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