No description available.

The purpose of this study is to improve spacecraft shielding from radiation in space. It focuses on the evaluation of shielding efficiency of different materials. The efficiency of a shield is evaluated by the dose profile within the shield and the amount of dose absorbed by a target using the Monte Carlo transport code called FLUKA. The output of this code is validated by recreating the experiments from published papers and comparing the results. Once the FLUKA’s output is validated, the efficiency of sixteen materials, subject to SPE and GCR sources, are evaluated. The efficiency comparison is made by fixing the area density of a shield. It was found that polyethylene, water, carbon and silicon outperform aluminum – the primary metal used in spacecraft. In case of composite shield, made of layers of different materials, the 3Carb-9Al combination has better performance than the shield made just of aluminum. This holds true for both Solar Particle Events (SPEs) and Galactic Cosmic Ray (GCR). However, the choice of material is more efficient at shielding from SPE particles rather than from GCR. In case of GCR, the choice of materials is found to have rather small effect on the efficiency of a shield. The percent difference between the rate of dose absorption by a target, shielded by different materials, is within about 9%. Secondary particles make a significant contribution to the target’s dose. For SPEs, the secondary particles are primarily electrons and neutrons. For GCRs, the secondary particles are primarily pions, α-particles and electrons. Protons contribute more than 50% to the target’s dose in both cases.

No description available.

Motivated by an increasing demand for functionality and reliability of systems operating in harsh, ionizing-radiation environments, the core of the present research is an investigation of the response of rare-earth-doped, aluminosilicate fibers to ionizing radiation. These rare-earth-doped fibers, consisting of fibers doped with ions of erbium (Er³⁺) and ytterbium (Yb³⁺) designed for use in amplifier systems, reveal average specific losses in response to ⁶⁰Co gamma radiation to be in the range of 0.0285 - 0.193 dB/(m•krad(Si)) at wavelengths from 1300 nm to 1400 nm. An ionizing dose rate dependence was identified in which high dose rates of approximately 40 rad(Si)/s invariably lead to higher induced losses than lower dose rates of approximately 14 rad(Si)/s, indicating the possibility of complex radiation-related phenomena underlying the observed absorption. Data clearly show that Er³⁺-doped fibers are more sensitive to ionizing-radiation in comparison to Yb³⁺-doped fibers, while Er³⁺/Yb³⁺ co-doped fibers are found to be the least sensitive to radiation of all the fibers examined. Evidence of color center formation associated with the dopant aluminum is found in results of visible spectroscopy conducted on gamma-irradiated preform samples and on fibers flown in low-Earth orbit. Near infrared spectroscopic data is consistent with absorption derived from this dopant as well, with the interpretation of band-tailing from the visible portion of the spectrum. Evidence of the formation of a defect intrinsic to the silicate host matrix, the Non-Bridging Oxygen Hole Center (NBOHC), is also found following ionizing radiation of the optical fiber preforms. Since the observed ionizing-radiation-induced absorption is concentrated in the visible portion of the spectrum, the performance of actively operated rare-earth-doped amplifiers is largely impacted by the pump wavelength, which is located at higher energies within the near-infrared portion of the spectrum and therefore closer to the visible portion of the spectrum than the lasing wavelength. Experimental results stemming from rare-earth-doped amplifiers operated under ionizing radiation substantiate the importance of the pumping wavelength, and suggest the presence of cascaded pump photon absorption processes. Based on these results, pumping at longer wavelengths is advised to reduce the effect of color center absorption on this crucial aspect of active fiber amplifier operation.

Space radiation and its effects on human life and sensitive equipment are of concern to a safe exploration of space. Radiation fields are modified in quality and quantity by intervening shielding materials. The modification of space radiation by shielding materials is modeled by deterministic transport codes using the Boltzmann transport equation. Databases of cross sections for particle production are needed as input for transport codes. A simple model of nucleon-nucleon interactions is developed and used to derive differential and total cross sections. The validity of the model is verified for proton-proton elastic scattering and applied to delta-resonance production. Additionally, a comprehensive validation program of the nucleus-nucleus fragmentation cross section models NUCFRG2 and QMSFRG is performed. A database of over 300 experiments was assembled and used to compare to model fragmentation cross sections.

Space radiation is significantly harmful to electronic Components. The operating time, duration and orbit of the space mission are affected by the characteristic of the radiation environment. The aging and the performance of the electronic components are modified by radiation. The performance of the space systems such as electronic units, sensors, power and power subsystem units, batteries, payload equipments, communication units, remote sensing instruments, data handling units, externally located units, and propulsion subsystem units is determined by the properly functioning of various electronic systems. Such systems are highly sensitive against space radiation. The space radiation can cause damage to electronic components or functional failure on the electronics. A precisely methodology is needed to ensure that space radiation is not a threat on the functionality and performance of the electronics during their operational lives. This methodology is called as &rdquo / Radiation Hardness Assurance&rdquo / . In this thesis, the hardening of electronics against space radiation is discussed. This thesis describes the space radiation environments, physical mechanisms, effects of space radiation, models of the space radiation environment, simulation of the Total Ionizing Dose, and &rdquo / Radiation Hardness Assurance&rdquo / which covers Total Ionizing Dose and Single Event Effects testing and analyzing of the electronics.

Cette thèse porte sur le développement d'un capteur de pixel monolithique CMOS utilisé pourl’identification et le comptage des particules ionisés dan l’espace avec un flux élevé. Un nouveauconcept pour l’identification de l’espèce des particules proposé dans la présente étude, est basésur l'analyse des amas de particules déclenchés. Pour valider ce nouveau concept, un capteur detaille complet, qui comprend la matrice de pixel sensible aux particules ionisés signal, une chaînede traitement du signal analogique, un convertisseur analogue numérique de 3 bits, et untraitement du signal numérique a été conçu dans un processus de 0.35 μm. Le capteur sortiedirectement des informations de flux à travers 4 canaux avec un débit de données très faible(80 bps) et dissipation d’énergie minimale (~ 100 mW). Chaque canal représente particules avecdifférentes espèces et les énergies. La densité maximum de flux mesurable est jusqu'à 108particules/cm2/s (coups s'accumulent < 5%). Un prototype à échelle réduite a été fabriqué et testéavec trois types d'illumination de rayonnement (rayons X, les électrons et laser infrarouge). Tousles résultats obtenus valident le nouveau concept proposé. Un moniteur de rayonnement spatialtrès miniaturisé basé sur un capteur de pixel CMOS peut être prévu. Le moniteur peut présente lesmêmes performances que les compteurs actuels, mais avec une dissipation de puissance réduited'un ordre de grandeur qu'un poids, un volume d'encombrement et un coût moindre. En outre, enraison de ses sorties de haut niveau et faible débit de données, aucune traitement supplémentairedu signal dehors du capteur est nécessaire, ce qui le rend particulièrement attrayant pour desapplications dan les petits satellitaires. / This thesis focuses on the development of a CMOS monolithic pixel sensor used for space ionizingparticles identification and counting in high flux. A new concept for single particle identification isproposed in this study, which is based on the analysis of particle triggered clusters. To validate thisnew concept, a full size sensor including the sensitive pixel matrix, an analogue signal processingchain, a 3-bit analogue to digital converter, and a digital processing stage was designed in a 0.35μm process. The sensor directly output particles flux information through 4 channels with a verylow data rate (80 bps) and minimal power dissipation (~ 100mW). Each channel representsparticles with different species and energies. The highest measurable flux density is up to 108particles/cm2/s (hits pile up < 5%). A reduced scale prototype was fabricated and tested with 3types of radiation illumination (X-ray, electrons and infrared laser). All the results obtained validatethe proposed new concept and a highly miniaturized space radiation monitor based on a singleCMOS pixel sensor could be foreseen. The monitor could provide measurements of comparable orbetter quality than existing instruments, but at around an order of magnitude lower powerconsumption, mass and volume and a lower unit cost. Moreover, due to its high level and low datarate outputs, no signal treatment power aside the sensor is required which makes it especiallyattractive for small satellite application.