DocumentCode
1434574
Title
Spacecraft electronics design for radiation tolerance
Author
Rasmussen, Robert D.
Author_Institution
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
Volume
76
Issue
11
fYear
1988
fDate
11/1/1988 12:00:00 AM
Firstpage
1527
Lastpage
1537
Abstract
Current 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
Keywords
digital integrated circuits; integrated circuit technology; integrated circuit testing; radiation hardening (electronics); reliability; space vehicles; design practices; electronics design; future trends; radiation effects; radiation tolerance requirements; spacecraft designs; spacecraft electronics; testability issues; Aerospace electronics; Electromagnetic radiation; Magnetic devices; Magnetic flux; Optical materials; Propulsion; Radiation effects; Radiation hardening; Space technology; Space vehicles;
fLanguage
English
Journal_Title
Proceedings of the IEEE
Publisher
ieee
ISSN
0018-9219
Type
jour
DOI
10.1109/5.90116
Filename
90116
Link To Document