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Dive into the research topics where Michael J. Campola is active.

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Featured researches published by Michael J. Campola.


IEEE Transactions on Nuclear Science | 2009

Impact of Low-Energy Proton Induced Upsets on Test Methods and Rate Predictions

Brian D. Sierawski; Jonathan A. Pellish; Robert A. Reed; Ronald D. Schrimpf; Kevin M. Warren; Robert A. Weller; Marcus H. Mendenhall; Jeffrey D. Black; Alan D. Tipton; Michael A. Xapsos; Robert C. Baumann; Xiaowei Deng; Michael J. Campola; Mark R. Friendlich; Hak S. Kim; Anthony M. Phan; Christina M. Seidleck

Direct ionization from low energy protons is shown to cause upsets in a 65-nm bulk CMOS SRAM, consistent with results reported for other deep submicron technologies. The experimental data are used to calibrate a Monte Carlo rate prediction model, which is used to evaluate the importance of this upset mechanism in typical space environments. For the ISS orbit and a geosynchronous (worst day) orbit, direct ionization from protons is a major contributor to the total error rate, but for a geosynchronous (solar min) orbit, the proton flux is too low to cause a significant number of events. The implications of these results for hardness assurance are discussed.


IEEE Transactions on Nuclear Science | 2008

Device-Orientation Effects on Multiple-Bit Upset in 65 nm SRAMs

Alan D. Tipton; Jonathan A. Pellish; John M. Hutson; Robert C. Baumann; Xiaowei Deng; Andrew Marshall; Michael A. Xapsos; Hak S. Kim; Mark R. Friendlich; Michael J. Campola; Christina M. Seidleck; Kenneth A. LaBel; Marcus H. Mendenhall; Robert A. Reed; Ronald D. Schrimpf; Robert A. Weller; Jeffrey D. Black

The effects of device orientation on heavy ion-induced multiple-bit upset (MBU) in 65 nm SRAMs are examined. The MBU response is shown to depend on the orientation of the device during irradiation. The response depends on the direction of the incident ion to the n- and p-wells of the SRAM. The MBU response is simulated using Monte Carlo methods for a space environment. The probability is calculated for event size. Single-bit upsets in the space environment account for 90% of all events with exponentially decreasing probabilities of larger MBU events.


IEEE Transactions on Nuclear Science | 2009

Evidence for Lateral Angle Effect on Single-Event Latchup in 65 nm SRAMs

John M. Hutson; Jonathan A. Pellish; Alan D. Tipton; G. Boselli; Michael A. Xapsos; Hak S. Kim; Mark R. Friendlich; Michael J. Campola; S. Seidleck; Kenneth A. LaBel; Andrew Marshall; Xiaowei Deng; Robert C. Baumann; Robert A. Reed; Ronald D. Schrimpf; Robert A. Weller; Lloyd W. Massengill

Single event latchup (SEL) in a 65 nm CMOS SRAM technology due to heavy ions is observed and device sensitivity is shown to be a strong function of lateral beam orientation, angle of incidence, and temperature. Experimental results show the importance of testing at multiple lateral beam orientations to properly characterize device sensitivity.


radiation effects data workshop | 2010

Recent Single Event Effects Compendium of Candidate Electronics for NASA Space Systems

Martha V. O'Bryan; Kenneth A. LaBel; Jonathan A. Pellish; Jean-Marie Lauenstein; Dakai Chen; Cheryl J. Marshall; Timothy R. Oldham; Hak S. Kim; Anthony M. Phan; Melanie D. Berg; Michael J. Campola; Anthony B. Sanders; Paul W. Marshall; Michael A. Xapsos; David F. Heidel; Kenneth P. Rodbell; Jim W. Swonger; Don Alexander; Michael Gauthier; Brian Gauthier

We present the results of single event effects (SEE) testing and investigating the effects of space radiation on electronics. This paper is a summary of test results.


IEEE Transactions on Nuclear Science | 2015

Improved Model for Increased Surface Recombination Current in Irradiated Bipolar Junction Transistors

Hugh J. Barnaby; B. Vermeire; Michael J. Campola

Current gain degradation in irradiated bipolar junction transistors is primarily due to excess base current caused by enhanced carrier recombination in the emitter-base space-charge region (SCR). Radiation-induced traps at the interface between silicon and the bipolar base oxide facilitate the recombination process primarily above the sensitive emitter-base junction. This leads to an increase in surface recombination current in the SCR, which is a non-ideal component of the BJTs base current characteristic under active bias conditions. In this paper, we derive a precise analytical model for surface recombination current that captures bias dependencies typically omitted from traditional models. This improved model is validated by comparisons to these traditional approaches.


radiation effects data workshop | 2012

Compendium of Current Total Ionizing Dose and Displacement Damage for Candidate Spacecraft Electronics for NASA

Michael J. Campola; Donna J. Cochran; Alvin J. Boutte; Dakai Chen; Robert A. Gigliuto; Kenneth A. LaBel; Jonathan A. Pellish; Raymond L. Ladbury; Megan C. Casey; Edward P. Wilcox; Martha V. O'Bryan; Jean-Marie Lauenstein; Dan Violette; Michael A. Xapsos

Total ionizing dose and displacement damage testing is performed to characterize and determine the suitability of candidate electronics for NASA spacecraft and program use.


IEEE Transactions on Nuclear Science | 2010

Heavy Ion Testing With Iron at 1 GeV/amu

Jonathan A. Pellish; Michael A. Xapsos; Kenneth A. LaBel; Paul W. Marshall; David F. Heidel; Kenneth P. Rodbell; Mark C. Hakey; Paul E. Dodd; M.R. Shaneyfelt; James R. Schwank; Robert C. Baumann; Xiaowei Deng; Andrew Marshall; Brian D. Sierawski; Jeffrey D. Black; Robert A. Reed; Ronald D. Schrimpf; Hak S. Kim; Melanie D. Berg; Michael J. Campola; Mark R. Friendlich; Christopher E. Perez; Anthony M. Phan; Christina M. Seidleck

A 1 GeV/amu 56Fe ion beam allows for true 90° tilt irradiations of various microelectronic components and reveals relevant upset trends at the GCR flux energy peak. Three SRAMs and an SRAM-based FPGA evaluated at the NASA Space Radiation Effects Laboratory demonstrate that a 90° tilt irradiation yields a unique device response. These tilt angle effects need to be screened for, and if found, pursued with radiation transport simulations to quantify their impact on event rate calculations.


radiation effects data workshop | 2009

Total Ionizing Dose and Displacement Damage Compendium of Candidate Spacecraft Electronics for NASA

Donna J. Cochran; Stephen P. Buchner; Dakai Chen; Hak S. Kim; Kenneth A. LaBel; Timothy R. Oldham; Michael J. Campola; Martha V. O'Bryan; Raymond L. Ladbury; Cheryl J. Marshall; Anthony B. Sanders; Michael A. Xapsos

Vulnerability of a variety of candidate spacecraft electronics to total ionizing dose and displacement damage is studied. Devices tested include optoelectronics, digital, analog, linear bipolar devices, and hybrid devices.


european conference on radiation and its effects on components and systems | 2009

Heavy ion testing at the galactic cosmic ray energy peak

Jonathan A. Pellish; Michael Xapsos; K. A. LaBel; Paul W. Marshall; David F. Heidel; Kenneth P. Rodbell; Mark C. Hakey; Paul E. Dodd; M.R. Shaneyfelt; James R. Schwank; Robert C. Baumann; Xiaowei Deng; Andrew Marshall; Brian D. Sierawski; Jeffrey D. Black; Robert A. Reed; Ronald D. Schrimpf; Hak S. Kim; Melanie D. Berg; Michael J. Campola; Mark R. Friendlich; Christopher E. Perez; Anthony M. Phan; Christina M. Seidleck

A 1 GeV/u 56Fe ion beam allows for true 90° tilt irradiations of various microelectronic components and reveals relevant upset trends for an abundant element at the GCR flux energy peak.


IEEE Transactions on Nuclear Science | 2013

Bayesian Methods for Bounding Single-Event Related Risk in Low-Cost Satellite Missions

Raymond L. Ladbury; Michael J. Campola

Adapting conventional SEE hardness assurance approaches to low-cost, risk tolerant missions has proven difficult. Such approaches do not have a natural approach for realizing cost savings for increased risk tolerance. We develop single-event-risk prior probability distributions based on historical and heritage data. The Priors can be used to bound SEE risk for testing, part selection and design. By adjusting the desired confidence and success probability for the prior, one can tailor it to the risk tolerance of the mission.

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Kenneth A. LaBel

Goddard Space Flight Center

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Edward P. Wilcox

Goddard Space Flight Center

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Megan C. Casey

Goddard Space Flight Center

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Michael A. Xapsos

Goddard Space Flight Center

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Melanie D. Berg

Goddard Space Flight Center

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Raymond L. Ladbury

Goddard Space Flight Center

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