航天器系统中ULP缩放CMOS的可靠性考虑

M. White, K. MacNeal, M. Cooper
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引用次数: 0

摘要

随着技术继续向亚微米深度扩展,NASA、航空航天界和其他高可靠性(高可靠性)的先进微电子产品用户面临着许多挑战。减小CMOS器件的特征尺寸不仅允许在单个芯片上放置更多组件,而且与更大规模的器件相比,它通过允许更快的开关(或时钟)速度和更低的功耗来提高性能。超低功耗(ULP)微电子器件具有更高的性能和更低的工作和待机功率特性,这不仅是理想的,而且是满足关键航天器系统低功耗设计目标所必需的。然而,在这样的系统中集成这些组件必须与项目的整体风险承受能力相平衡。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Reliability considerations of ULP scaled CMOS in spacecraft systems
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.
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