Código híbrido avanzado de motores de plasma de efecto Hall

La propulsión eléctrica constituye hoy una tecnología muy competitiva y de gran proyección de futuro. Dentro de los diversos motores de plasma existentes, el motor de efecto Hall ha adquirido una gran madurez y constituye un medio de propulsión idóneo para un rango amplio de misiones. En la presente Tesis se estudian los motores Hall con geometría convencional y paredes dieléctricas. La compleja interacción entre los múltiples fenómenos físicos presentes hace que sea difícil la simulación del plasma en estos motores. Los modelos híbridos son los que representan un mejor compromiso entre precisión y tiempo de cálculo. Se basan en utilizar un modelo fluido para los electrones y algoritmos de dinámica de partículas PIC (Particle-In- Cell) para los iones y los neutros. Permiten hacer uso de la hipótesis de cuasineutralidad del plasma, a cambio de resolver separadamente las capas límite (o vainas) que se forman en torno a las paredes de la cámara. Partiendo de un código híbrido existente, llamado HPHall-2, el objetivo de la Tesis doctoral ha sido el desarrollo de un código híbrido avanzado que mejorara la simulación de la descarga de plasma en un motor de efecto Hall. Las actualizaciones y mejoras realizadas en las diferentes partes que componen el código comprenden tanto aspectos teóricos como numéricos. Fruto de la extensa revisión de la algoritmia del código HPHall-2 se han conseguido reducir los errores de precisión un orden de magnitud, y se ha incrementado notablemente su consistencia y robustez, permitiendo la simulación del motor en un amplio rango de condiciones. Algunos aspectos relevantes a destacar en el subcódigo de partículas son: la implementación de un nuevo algoritmo de pesado que permite determinar de forma más precisa el flujo de las magnitudes del plasma; la implementación de un nuevo algoritmo de control de población, que permite tener suficiente número de partículas cerca de las paredes de la cámara, donde los gradientes son mayores y las condiciones de cálculo son más críticas; las mejoras en los balances de masa y energía; y un mejor cálculo del campo eléctrico en una malla no uniforme. Merece especial atención el cumplimiento de la condición de Bohm en el borde de vaina, que en los códigos híbridos representa una condición de contorno necesaria para obtener una solución consistente con el modelo de interacción plasma-pared, y que en HPHall-2 aún no se había resuelto satisfactoriamente. En esta Tesis se ha implementado el criterio cinético de Bohm para una población de iones con diferentes cargas eléctricas y una gran dispersión de velocidades. En el código, el cumplimiento de la condición cinética de Bohm se consigue por medio de un algoritmo que introduce una fina capa de aceleración nocolisional adyacente a la vaina y mide adecuadamente el flujo de partículas en el espacio y en el tiempo. Las mejoras realizadas en el subcódigo de electrones incrementan la capacidad de simulación del código, especialmente en la región aguas abajo del motor, donde se simula la neutralización del chorro del plasma por medio de un modelo de cátodo volumétrico. Sin abordar el estudio detallado de la turbulencia del plasma, se implementan modelos sencillos de ajuste de la difusión anómala de Bohm, que permiten reproducir los valores experimentales del potencial y la temperatura del plasma, así como la corriente de descarga del motor. En cuanto a los aspectos teóricos, se hace especial énfasis en la interacción plasma-pared y en la dinámica de los electrones secundarios libres en el interior del plasma, cuestiones que representan hoy en día problemas abiertos en la simulación de los motores Hall. Los nuevos modelos desarrollados buscan una imagen más fiel a la realidad. Así, se implementa el modelo de vaina de termalización parcial, que considera una función de distribución no-Maxwelliana para los electrones primarios y contabiliza unas pérdidas energéticas más cercanas a la realidad. Respecto a los electrones secundarios, se realiza un estudio cinético simplificado para evaluar su grado de confinamiento en el plasma, y mediante un modelo fluido en el límite no-colisional, se determinan las densidades y energías de los electrones secundarios libres, así como su posible efecto en la ionización. El resultado obtenido muestra que los electrones secundarios se pierden en las paredes rápidamente, por lo que su efecto en el plasma es despreciable, no así en las vainas, donde determinan el salto de potencial. Por último, el trabajo teórico y de simulación numérica se complementa con el trabajo experimental realizado en el Pnnceton Plasma Physics Laboratory, en el que se analiza el interesante transitorio inicial que experimenta el motor en el proceso de arranque. Del estudio se extrae que la presencia de gases residuales adheridos a las paredes juegan un papel relevante, y se recomienda, en general, la purga completa del motor antes del modo normal de operación. El resultado final de la investigación muestra que el código híbrido desarrollado representa una buena herramienta de simulación de un motor Hall. Reproduce adecuadamente la física del motor, proporcionando resultados similares a los experimentales, y demuestra ser un buen laboratorio numérico para estudiar el plasma en el interior del motor. Abstract Electric propulsion is today a very competitive technology and has a great projection into the future. Among the various existing plasma thrusters, the Hall effect thruster has acquired a considerable maturity and constitutes an ideal means of propulsion for a wide range of missions. In the present Thesis only Hall thrusters with conventional geometry and dielectric walls are studied. The complex interaction between multiple physical phenomena makes difficult the plasma simulation in these engines. Hybrid models are those representing a better compromise between precision and computational cost. They use a fluid model for electrons and Particle-In-Cell (PIC) algorithms for ions and neutrals. The hypothesis of plasma quasineutrality is invoked, which requires to solve separately the sheaths formed around the chamber walls. On the basis of an existing hybrid code, called HPHall-2, the aim of this doctoral Thesis is to develop an advanced hybrid code that better simulates the plasma discharge in a Hall effect thruster. Updates and improvements of the code include both theoretical and numerical issues. The extensive revision of the algorithms has succeeded in reducing the accuracy errors in one order of magnitude, and the consistency and robustness of the code have been notably increased, allowing the simulation of the thruster in a wide range of conditions. The most relevant achievements related to the particle subcode are: the implementation of a new weighing algorithm that determines more accurately the plasma flux magnitudes; the implementation of a new algorithm to control the particle population, assuring enough number of particles near the chamber walls, where there are strong gradients and the conditions to perform good computations are more critical; improvements in the mass and energy balances; and a new algorithm to compute the electric field in a non-uniform mesh. It deserves special attention the fulfilment of the Bohm condition at the edge of the sheath, which represents a boundary condition necessary to match consistently the hybrid code solution with the plasma-wall interaction, and remained as a question unsatisfactory solved in the HPHall-2 code. In this Thesis, the kinetic Bohm criterion has been implemented for an ion particle population with different electric charges and a large dispersion in their velocities. In the code, the fulfilment of the kinetic Bohm condition is accomplished by an algorithm that introduces a thin non-collisional layer next to the sheaths, producing the ion acceleration, and measures properly the flux of particles in time and space. The improvements made in the electron subcode increase the code simulation capabilities, specially in the region downstream of the thruster, where the neutralization of the plasma jet is simulated using a volumetric cathode model. Without addressing the detailed study of the plasma turbulence, simple models for a parametric adjustment of the anomalous Bohm difussion are implemented in the code. They allow to reproduce the experimental values of the plasma potential and the electron temperature, as well as the discharge current of the thruster. Regarding the theoretical issues, special emphasis has been made in the plasma-wall interaction of the thruster and in the dynamics of free secondary electrons within the plasma, questions that still remain unsolved in the simulation of Hall thrusters. The new developed models look for results closer to reality, such as the partial thermalization sheath model, that assumes a non-Maxwellian distribution functions for primary electrons, and better computes the energy losses at the walls. The evaluation of secondary electrons confinement within the chamber is addressed by a simplified kinetic study; and using a collisionless fluid model, the densities and energies of free secondary electrons are computed, as well as their effect on the plasma ionization. Simulations show that secondary electrons are quickly lost at walls, with a negligible effect in the bulk of the plasma, but they determine the potential fall at sheaths. Finally, numerical simulation and theoretical work is complemented by the experimental work carried out at the Princeton Plasma Physics Laboratory, devoted to analyze the interesting transitional regime experienced by the thruster in the startup process. It is concluded that the gas impurities adhered to the thruster walls play a relevant role in the transitional regime and, as a general recomendation, a complete purge of the thruster before starting its normal mode of operation it is suggested. The final result of the research conducted in this Thesis shows that the developed code represents a good tool for the simulation of Hall thrusters. The code reproduces properly the physics of the thruster, with results similar to the experimental ones, and represents a good numerical laboratory to study the plasma inside the thruster.

Electron transport and azimuthal oscillations in hall thrusters

The Hall Effect Thruster (HET) is a type of satellite electric propulsion device initially developed in the 1960’s independently by USA and the former USSR. The development continued in the shadow during the 1970’s in the Soviet Union to reach a mature status from the technological point of view in the 1980’s. In the 1990’s the advanced state of this Russian technology became known in western countries, which rapidly restarted the analysis and development of modern Hall thrusters. Currently, there are several companies in USA, Russia and Europe manufacturing Hall thrusters for operational use. The main applications of these thrusters are low-thrust propulsion of interplanetary probes, orbital raising of satellites and stationkeeping of geostationary satellites. However, despite the well proven in-flight experience, the physics of the Hall Thruster are not completely understood yet. Over the last two decades large efforts have been dedicated to the understanding of the physics of Hall Effect thrusters. However, the so-called anomalous diffusion, short name for an excessive electron conductivity along the thruster, is not yet fully understood as it cannot be explained with classical collisional theories. One commonly accepted explanation is the existence of azimuthal oscillations with correlated plasma density and electric field fluctuations. In fact, there is experimental evidence of the presence of an azimuthal oscillation in the low frequency range (a few kHz). This oscillation, usually called spoke, was first detected empirically by Janes and Lowder in the 1960s. More recently several experiments have shown the existence of this type of oscillation in various modern Hall thrusters. Given the frequency range, it is likely that the ionization is the cause of the spoke oscillation, like for the breathing mode oscillation. In the high frequency range (a few MHz), electron-drift azimuthal oscillations have been detected in recent experiments, in line with the oscillations measured by Esipchuk and Tilinin in the 1970’s. Even though these low and high frequency azimuthal oscillations have been known for quite some time already, the physics behind them are not yet clear and their possible relation with the anomalous diffusion process remains an unknown. This work aims at analysing from a theoretical point of view and via computer simulations the possible relation between the azimuthal oscillations and the anomalous electron transport in HET. In order to achieve this main objective, two approaches are considered: local linear stability analyses and global linear stability analyses. The use of local linear stability analyses shall allow identifying the dominant terms in the promotion of the oscillations. However, these analyses do not take into account properly the axial variation of the plasma properties along the thruster. On the other hand, global linear stability analyses do account for these axial variations and shall allow determining how the azimuthal oscillations are promoted and their possible relation with the electron transport.

Current Mode with RMS Voltage and Offset Control Loops for a Single-Phase Aircraft Inverter Suitable for Parallel and 3-Phase Operation Modes

Rms voltage regulation may be an attractive possibility for controlling power inverters. Combined with a Hall Effect sensor for current control, it keeps its parallel operation capability while increasing its noise immunity, which may lead to a reduction of the Total Harmonic Distortion (THD). Besides, as voltage regulation is designed in DC, a simple PI regulator can provide accurate voltage tracking. Nevertheless, this approach does not lack drawbacks. Its narrow voltage bandwidth makes transients last longer and it increases the voltage THD when feeding non-linear loads, such as rectifying stages. On the other hand, the implementation can fall into offset voltage error. Furthermore, the information of the output voltage phase is hidden for the control as well, making the synchronization of a 3-phase setup not trivial. This paper explains the concept, design and implementation of the whole control scheme, in an on board inverter able to run in parallel and within a 3-phase setup. Special attention is paid to solve the problems foreseen at implementation level: a third analog loop accounts for the offset level is added and a digital algorithm guarantees 3-phase voltage synchronization.

Movimiento de paredes de dominio magnético en nanohilos con defectos controlados

La investigación realizada en este trabajo de tesis se ha centrado en el estudio de la generación, anclaje y desenganche de paredes de dominio magnético en nanohilos de permalloy con defectos controlados. Las últimas tecnologías de nanofabricación han abierto importantes líneas de investigación centradas en el estudio del movimiento de paredes de dominio magnético, gracias a su potencial aplicación en memorias magnéticas del futuro. En el 2004, Stuart Parkin de IBM introdujo un concepto innovador, el dispositivo “Racetrack”, basado en un nanohilo ferromagnético donde los dominios de imanación representan los "bits" de información. La frontera entre dominios, ie pared magnética, se moverían en una situación ideal por medio de transferencia de espín de una corriente polarizada. Se anclan en determinadas posiciones gracias a pequeños defectos o constricciones de tamaño nanométrico fabricados por litografía electrónica. El éxito de esta idea se basa en la generación, anclaje y desenganche de las paredes de dominio de forma controlada y repetitiva, tanto para la lectura como para la escritura de los bits de información. Slonczewski en 1994 muestra que la corriente polarizada de espín puede transferir momento magnético a la imanación local y así mover paredes por transferencia de espín y no por el campo creado por la corriente. Desde entonces muchos grupos de investigación de todo el mundo trabajan en optimizar las condiciones de transferencia de espín para mover paredes de dominio. La fracción de electrones polarizados que viaja en un hilo ferromagnético es considerablemente pequeña, así hoy por hoy la corriente necesaria para mover una pared magnética por transferencia de espín es superior a 1 107 A/cm2. Una densidad de corriente tan elevada no sólo tiene como consecuencia una importante degradación del dispositivo sino también se observan importantes efectos relacionados con el calentamiento por efecto Joule inducido por la corriente. Otro de los problemas científico - tecnológicos a resolver es la diversidad de paredes de dominio magnético ancladas en el defecto. Los diferentes tipos de pared anclados en el defecto, su quiralidad o el campo o corriente necesarios para desenganchar la pared pueden variar dependiendo si el defecto posee dimensiones ligeramente diferentes o si la pared se ancla con un método distinto. Además, existe una componente estocástica presente tanto en la nucleación como en el proceso de anclaje y desenganche que por un lado puede ser debido a la naturaleza de la pared que viaja por el hilo a una determinada temperatura distinta de cero, así como a defectos inevitables en el proceso de fabricación. Esto constituye un gran inconveniente dado que según el tipo de pared es necesario aplicar distintos valores de corriente y/o campo para desenganchar la pared del defecto. Como se menciona anteriormente, para realizar de forma eficaz la lectura y escritura de los bits de información, es necesaria la inyección, anclaje y desenganche forma controlada y repetitiva. Esto implica generar, anclar y desenganchar las paredes de dominio siempre en las mismas condiciones, ie siempre a la misma corriente o campo aplicado. Por ello, en el primer capítulo de resultados de esta tesis estudiamos el anclaje y desenganche de paredes de dominio en defectos de seis formas distintas, cada uno, de dos profundidades diferentes. Hemos realizado un análisis estadístico en diferentes hilos, donde hemos estudiado la probabilidad de anclaje cada tipo de defecto y la dispersión en el valor de campo magnético aplicado necesario para desenganchar la pared. Luego, continuamos con el estudio de la nucleación de las paredes de dominio magnético con pulsos de corriente a través una linea adyacente al nanohilo. Estudiamos defectos de tres formas distintas e identificamos, en función del valor de campo magnético aplicado, los distintos tipos de paredes de dominio anclados en cada uno de ellos. Además, con la ayuda de este método de inyección que es rápido y eficaz, hemos sido capaces de generar y anclar un único tipo de pared minimizando el comportamiento estocástico de la pared mencionado anteriormente. En estas condiciones óptimas, hemos estudiado el desenganche de las paredes de dominio por medio de corriente polarizada en espín, donde hemos conseguido desenganchar la pared de forma controlada y repetitiva siempre para los mismos valores de corriente y campo magnético aplicados. Además, aplicando pulsos de corriente en distintas direcciones, estudiamos en base a su diferencia, la contribución térmica debido al efecto Joule. Los resultados obtenidos representan un importante avance hacia la explotación práctica de este tipo de dispositivos. ABSTRACT The research activity of this thesis was focused on the nucleation, pinning and depinning of magnetic domain walls (DWs) in notched permalloy nanowires. The access to nanofabrication techniques has boosted the number of applications based on magnetic domain walls (DWs) like memory devices. In 2004, Stuart Parkin at IBM, conceived an innovative concept, the “racetrack memory” based on a ferromagnetic nanowire were the magnetic domains constitute the “bits” of information. The frontier between those magnetic domains, ie magnetic domain wall, will move ideally assisted by a spin polarized current. DWs will pin at certain positions due to artificially created pinning sites or “notches” fabricated with ebeam lithography. The success of this idea relies on the careful and predictable control on DW nucleation and a defined pinning-depinning process in order to read and write the bits of information. Sloncsewski in 1994 shows that a spin polarized current can transfer magnetic moment to the local magnetization to move the DWs instead of the magnetic field created by the current. Since then many research groups worldwide have been working on optimizing the conditions for the current induced DW motion due to the spin transfer effect. The fraction of spin polarized electrons traveling through a ferromagnetic nanowire is considerably small, so nowadays the current density required to move a DW by STT exceeds 1 107 A/cm2. A high current density not only can produce a significant degradation of the device but also important effects related to Joule heating were also observed . There are other scientific and technological issues to solve regarding the diversity of DWs states pinned at the notch. The types of DWs pinned, their chirality or their characteristic depinning current or field, may change if the notch has slightly different dimensions, the stripe has different thickness or even if the DW is pinned by a different procedure. Additionally, there is a stochastic component in both the injection of the DW and in its pinning-depinning process, which may be partly intrinsic to the nature of the travelling DW at a non-zero temperature and partly due to the unavoidable defects introduced during the nano-fabrication process. This constitutes an important inconvenient because depending on the DW type different values of current of magnetic field need to be applied in order to depin a DW from the notch. As mentioned earlier, in order to write and read the bits of information accurately, a controlled reproducible and predictable pinning- depinning process is required. This implies to nucleate, pin and depin always at the same applied magnetic field or current. Therefore, in the first chapter of this thesis we studied the pinning and depinning of DW in six different notch shapes and two depths. An statistical analysis was conducted in order to determine which notch type performed best in terms of pinning probability and the dispersion measured in the magnetic field necessary to depin the magnetic DWs. Then, we continued studying the nucleation of DWs with nanosecond current pulses by an adjacent conductive stripe. We studied the conditions for DW injection that allow a selective pinning of the different types of DWs in Permalloy nanostripes with 3 different notch shapes. Furthermore, with this injection method, which has proven to be fast and reliable, we manage to nucleate only one type of DW avoiding its stochastic behavior mentioned earlier. Having achieved this optimized conditions we studied current induced depinning where we also achieved a controlled and reproducible depinning process at always the same applied current and magnetic field. Additionally, changing the pulse polarity we studied the joule heating contribution in a current induced depinning process. The results obtained represent an important step towards the practical exploitation of these devices.

Measurement of the intrinsic damping constant in individual nanodisks of Y3Fe5O12 and Y3Fe5O12|Pt

We report on an experimental study on the spin-waves relaxation rate in two series of nanodisks of diameter ϕ=300 , 500, and 700 nm, patterned out of two systems: a 20 nm thick yttrium iron garnet (YIG) film grown by pulsed laser deposition either bare or covered by 13 nm of Pt. Using a magnetic resonance force microscope, we measure precisely the ferromagnetic resonance linewidth of each individual YIG and YIG|Pt nanodisks. We find that the linewidth in the nanostructure is sensibly smaller than the one measured in the extended film. Analysis of the frequency dependence of the spectral linewidth indicates that the improvement is principally due to the suppression of the inhomogeneous part of the broadening due to geometrical confinement, suggesting that only the homogeneous broadening contributes to the linewidth of the nanostructure. For the bare YIG nano-disks, the broadening is associated to a damping constant α=4 × 10−4 . A threefold increase of the linewidth is observed for the series with Pt cap layer, attributed to the spin pumping effect. The measured enhancement allows to extract the spin mixing conductance found to be G↑↓=1.55 × 1014 Ω−1 m−2 for our YIG(20nm)|Pt interface, thus opening large opportunities for the design of YIG based nanostructures with optimized magnetic losses.

A new approach on the long term dynamics of neo's under Yarkorsky effect

To calculate the force associated with the Yarkovsky effect the temperature distribution on the surface of the asteroid should be determined; it depends on the asteroid orbit, size and shape, spin axis orientation and period, mass, density of surface layers, albedo, thermal conductivity, capacity and IR emissivity of the material. The uncertainty of many of these parameters invites to develop simplified methods to calculate the influence of the Yarkovsky effect on long term dynamics of asteroids. In this paper we present one of this method based in a special perturbation procedure developed in our group.

Electrical decoupling effect on intermediate band Ti-implanted silicon layers

We investigated the electrical transport properties of ultraheavily Ti-implanted silicon layers subsequently pulsed laser melted (PLM). After PLM, the samples exhibit anomalous electrical behaviour in sheet resistance and Hall mobility measurements, which is associated with the formation of an intermediate band (IB) in the implanted layer. An analytical model that assumes IB formation and a current limitation effect between the implanted layer and the substrate was developed to analyse this anomalous behaviour. This model also describes the behaviour of the function V/Delta V and the electrical function F that can be extracted from the electrical measurements in the bilayer. After chemical etching of the implanted layer, the anomalous electrical behaviour observed in sheet resistance and Hall mobility measurements vanishes, recovering the unimplanted Si behaviour, in agreement with the analytical model. The behaviour of V/Delta V and the electrical function F can also be successfully described in terms of the analytical model in the bilayer structure with the implanted layer entirely stripped.

Induced radioisotopes in a linac treatment hall

When linacs operate above 8MV an undesirable neutron field is produced whose spectrum has three main components: the direct spectrum due to those neutrons leaking out from the linac head, the scattered spectrum due to neutrons produced in the head that collides with the nuclei in the head losing energy and the third spectrum due to room-return effect. The third category of spectrum has mainly epithermal and thermal neutrons being constant at any location in the treatment hall. These neutrons induce activation in the linac components, the concrete walls and in the patient body. Here the induced radioisotopes have been identified in concrete samples located in the hall and in one of the wedges. The identification has been carried out using a gamma-ray spectrometer.