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