Relevant bibliographies by topics / Non-ionizing displacement dose

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  1. Journal articles
  2. Dissertations / Theses

Academic literature on the topic 'Non-ionizing displacement dose'

Author: Grafiati
Published: 5 October 2024
Last updated: 31 July 2025

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Journal articles on the topic "Non-ionizing displacement dose"

1

Foster, Charles C. "Total Ionizing Dose and Displacement-Damage Effects in Microelectronics." MRS Bulletin 28, no. 2 (2003): 136–40. http://dx.doi.org/10.1557/mrs2003.42.

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AbstractWhen exposed to radiation, the function of microelectronic devices is not only degraded by single-event phenomena but by cumulative effects. Most of the energy lost by radiation passing through semiconductors is through ionization. Buildup of charge in gate oxide layers and of interface and border traps due to ionization result in semipermanent damage to the device. These effects are known as total ionizing dose effects. A fraction of the energy of the radiation passing through semiconductors is lost to displacement of atoms from their sites in the crystal lattice structure. The buildu
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2

Xun, Mingzhu, Yudong Li, and Mingyu Liu. "Comparison of Proton and Gamma Irradiation on Single-Photon Avalanche Diodes." Electronics 13, no. 6 (2024): 1086. http://dx.doi.org/10.3390/electronics13061086.

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In this paper, the effects of proton and gamma irradiation on reach-through single-photon avalanche diodes (SPADs) are investigated. The I–V characteristics, gain and spectral response of SPAD devices under proton and gamma irradiation were measured at different proton energies and irradiation bias conditions. Comparison experiments of proton and gamma irradiation were performed in the radiation environment of geosynchronous transfer orbit (GTO) with two different radiation shielding designs at the same total ionizing dose (TID). The results show that after 30 MeV and 60 MeV proton irradiation
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3

Peters, Anthony, Matthias Preindl, and Vasilis Fthenakis. "Semiconductor Material Damage Mechanisms Due to Non-Ionizing Energy in Space-Based Solar Systems." Energies 18, no. 3 (2025): 509. https://doi.org/10.3390/en18030509.

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Radiation impacts on space-based systems operating on various orbits are evaluated in this paper. Specifically, satellite operations in Low Earth Orbit (LEO), Medium Earth Orbit (MEO), and Geosynchronous Orbit (GEO) are analyzed. Special focus is given on quantifying the effect of high-energy particle space radiation on materials used for critical power components, where component fault can lead to total mission failure. Methods, using multiple computational platforms for the quantification of non-ionizing energy loss (NIEL) and displacement damage dose (DDD), are used to assess semiconductor
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4

Yang Wei-Tao, Wu Yi-Chen, Xu Rui-Ming, et al. "Hg<sub>1-x</sub>Cd<sub>x</sub>Te Infrared Focal Plane Arrays Image Sensor Space Proton Displacement Damage and Total Ionizing Dose Effects Geant4 Simulation." Acta Physica Sinica 73, no. 21 (2024): 0. http://dx.doi.org/10.7498/aps.73.20241246.

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A large-format, high-resolution Hg&lt;sub&gt;1-x&lt;/sub&gt;Cd&lt;sub&gt;x&lt;/sub&gt;Te infrared focal plane array (IRFPA) image sensor can be used in aerospace remote sensing and high-precision satellite imaging. The next generation of meteorological satellites in China will fully adopt this type of image sensor. However, space high-energy protons can cause displacement damage effects in Hg&lt;sub&gt;1-x&lt;/sub&gt;Cd&lt;sub&gt;x&lt;/sub&gt;Te IRFPA detectors and induce total ionizing dose (TID) effects in the pixel unit metal-oxide-semiconductor (MOS) transistors. This paper focuses on a 55
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5

Qi, Xuan. "Near-space radiation environment analysis and protective measures." Theoretical and Natural Science 52, no. 1 (2024): 1–9. http://dx.doi.org/10.54254/2753-8818/52/2024ch0112.

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As a matter of fact, near space radiation environment analysis plays a crucial role in near space physics. With this in mind, this study introduces the types of radiation damage in the near-space radiation environment as well as corresponding protective measures. To be specific, the protective strategy for Total Ionizing Dose (TID) and for Displacement Damage (DD) are similar, focusing on material shielding to mitigate the effects. According to the analysis, the guiding principle for the protection strategy against Single Event Effects (SEE) is risk management, aiming to minimize the probabili
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6

Iwamoto, Yosuke, and Tatsuhiko Sato. "Development of a method for calculating effective displacement damage doses in semiconductors and applications to space field." PLOS ONE 17, no. 11 (2022): e0276364. http://dx.doi.org/10.1371/journal.pone.0276364.

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The displacement damage dose (DDD) is a common index used to predict the life of semiconductor devices employed in space-based environments where they will be exposed to radiation. The DDD is commonly estimated from the non-ionizing energy loss based on the Norgett-Robinson-Torrens (NRT) model, although a new definition for a so-called effective DDD considers the molecular dynamic (MD) simulation with the amorphization in semiconductors. The present work developed a new model for calculating the conventional and effective DDD values for silicon carbide (SiC), indium arsenide (InAs), gallium ar
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7

Gurimskaya, Yana, Alex Fedoseyev, and Stanislau Herasimenka. "Combined electron and proton radiation effects on solar cells for earth orbit." Journal of Physics: Conference Series 2910, no. 1 (2024): 012015. https://doi.org/10.1088/1742-6596/2910/1/012015.

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Abstract We present a computational approach for accurate calculations of the combined effects of electron and proton radiation in space, tailored to a specific orbit and accounting for the full range of particle energies. The radiation-induced defect formation is shown to depend on the NIEL (Non-Ionizing Energy Loss), which reflects the small fraction of particle energy (from electrons, protons or other ions) lost through the ionisation of the material. The model developed by the Naval Research Laboratory (NRL) for predicting solar cell degradation based on NIEL aligns closely with the result
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8

Ahmed, S., D. J. Hall, J. M. Skottfelt, et al. "Modelling the impact of radiation damage effects in in-flight and on-ground irradiated Gaia CCDs." Journal of Instrumentation 17, no. 08 (2022): C08010. http://dx.doi.org/10.1088/1748-0221/17/08/c08010.

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Abstract The European Space Agency’s Gaia spacecraft was launched in 2013 and has been in operation ever since. It has a focal plane of 106 Charge-Coupled Devices (CCDs) which are of the CCD91-72 variant, custom designed by Teledyne e2v. The detectors have been making measurements of parallaxes, positions, velocities, and other physical properties of over one billion stars and other astronomical objects in the Milky Way. Whilst operating in space, CCDs undergo non-ionizing displacement damage from incoming radiation. This causes radiation induced trap defects to form in the silicon lattice whi
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9

Huffman, Nickelas, Ajay Nair, Summer M. Drees, et al. "Radiation Exposure in Operatively Treated Pediatric Femur Fracture Patients." Journal of Pediatric Orthopaedics, February 4, 2025. https://doi.org/10.1097/bpo.0000000000002907.

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Background: Children who sustain femur fractures are exposed to medical radiation as part of their treatment. In addition to standard radiographs and fluoroscopy, computerized tomography (CT) is a major source of ionizing radiation (IR). These patients frequently undergo CT scans during their treatment. The aim of the current study was to quantify the factors associated with greater IR exposure in children with operatively treated femur fractures and compare radiation exposure among those who received CT scans versus those who did not. Methods: Thirty-eight patients below 18 years old with ope
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Kirmani, Ahmad R., Todd A. Byers, Zhenyi Ni, et al. "Unraveling radiation damage and healing mechanisms in halide perovskites using energy-tuned dual irradiation dosing." Nature Communications 15, no. 1 (2024). http://dx.doi.org/10.1038/s41467-024-44876-1.

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AbstractPerovskite photovoltaics have been shown to recover, or heal, after radiation damage. Here, we deconvolve the effects of radiation based on different energy loss mechanisms from incident protons which induce defects or can promote efficiency recovery. We design a dual dose experiment first exposing devices to low-energy protons efficient in creating atomic displacements. Devices are then irradiated with high-energy protons that interact differently. Correlated with modeling, high-energy protons (with increased ionizing energy loss component) effectively anneal the initial radiation dam
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Dissertations / Theses on the topic "Non-ionizing displacement dose"

1

Ferraro, Rudy. "Development of Test Methods for the Qualification of Electronic Components and Systems Adapted to High-Energy Accelerator Radiation Environments." Thesis, Montpellier, 2019. http://www.theses.fr/2019MONTS118.

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Le Grand collisionneur de hadrons (LHC), le plus grand et le plus puissant au monde, a démarré en 2008 et constitue la dernière étape du complexe des accélérateurs du CERN. Le LHC consiste en un anneau de 27 kilomètres d'aimants supraconducteurs permettant d'accélérer deux faisceaux jusqu'à 7 TeV avant de les faire entrer en collision à 14 TeV dans l'une des cinq expériences de contrôle du résultat de la collision. Le LHC a notamment permis la découverte du boson de Higgs et d'autres particules baryoniques prédites par le modèle standard. L'environnement de rayonnement du LHC et de ses lignes
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Colcombet, Paul. "Étude de photorécepteurs sous irradiation de protons, électrons et rayons gamma pour la mission LISA." Electronic Thesis or Diss., Université Côte d'Azur, 2024. http://www.theses.fr/2024COAZ5022.

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Programmée pour 2035, la mission LISA (Laser Interferometer Space Antenna), pilotée par l'Agence spatiale européenne (ESA), marquera une première en devenant le premier détecteur spatial d'ondes gravitationnelles. Opérant dans la gamme des basses fréquences de 0,1 mHz à 1 Hz inaccessible aux détecteurs terrestres, LISA ouvrira une nouvelle fenêtre sur notre univers et une nouvelle ère dans l'étude de la cosmologie. Le design de LISA présente trois vaisseaux formant un triangle équilatéral de 2,5 millions de km de côté, suivant la Terre dans son orbite autour du Soleil. Au cœur du fonctionnemen
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