeting Information
Meeting: IEEE Reliability and Maintainability Symposium (RAMS)
Location: Orlando, FL
Country: United States
Start Date: January 28, 2012
End Date: January 30, 2012
Sponsors: Institute of Electrical and Electronics Engineers
Distribution Limits
Public
Copyright
Other
Keywords
reliability
spacecraft systems
ultra low power
scaled CMOS

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