Krapp's Last Tape, un recorrido por las metáforas de la memoria

A partir de la obra de Samuel Beckett Krapp's Last Tape, el presente artículo se propone presentar y revisar críticamente las metáforas de la memoria. A lo largo de la historia, los diferentes pensadores que se refirieron a la memoria hicieron uso de esta figura retórica para explicar su funcionamiento. En la crítica se verá que las metáforas poseen sus limitaciones, si bien pueden sugerir cómo se dan los procesos de almacenamiento y sus funciones, resultan insuficientes ante la cuestión del sentido que brinda la memoria. Así, y a partir de esas críticas, quedará abierto el lugar de la imaginación en nuestra relación con el pasado

Krapp's Last Tape, un recorrido por las metáforas de la memoria

A partir de la obra de Samuel Beckett Krapp's Last Tape, el presente artículo se propone presentar y revisar críticamente las metáforas de la memoria. A lo largo de la historia, los diferentes pensadores que se refirieron a la memoria hicieron uso de esta figura retórica para explicar su funcionamiento. En la crítica se verá que las metáforas poseen sus limitaciones, si bien pueden sugerir cómo se dan los procesos de almacenamiento y sus funciones, resultan insuficientes ante la cuestión del sentido que brinda la memoria. Así, y a partir de esas críticas, quedará abierto el lugar de la imaginación en nuestra relación con el pasado

Krapp's Last Tape, un recorrido por las metáforas de la memoria

A partir de la obra de Samuel Beckett Krapp's Last Tape, el presente artículo se propone presentar y revisar críticamente las metáforas de la memoria. A lo largo de la historia, los diferentes pensadores que se refirieron a la memoria hicieron uso de esta figura retórica para explicar su funcionamiento. En la crítica se verá que las metáforas poseen sus limitaciones, si bien pueden sugerir cómo se dan los procesos de almacenamiento y sus funciones, resultan insuficientes ante la cuestión del sentido que brinda la memoria. Así, y a partir de esas críticas, quedará abierto el lugar de la imaginación en nuestra relación con el pasado

Casting a voice for rural struggles during apartheid : the case of AFRA

This paper explores the attempts to co-ordinate rural resistance and struggles in South Africa during apartheid through a case study of the Association for Rural Advancement (AFRA), a land NGO established in Natal in 1979. It was a small group but had a significant local and national impact. The paper addresses three key questions concerning the character and works of AFRA: (1) What was the character and strategy of AFRA in the politicised context of the late 1970s and 1980s? (2) Was there any historical continuity and discontinuity with early attempts by Natal liberals and African landowners to organise anti-removal campaigns in the 1950s? (3) How and to what extent could AFRA negotiate the increasing influence of the Inkatha and KwaZulu government over Natal rural communities? The paper aims to serve as a critical evaluation of AFRA's strategies and activities, and its relationship with rural communities up to 1990 when land movements became nationwide.

Mono-crystalline silicon wafers manufactured by casting methods: Optoelectronic, structural and solar cell study

1) Introduction 2) The Quasi-mono, pseudo-mono, mono-like ERA. 3) Manufacturing mono-cast ingots: COST (seed recycling) 4) Summary and findings 5) Current status at DCWafers

Analysis of the Mechanical Properties of Multicrystalline and Monocrystalline Silicon Wafers Manufactured by Casting Methods

Quasi-monocrystalline silicon wafers have appeared as a critical innovation in the PV industry, joining the most favourable characteristics of the conventional substrates: the higher solar cell efficiencies of monocrystalline Czochralski-Si (Cz-Si) wafers and the lower cost and the full square-shape of the multicrystalline ones. However, the quasi-mono ingot growth can lead to a different defect structure than the typical Cz-Si process. Thus, the properties of the brand-new quasi-mono wafers, from a mechanical point of view, have been for the first time studied, comparing their strength with that of both Cz-Si mono and typical multicrystalline materials. The study has been carried out employing the four line bending test and simulating them by means of FE models. For the analysis, failure stresses were fitted to a three-parameter Weibull distribution. High mechanical strength was found in all the cases. The low quality quasi-mono wafers, interestingly, did not exhibit critical strength values for the PV industry, despite their noticeable density of extended defects.

Buque LNG con tanques tipo membrana

TIPO DE BUQUE: LNG con tanques tipo membrana. TRIPULACIÓN: 30 personas PESO MUERTO: 32000 Toneladas VELOCIDAD EN PRUEBAS: 17,5 nudos al 90% de la M.C.R, 21 % de margen de mar. PROPULSIÓN: Turbina marina a vapor. Hélice de palas fijas CAPACIDAD DE ALMACENAMIENTO: 4 bodegas con tanques de tipo membrana de capacidad total de 51000 m3 (100 % y –163ºC). Combustible 3000 m3. D.O 250 m3. Agua dulce 200 m3. Agua destilada 200 m3. Aceite 200 m3. EQUIPO DE MANIPULACIÓN DE CARGA: 8 bombas de descarga de 700 m3/h a 150 mcl, 4 bombas de achique de 25 m3/h a 150 mcl CLASIFICACIÓN Y COTA: Bureau Veritas.+I3/3, Liquified Gas Carrier, deep sea, AUT, AUTPORT. REGLAMENTOS Y LIMITACIONES: B.V, SOLAS código gas. OTROS REQUERIMIENTOS: Gas inerte. Generador de nitrógeno. Detección de gases en espacios vacíos y lastres.

Análisis del acoplamiento vibro-acústico en resonadores de membrana

El presente Trabajo Fin de Máster pretende llevar a cabo el análisis del comportamiento vibratorio de resonadores de membrana, consistentes en un panel delgado y ligero montado a cierta distancia de un elemento constructivo rígido y pesado. Este tipo de sistemas resonantes son empleados habitualmente como absorbentes de media-baja frecuencia en aplicaciones de acondicionamiento acústico de salas. El análisis hará especial hincapié en la influencia del acoplamiento mecánico-acústico entre la placa vibrante (estructura) y el colchón de aire (fluido) encerrado entre la misma y la pared rígida. En primer lugar, realizaremos el análisis modal experimental del resonador objeto de ensayo a partir de las mediciones de su respuesta vibratoria, con el fin de caracterizar su comportamiento en base a sus primeros modos propios acoplados de flexión. El análisis de las señales vibratorias en el dominio de la frecuencia para la identificación de dicho modos se realizará en el entorno de programación MATLAB, haciendo uso de una herramienta propia que implementa los métodos de cálculo y los algoritmos necesarios para tal fin. Asimismo, simularemos el comportamiento del resonador mediante el método de elementos finitos (FEM), utilizando las aplicaciones ANSYS y SYSNOISE, considerando diferentes condiciones frontera en el modelo generado. Los resultados aquí obtenidos serán de utilidad para complementar aquellos obtenidos de forma experimental a la hora de extraer conclusiones prácticas del análisis realizado. SUMMARY. This Master's Thesis intends to carry out the analysis of the vibratory behaviour of resonance absorbers, consisting of a thin and lightweight panel mounted at a distance from a rigid wall. Such systems are commonly used as sound absorption systems for mid-low frequency in room acoustics applications. The analysis will emphasize the influence of mechanical-acoustic coupling between the vibrating plate (structure) and the air cushion (acoustic element) enclosed behind it. First of all, we are performing the experimental modal analysis of the resonance absorber under test from the vibrational response measurements, in order to characterize its behaviour based on its first bending coupled-modes. The analysis of vibration signals in the frequency domain for the identification of such modes will be made in MATLAB programming environment, using a proprietary tool that implements the calculation methods and algorithms needed for this purpose. Furthermore, we are simulating the behaviour of the resonance absorber applying the Finite Element Method (FEM) – using ANSYS and SYSNOISE applications - considering different boundary conditions in the model created. The results from the simulation will be useful to complement those obtained experimentally when drawing practical conclusions from this analysis.

T-REX: Bare electro-dynamic tape-tether technology experimetn on sounding rocket S520

The project to verify the performance of space tether technology was successfully demonstrated by the launch of the sounding rocket S520 the 25tu. The project is the space demonstration of science and engineering technologies of a bare tape electrodynamic tether (EDT) in the international campaign between Japan, USA, Europe and Australia. Method of "Inverse ORIGAMI (Tape tether folding)" was employed in order to deploy the bare tape EDT in a short period time of the suborbital flight. The deployment of tape tether was tested in a various experimental schemes on ground to show high reliability of tape tether deployment. The rocket was launched on the summer of 2010 and deployed a bare electro-dynamic tape tether with length 132.6 m, which is the world record of the length deployment of tape tether. The verification of tether technology has found a variety kind of science and technology results as the first in the humankind and will lead a large number of applications of space tether technologies

Tape-tether design for de-orbiting from given altitude and inclination

The product of the tether-to-satellite mass ratio and the probability of tether cuts by small debris must be small to make electrodynamic bare tethers a competitive and useful de-orbiting technology. In the case of a circular orbit and assuming a model for the debris population, the product can be written as a function that just depends on the initial orbit parameters (altitude and inclination) and the tether geometry. This formula, which does not contain the time explicitly and ignores the details of the tether dynamics during the de-orbiting, is used to find design rules for the tape dimensions and the orbit parameter ranges where tethers dominate other de-orbiting technologies like rockets, electrical propulsion, and sails.

Survival probability of round and tape tethers against debris impact

The current space environment, consisting of manmade debris and micrometeoroids, poses a risk to safe operations in space, and the situation is continuously deteriorating due to in-orbit debris collisions and to new satellite launches. Bare electrodynamic tethers can provide an efficient mechanism for rapid deorbiting of satellites from low Earth orbit at end of life. Because of its particular geometry (length very much larger than cross-sectional dimensions), a tether may have a relatively high risk of being severed by the single impact of small debris. The rates of fatal impact of orbital debris on round and tape tethers of equal length and mass, evaluated with an analytical approximation to debris flux modeled by NASA’s ORDEM2000, shows much higher survival probability for tapes. A comparative numerical analysis using debris flux model ORDEM2000 and ESA’s MASTER2005 validates the analytical result and shows that, for a given time in orbit, a tape has a probability of survival of about one and a half orders of magnitude higher than a round tether of equal mass and length. Because deorbiting from a given altitude is much faster for the tape due to its larger perimeter, its probability of survival in a practical sense is quite high.

Analysis of tape tether survival in LEO against orbital debris

The low earth orbit (LEO) environment contains a large number of artificial debris, of which a significant portion is due to dead satellites and fragments of satellites resulted from explosions and in-orbit collisions. Deorbiting defunct satellites at the end of their life can be achieved by a successful operation of an Electrodynamic Tether (EDT) system. The effectiveness of an EDT greatly depends on the survivability of the tether, which can become debris itself if cut by debris particles; a tether can be completely cut by debris having some minimal diameter. The objective of this paper is to develop an accurate model using power laws for debris-size ranges, in both ORDEM2000 and MASTER2009 debris flux models, to calculate tape tether survivability. The analytical model, which depends on tape dimensions (width, thickness) and orbital parameters (inclinations, altitudes) is then verified with fully numerical results to compare for different orbit inclinations, altitudes and tape width for both ORDEM2000 and MASTER2009 flux data.

Survivability analysis of tape-tether against multiple impact with tiny debris

We show that for a tether at 800 km altitude, which is 5 km long, 2 cm wide and 0.05 mm thick, the risk of substantial damage during a 3 month period due to multiple impacts with debris or micrometeoroids is low, of about 1.4%. By substantial damage we mean that if the tape is divided in 2 cm2 cm squares, then in some square the damaged area by bombardment with debris or micrometeoroids exceeds 11% of the area of the square. Furthermore, we show that the danger posed by the micrometeoroids is negligible compared to the risk posed by the debris.

Space demostration of bare electrodynamic tape-tether technology on the sounding rocket S520-25

A spaceflight validation of bare electro dynamic tape tether technology was conducted. A S520-25 sounding rocket was launched successfully at 05:00am on 31 August 2010 and successfully deployed 132.6m of tape tether over 120 seconds in a ballistic flight. The electrodynamic performance of the bare tape tether employed as an atmospheric probe was measured. Flight results are introduced through the present progressive report of the demonstration and the results of flight experiment are examined as the premier report of the international cooperation between Japan, Europe, USA and Australia. Future plans for maturing space tether technology, which will play an important role for future space activities, are also discussed.

Tanque aéreo de almacenamiento de gas natural licuado de tipo membrana y 200.000 m3 de volumen

El presente proyecto consiste en el diseño básico de ingeniería de un tanque aéreo de almacenamiento de gas natural licuado (GNL) de integridad total con tecnología de membrana y con una capacidad neta de almacenamiento de 200 000 m3 a una temperatura de -162ºC y una presión máxima de 15 kPa. El proyecto desarrolla los siguientes puntos: el diseño del tanque interno con tecnología de membrana, dimensionamiento del aislante, diseño del techo suspendido, tanque externo, cúpula de hormigón, cimentación, dimensionamiento de los equipos, Ensayos, puesta en frío, puesta en servicio, planificación de la ejecución del proyecto, recursos empleados, control de la presión, prevención del rollover, coste del tanque y análisis económico del proyecto