DocumentCode
1856608
Title
Space-hardware design for long life with high reliability
Author
Gindorf, Tom E. ; Miles, Ralph F. ; Murphy, Gerald B.
Author_Institution
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
fYear
1994
fDate
24-27Jan 1994
Firstpage
338
Lastpage
341
Abstract
In 1991, the Cassini Project, NASA´s planetary project to place a spacecraft in orbit about Saturn, funded a study at the Jet Propulsion Laboratory (JPL) to identify rules for design and test of hardware required to function reliably in space for very long lifetimes. Twenty-nine subjects were considered comprising 130 specific rules related to long-life issues such as accelerated life testing, cycling of mechanical devices, selection and application of parts, semiconductor junction temperatures, and worst-case analysis for long life. The study was subsequently published as a JPL document. One major conclusion of the workshop was that unattended space missions extending out to 25 years or more are feasible. The paper reports on the study and the one-day workshop
Keywords
life testing; reliability; software reliability; Cassini Project; Jet Propulsion Laboratory; NASA´s planetary project; Saturn; accelerated life testing; cycling; high reliability; long life; mechanical devices; semiconductor junction temperatures; space-hardware design; worst-case analysis; Hardware; Laboratories; Life estimation; Life testing; Planetary orbits; Propulsion; Saturn; Space missions; Space vehicles; Temperature;
fLanguage
English
Publisher
ieee
Conference_Titel
Reliability and Maintainability Symposium, 1994. Proceedings., Annual
Conference_Location
Anaheim, CA
Print_ISBN
0-7803-1786-6
Type
conf
DOI
10.1109/RAMS.1994.291131
Filename
291131
Link To Document