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
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