• DocumentCode
    817713
  • Title

    Transient SEUs in a fiber optic system for space applications

  • Author

    LaBel, Ken ; Stassinopoulos, E.G. ; Brucker, G.J.

  • Author_Institution
    NASA/Goddard Space flight Center, Greenbelt, MD, USA
  • Volume
    38
  • Issue
    6
  • fYear
    1991
  • fDate
    12/1/1991 12:00:00 AM
  • Firstpage
    1546
  • Lastpage
    1550
  • Abstract
    The results of an investigation on the SEU sensitivity for a fiber optic operating system are reported. Measurements were made on the upset cross sections for the system in static and dynamic modes of operation. The heavy ion SEU test facility at Brookhaven and the proton facility at Harvard University were used in this study. Cross sections were obtained for Honeywell transmitter and receiver devices operating in a system at a frequency of 100 kHz. Both devices were independently irradiated. The results show that the dynamic mode was the worst case, and the receiver was the most sensitive part type in the system. The threshold linear energy transfer (LET) for the receiver was determined to be 1.6 MeV.cm 2/mg for the three input signals used in the tests, which were: a continuous high state, a low state, and a 100 kHz square wave
  • Keywords
    aerospace instrumentation; environmental testing; ion beam effects; optical links; optical testing; proton effects; transients; Honeywell receiver; Honeywell transmitter; SEU sensitivity; dynamic mode; fiber optic operating system; heavy ion SEU test facility; proton facility; space applications; spacecraft systems; static mode; threshold linear energy transfer; transient SEUs; upset cross sections; Optical fiber cables; Optical fibers; Optical receivers; Optical transmitters; Protons; Single event transient; Single event upset; Space vehicles; Test facilities; Testing;
  • fLanguage
    English
  • Journal_Title
    Nuclear Science, IEEE Transactions on
  • Publisher
    ieee
  • ISSN
    0018-9499
  • Type

    jour

  • DOI
    10.1109/23.124144
  • Filename
    124144