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Spacecraft electronics design for radiation toleranceCurrent design practices are described and future trends in spacecraft electronics which are likely to alter traditional approaches are discussed. A summary of radiation effects and radiation tolerance requirements typically levied on spacecraft designs is provided. Methods of dealing with radiation and testability issues are considered.
Document ID
19890035069
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
External Source(s)
Authors
Rasmussen, Robert D.
(California Institute of Technology Jet Propulsion Laboratory, Pasadena, United States)
Date Acquired
August 14, 2013
Publication Date
November 1, 1988
Publication Information
Publication: IEEE, Proceedings
Volume: 76
ISSN: 0018-9219
Subject Category
Electronics And Electrical Engineering
Accession Number
89A22440
Distribution Limits
Public
Copyright
Other

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