DocumentCode :
1307702
Title :
Single event test methodology and test results of commercial gigabit per second Fiber Channel hardware
Author :
Carts, M.A. ; Marshall, P.W. ; Marshall, C.J. ; LaBel, K.A. ; Flanegan, M. ; Bretthaue, J.
Author_Institution :
Naval Res. Lab., Washington, DC, USA
Volume :
44
Issue :
6
fYear :
1997
fDate :
12/1/1997 12:00:00 AM
Firstpage :
1878
Lastpage :
1884
Abstract :
This article presents a detailed description of the single event test methods used to evaluate two different component sets conforming to the Fiber Channel (FC) commercial high-speed serial bus standard. The devices tested perform the hierarchically low-level functions such as transmission coding and actual electrical or optical linking. Pertinent portions of the FC specification, and details of the test setup and methods are presented prior to description of the observed error types, correlation of error types to source circuitry, and radiation test results. The authors conclude that one of these COTS device sets may be suitable for space use with the use of additional circuit hardening, and that the other (also a COTS device set) is not suitable for space use. The test methods and descriptions of error types should prove useful in preparation for future FC component SEE testing
Keywords :
aerospace testing; data communication; optical fibre communication; optical fibre testing; optical fibres; optical links; radiation hardening (electronics); Fiber Channel hardware; SEE testing; circuit hardening; hierarchically low-level functions; high-speed serial bus standard; observed error types; optical linking; radiation test results; single event test methodology; space use; transmission coding; Circuit testing; NASA; Optical devices; Optical fiber communication; Optical fiber testing; Optical fibers; Optical sensors; Performance evaluation; Space technology; Space vehicles;
fLanguage :
English
Journal_Title :
Nuclear Science, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9499
Type :
jour
DOI :
10.1109/23.658956
Filename :
658956
Link To Document :
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