Heat losses in a CVD reactor for polysilicon: comprehensive model and experimental validation

This work addresses heat losses in a CVD reactor for polysilicon production. Contributions to the energy consumption of the so-called Siemens process are evaluated, and a comprehensive model for heat loss is presented. A previously-developed model for radiative heat loss is combined with conductive heat loss theory and a new model for convective heat loss. Theoretical calculations are developed and theoretical energy consumption of the polysilicon deposition process is obtained. The model is validated by comparison with experimental results obtained using a laboratory-scale CVD reactor. Finally, the model is used to calculate heat consumption in a 36-rod industrial reactor; the energy consumption due to convective heat loss per kilogram of polysilicon produced is calculated to be 22-30 kWh/kg along a deposition process.

Drifting plasma collection by a positive biased tether wire in LEO-like plasma conditions: current measurement and plasma diagnostic

BETs is a three-year project financed by the Space Program of the European Commission, aimed at developing an efficient deorbit system that could be carried on board any future satellite launched into Low Earth Orbit (LEO). The operational system involves a conductive tape-tether left bare to establish anodic contact with the ambient plasma as a giant Langmuir probe. As a part of this project, we are carrying out both numerical and experimental approaches to estimate the collected current by the positive part of the tether. This paper deals with experimental measurements performed in the IONospheric Atmosphere Simulator (JONAS) plasma chamber of the Onera-Space Environment Department. The JONAS facility is a 9- m3 vacuum chamber equipped with a plasma source providing drifting plasma simulating LEO conditions in terms of density and temperature. A thin metallic cylinder, simulating the tether, is set inside the chamber and polarized up to 1000 V. The Earth's magnetic field is neutralized inside the chamber. In a first time, tether collected current versus tether polarization is measured for different plasma source energies and densities. In complement, several types of Langmuir probes are used at the same location to allow the extraction of both ion densities and electron parameters by computer modeling (classical Langmuir probe characteristics are not accurate enough in the present situation). These two measurements permit estimation of the discrepancies between the theoretical collection laws, orbital motion limited law in particular, and the experimental data in LEO-like conditions without magnetic fields. In a second time, the spatial variations and the time evolutions of the plasma properties around the tether are investigated. Spherical and emissive Langmuir probes are also used for a more extensive characterization of the plasma in space and time dependent analysis. Results show the ion depletion because of the wake effect and the accumulation of- ions upstream of the tether. In some regimes (at large positive potential), oscillations are observed on the tether collected current and on Langmuir probe collected current in specific sites.

An universal system to de-orbit satellites at end of life

A 3-year Project financed by the European Commission is aimed at developing a universal system to de-orbit satellites at their end of life, as a fundamental contribution to limit the increase of debris in the Space environment. The operational system involves a conductive tapetether left bare to establish anodic contact with the ambient plasma as a giant Langmuir probe. The Project will size the three disparate dimensions of a tape for a selected de-orbit mission and determine scaling laws to allow system design for a general mission. Starting at the second year, mission selection is carried out while developing numerical codes to implement control laws on tether dynamics in/off the orbital plane; performing numerical simulations and plasma chamber measurements on tether-plasma interaction; and completing design of subsystems: electronejecting plasma contactor, power module, interface elements, deployment mechanism, and tether-tape/end-mass. This will be followed by subsystems manufacturing and by currentcollection, free-fall, and hypervelocity impact tests.

A proposed bare-tether experiment on board a sounding rocket

A mission on board a sounding rocket to carry out two bare-tether experiments is proposed: a test of orbital-motion-limited (OML) collection and the proof-of-flight of a technique to determine the (neutral) density vertical profile in the critical E-layer. Since full bias from the motional field will be small (~ 20V), corresponding to a tape 1 km long and V rocket <8 km/s, a power source with a range of supply voltages of few kV would be used. First, the negative terminal of the supply would be connected to the tape, and the positive terminal to a round, conductive boom of length 10 - 20 m; electrons collected by the boom cross the supply into the tape, where they leak out at the rate of ion impact plus secondary emission. Determination of the density profile from measurements of auroral emissions observed from the rocket, as secondaries racing down the magnetic field reach an E-layer footprint, are discussed. Next the positive terminal of the voltage supply is connected to the tape, and the negative terminal to a Hollow Cathode (HC); electrons now collected by the tape cross the supply, and are ejected at the HC. The opposite connections, with current collection operated by tape and boom, and operating on electrons and ions, and through partial switching in the supply, allow testing OML collection in almost all respects it depends on.

Floating Bare Tether as Upper Atmosphere Probe

Use of a (bare) conductive tape electrically floating in LEO as an effective e-beam source that produces artificial auroras, and is free of problems that have marred standard beams, is considered. Ambient ions impacting the tape with KeV energies over most of its length liberate secondary electrons, which race down the magnetic field and excite neutrals in the E-layer, resulting in auroral emissions. The tether would operate at night-time with both a power supply and a plasma contactor off; power and contactor would be on at daytime for reboost. The optimal tape thickness yielding a minimum mass for an autonomous system is determined; the alternative use of an electric thruster for day reboost, depending on mission duration, is discussed. Measurements of emission brightness from the spacecraft could allow determination of the (neutral) density vertical profile in the critical E-layer; the flux and energy in the beam, varying along the tether, allow imaging line-of-sight integrated emissions that mix effects with altitude-dependent neutral density and lead to a brightness peak in the beam footprint at the E-layer. Difficulties in tomographic inversion, to determine the density profile, result from beam broadening, due to elastic collisions, which flattens the peak, and to the highly nonlinear functional dependency of line-of-sight brightness. Some dynamical issues are discussed.

Effect of magnetic field on current colection on bare tether in LEO

An eiectrodynamic Tether is a long thin conductive string deployed from a spacecraft. A part of the ED tether near one end, which is rendered positive by the Electromotive force (EMF)along the tether, collects electrons from the ambient plasma. In the frame of reference moving with theter, ions flow toward the tether, get deflected near the tether by its high positive potential and create a wake. Due to the asymmetry of plasma distribution and the weak but significant Geomagnetic field, the conventional probe theory becomes almost inapplicable. Computational work for the prediction of current collection is thus necessiated.. In this paper, we analyze effects of magnetic field on velocity distribution funtion at a point that is far from the tether, and discuss a new way to treat electrons at computational boundary. Three cases with different magnetic field are simulated and compiled so as to provide a part of the pre-flight prediction of the space experiment by NASA ProSEDS, which is planned September 2002.

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.

A review of electrodynamic tethers for science applications

A bare electrodynamic tether (EDT) is a conductive thin wire or tape tens of kilometres long, which is kept taut in space by gravity gradient or spinning, and is left bare of insulation to collect (and carry) current as a cylindrical Langmuir probe in an ambient magnetized plasma. An EDT is a probe in mesothermal flow at highly positive (or negative) bias, with a large or extremely large 2D sheath, which may show effects from the magnetic self-field of its current and have electrons adiabatically trapped in its ram front. Beyond technical applications ranging from propellantless propulsion to power generation in orbit, EDTs allow broad scientific uses such as generating electron beams and artificial auroras; exciting Alfven waves and whistlers; odifying the radiation belts; and exploring interplanetary space and the Jovian magnetosphere. Asymptotic analysis, numerical simulations, laboratory tests, and planned missions on EDTs are reviewed

New strategies in laser processing of TCOs for light management improvement in thin-film silicon solar cells

Light confinement strategies play a crucial role in the performance of thin-film (TF) silicon solar cells. One way to reduce the optical losses is the texturing of the transparent conductive oxide (TCO) that acts as the front contact. Other losses arise from the mismatch between the incident light spectrum and the spectral properties of the absorbent material that imply that low energy photons (below the bandgap value) are not absorbed, and therefore can not generate photocurrent. Up-conversion techniques, in which two sub-bandgap photons are combined to give one photon with a better matching with the bandgap, were proposed to overcome this problem. In particular, this work studies two strategies to improve light management in thin film silicon solar cells using laser technology. The first one addresses the problem of TCO surface texturing using fully commercial fast and ultrafast solid state laser sources. Aluminum doped Zinc Oxide (AZO) samples were laser processed and the results were optically evaluated by measuring the haze factor of the treated samples. As a second strategy, laser annealing experiments of TCOs doped with rare earth ions are presented as a potential process to produce layers with up-conversion properties, opening the possibility of its potential use in high efficiency solar cells.

Optimum sizing of bare-tape tethers for de-orbiting satellites at end of mission

De-orbiting satellites at end of mission would prevent generation of new space debris. A proposed de-orbit technology involves a bare conductive tape-tether, which uses neither propellant nor power supply while generating power for on-board use during de-orbiting. The present work shows how to select tape dimensions for a generic mission so as to satisfy requirements of very small tether-to-satellite mass ratio mt/MS and probability Nf of tether cut by small debris, while keeping de-orbit time tf short and product tf ×× tether length low to reduce maneuvers in avoiding collisions with large debris. Design is here discussed for particular missions (initial orbit of 720 km altitude and 63° and 92° inclinations, and 3 disparate MS values, 37.5, 375, and 3750 kg), proving it scalable. At mid-inclination and a mass-ratio of a few percent, de-orbit time takes about 2 weeks and Nf is a small fraction of 1%, with tape dimensions ranging from 1 to 6 cm, 10 to 54 μμm, and 2.8 to 8.6 km. Performance drop from middle to high inclination proved moderate: if allowing for twice as large mt/MS, increases are reduced to a factor of 4 in tf and a slight one in Nf, except for multi-ton satellites, somewhat more requiring because efficient orbital-motion-limited electron collection restricts tape-width values, resulting in tape length (slightly) increasing too.

Propellantless deorbiting of space debris by bare electrodynamic tethers : final report

A Space tether is a thin, multi-kilometers long conductive wire, joining a satellite and some opposite end mass, and keeping vertical in orbit by the gravity-gradient. The ambient plasma, being highly conductive, is equipotential in its own co-moving frame. In the tether frame, in relative motion however, there is in the plasma a motional electric field of order of 100 V/km, product of (near) orbital velocity and geomagnetic field. The electromotive force established over the tether length allows plasma contactor devices to collect electrons at one polarized-positive (anodic) end and eject electrons at the opposite end, setting up a current along a standard, fully insulated tether. The Lorentz force exerted on the current by the geomagnetic field itself is always drag; this relies on just thermodynamics, like air drag. The bare tether concept, introduced in 1992 at the Universidad Politécnica de Madrid (UPM), takes away the insulation and has electrons collected over the tether segment coming out polarized positive; the concept rests on 2D (Langmuir probe) current-collection in plasmas being greatly more efficient than 3D collection. A Plasma Contactor ejects electrons at the cathodic end. A bare tether with a thin-tape cross section has much greater perimeter and de-orbits much faster than a (corresponding) round bare tether of equal length and mass. Further, tethers being long and thin, they are prone to cuts by abundant small space debris, but BETs has shown that the tape has a probability of being cut per unit time smaller by more than one order of magnitude than the corresponding round tether (debris comparable to its width are much less abundant than debris comparable to the radius of the corresponding round tether). Also, the tape collects much more current, and de-orbits much faster, than a corresponding multi-line “tape” made of thin round wires cross-connected to survive debris cuts. Tethers use a dissipative mechanism quite different from air drag and can de-orbit in just a few months; also, tape tethers are much lighter than round tethers of equal length and perimeter, which can capture equal current. The 3 disparate tape dimensions allow easily scalable design. Switching the cathodic Contactor off-on allows maneuvering to avoid catastrophic collisions with big tracked debris. Lorentz braking is as reliable as air drag. Tethers are still reasonably effective at high inclinations, where the motional field is small, because the geomagnetic field is not just a dipole along the Earth polar axis. BETs is the EC FP7/Space Project 262972, financed in about 1.8 million euros, from 1 November 2010 to 31 January 2014, and carrying out RTD work on de-orbiting space debris. Coordinated by UPM, it has partners Università di Padova, ONERA-Toulouse, Colorado State University, SME Emxys, DLR–Bremen, and Fundación Tecnalia. BETs work involves 1) Designing, building, and ground-testing basic hardware subsystems Cathodic Plasma Contactor, Tether Deployment Mechanism, Power Control Module, and Tape with crosswise and lengthwise structure. 2) Testing current collection and verifying tether dynamical stability. 3) Preliminary design of tape dimensions for a generic mission, conducive to low system-to-satellite mass ratio and probability of cut by small debris, and ohmic-effects regime of tether current for fast de-orbiting. Reaching TRL 4-5, BETs appears ready for in-orbit demostration.

The peculiar electrical response of liquid crystal-carbon nanotube systems as seen by impedance spectroscopy

Conductive nanoparticles, especially elongated ones such as carbon nanotubes, dramatically modify the electrical behavior of liquid crystal cells. These nanoparticles are known to reorient with liquid crystals in electric fields, causing significant variations of conductivity at minute concentrations of tens or hundreds ppm. The above notwithstanding, impedance spectroscopy of doped cells in the frequency range customarily employed by liquid crystal devices, 100 Hz?10 kHz, shows a relatively simple resistor/capacitor response where the components of the cell can be univocally assigned to single components of the electrical equivalent circuit. However, widening the frequency range up to 1 MHz or beyond reveals a complex behavior that cannot be explained with the same simple EEC. Moreover, the system impedance varies with the application of electric fields, their effect remaining after removing the field. Carbon nanotubes are reoriented together with liquid crystal reorientation when applying voltage, but barely reoriented back upon liquid crystal relaxation once the voltage is removed. Results demonstrate a remarkable variation in the impedance of the dielectric blend formed by liquid crystal and carbon nanotubes, the irreversible orientation of the carbon nanotubes and possible permanent contacts between electrodes.