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Assessing the SEU resistance of CMOS latches using alpha-particle sensitive test circuitsThe importance of Cosmic Rays on the performance of integrated circuits (IC's) in a space environment is evident in the upset rate of the Tracking and Data Relay Satellite (TDRS) launched in Apr. 1983. This satellite experiences a single-event-upset (SEU) per day which must be corrected from the ground. Such experience caused a redesign of the Galileo spacecraft with SEU resistant IC's. The solution to the SEU problem continues to be important as the complexity of spacecraft grows, the feature size of IC's decreases, and as space systems are designed with circuits fabricated at non-radiation hardened foundries. This paper describes an approach for verifying the susceptibility of CMOS latches to heavy-ion induced state changes. The approach utilizes alpha particles to induce the upsets in test circuits. These test circuits are standard cells that have offset voltages which sensitize the circuits to upsets. These results are then used to calculate the upsetability at operating voltages. In this study results are presented for the alpha particle upset of a six-transistor static random access memory (SRAM) cell. Then a methodology is described for the analysis of a standard-cell inverter latch.
Document ID
19940004347
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Buehler, M.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Blaes, B.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Nixon, R.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 16, 2013
Publication Date
November 6, 1990
Publication Information
Publication: Idaho Univ., The 2nd 1990 NASA SERC Symposium on VLSI Design
Subject Category
Electronics And Electrical Engineering
Accession Number
94N71102
Distribution Limits
Public
Copyright
Public Use Permitted.
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