DocumentCode
3610081
Title
The Contribution of Low-Energy Protons to the Total On-Orbit SEU Rate
Author
Dodds, N.A. ; Martinez, M.J. ; Dodd, P.E. ; Shaneyfelt, M.R. ; Sexton, F.W. ; Black, J.D. ; Lee, D.S. ; Swanson, S.E. ; Bhuva, B.L. ; Warren, K.M. ; Reed, R.A. ; Trippe, J. ; Sierawski, B.D. ; Weller, R.A. ; Mahatme, N. ; Gaspard, N.J. ; Assis, T. ; Austi
Author_Institution
Sandia Nat. Labs., Albuquerque, NM, USA
Volume
62
Issue
6
fYear
2015
Firstpage
2440
Lastpage
2451
Abstract
Low- and high-energy proton experimental data and error rate predictions are presented for many bulk Si and SOI circuits from the 20-90 nm technology nodes to quantify how much low-energy protons (LEPs) can contribute to the total on-orbit single-event upset (SEU) rate. Every effort was made to predict LEP error rates that are conservatively high; even secondary protons generated in the spacecraft shielding have been included in the analysis. Across all the environments and circuits investigated, and when operating within 10% of the nominal operating voltage, LEPs were found to increase the total SEU rate to up to 4.3 times as high as it would have been in the absence of LEPs. Therefore, the best approach to account for LEP effects may be to calculate the total error rate from high-energy protons and heavy ions, and then multiply it by a safety margin of 5. If that error rate can be tolerated then our findings suggest that it is justified to waive LEP tests in certain situations. Trends were observed in the LEP angular responses of the circuits tested. Grazing angles were the worst case for the SOI circuits, whereas the worst-case angle was at or near normal incidence for the bulk circuits.
Keywords
nuclear electronics; shielding; space vehicles; LEP angular responses; bulk SOI circuits; bulk Si circuits; error rate predictions; grazing angles; heavy ions; high-energy proton experimental data; low-energy proton error rates; low-energy proton experimental data; nominal operating voltage; normal incidence; secondary protons; spacecraft shielding; total on-orbit single-event upset rate; worst-case angle; Error analysis; Protons; Random access memory; Silicon; Silicon-on-insulator; Single event upsets; Space vehicles; Angular effects; error rate prediction; proton direct ionization; secondary protons; single-event effects (SEEs);
fLanguage
English
Journal_Title
Nuclear Science, IEEE Transactions on
Publisher
ieee
ISSN
0018-9499
Type
jour
DOI
10.1109/TNS.2015.2486763
Filename
7323869
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