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 :
بازگشت