• 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