DocumentCode :
3379454
Title :
Space radiation effects and reliability considerations for the proposed Jupiter Europa Orbiter
Author :
Johnston, Allan
Author_Institution :
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
fYear :
2011
fDate :
10-14 April 2011
Abstract :
The proposed Jupiter Europa Orbiter (JEO) mission to explore the Jovian moon Europa poses a number of challenges. The spacecraft must operate for about seven years during the transit time to the vicinity of Jupiter, and then endure unusually high radiation levels during exploration and orbiting phases. The ability to withstand usually high total dose levels is critical for the mission, along with meeting the high reliability standards for flagship NASA missions. Reliability of new microelectronic components must be sufficiently understood to meet overall mission requirements.
Keywords :
Jupiter; geophysical prospecting; integrated circuits; radiation effects; reliability; space vehicle electronics; space vehicles; Jovian moon Europa; Jupiter Europa Orbiter; NASA mission; microelectronic component; reliability; space radiation effect; transit time; Integrated circuit reliability; Space missions; Temperature distribution; Testing; Transistors; Voltage control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Reliability Physics Symposium (IRPS), 2011 IEEE International
Conference_Location :
Monterey, CA
ISSN :
1541-7026
Print_ISBN :
978-1-4244-9113-1
Electronic_ISBN :
1541-7026
Type :
conf
DOI :
10.1109/IRPS.2011.5784471
Filename :
5784471
Link To Document :
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