DocumentCode :
2178077
Title :
Implementation of FMEA to improve the reliability of GEO satellite payload
Author :
Mozaffari, F. ; Eidi, A. ; Mohammadi, Leila ; Alavi, Z.
Author_Institution :
Satellite Commun. Group, Res. Inst. for ICT, Tehran, Iran
fYear :
2013
fDate :
28-31 Jan. 2013
Firstpage :
1
Lastpage :
6
Abstract :
In this paper, general procedure of failure modes and effects analysis (FMEA) for designing a GEO satellite payload has been implemented and it has been shown that this analysis serves as a useful tool to identify critical items of the product which leads to consider modifications for preventing or compensating failures and finally improving product reliability. The overall actions which have been done using FMEA technique and the design of a redundancy scheme with regard to cost, practical limitations, and system complications lead to an improvement in reliability from 79.15% to 97.52% for preassigned lifetime which can satisfy the desired requirement for this kind of products.
Keywords :
aerospace industry; artificial satellites; reliability; FMEA; GEO satellite payload; failure mode and effect analysis; product reliability; redundancy scheme; Interrupters; Payloads; Power harmonic filters; Redundancy; Reliability engineering; Satellites; FMEA; GEO satellite; reliability;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Reliability and Maintainability Symposium (RAMS), 2013 Proceedings - Annual
Conference_Location :
Orlando, FL
ISSN :
0149-144X
Print_ISBN :
978-1-4673-4709-9
Type :
conf
DOI :
10.1109/RAMS.2013.6517679
Filename :
6517679
Link To Document :
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