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The Impact on Space Radiation Requirements and Effects on ASIMSThe evolution of highly miniaturized electronic and mechanical systems will be accompanied by new problems and issues regarding the radiation response of these systems in the space environment. In this paper we discuss some of the more prominent radiation problems brought about by miniaturization. For example, autonomous micro-spacecraft will require large amounts of high density memory, most likely in the form of stacked, multichip modules of DRAM's, that must tolerate the radiation environment. However, advanced DRAM's (16 to 256 Mbit) are quite susceptible to radiation, particularly single event effects, and even exhibit new radiation phenomena that were not a problem for older, less dense memory chips. Another important trend in micro-spacecraft electronics is toward the use of low-voltage microelectronic systems that consume less power. However, the reduction in operating voltage also caries with it an increased susceptibility to radiation. In the case of application specific integrated microcircuits (ASIM's), advanced devices of this type, such as high density field programmable gate arrays (FPGA's) exhibit new single event effects (SEE), such as single particle reprogramming of anti-fuse links. New advanced bipolar circuits have been shown recently to degrade more rapidly in the low dose rate space environment than in the typical laboratory total dose radiation test used to qualify such devices. Thus total dose testing of these parts is no longer an appropriately conservative measure to be used for hardness assurance. We also note that the functionality of micromechanical Si-based devices may be altered due to the radiation-induced deposition of charge in the oxide passivation layers.
Document ID
19960054134
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Barnes, C.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Johnston, A.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Swift, G.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1995
Subject Category
Quality Assurance And Reliability
Accession Number
96N36380
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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