1000 resultados para Fuerza y energía


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El objetivo principal del proyecto es la construcción de un cargadero de camiones cisternas de GNL integrado en una planta de regasificación. Se realiza el diseño de la instalación para la carga diaria de aproximadamente 100 camiones cisterna. Para un funcionamiento óptimo se ha calculado el caudal y la presión de las diferentes líneas que abastecen el cargadero. Para el dimensionamiento de la instalación se ha tenido en cuenta las dimensiones de los camiones así como la facilidad de acceso y carga del gas natural licuado.

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The general purpose of this study was the determination of the safety conditions to avoid the presence of explosive atmospheres in the wastewater industry. Eight Spanish plants located in Madrid, Barcelona and Málaga were considered and several sludge samples were taken in different seasons. The base for the assessment of the spontaneous ignition behaviour of dust accumulations is the experimental determination of the self-ignition temperature under isothermal conditions. Self-ignition temperatures at four volumes were obtained for one sample of sewage sludge, allowing their extrapolation to large storage facilities. A simple test method, based also on an isothermal study of samples, is the UN classification of substances liable to spontaneous combustion. Two different samples were so tested, obtaining unlike results if transported in packages of different volumes. By means of thermogravimetric techniques it is possible to analyse the thermal susceptibility of dried sewage sludge. Apparent activation energy can be obtained from the rate of weight loss. It is also applied to the study of self-ignition susceptibility by modifying test conditions when oxygen stream is introduced. As a consequence of this oxidant contribution, sample behaviour can be very different during testing and a step drop or sudden loss of weight is observed at a characteristic temperature for every substance, associated to a rapid combustion. Plotting both the activation energy and the characteristic temperature, a map of self-ignition risk was obtained for 10 samples, showing different risk levels for samples taken in different locations and at different seasons. A prediction of the self-ignition risk level can be also determined.

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The treatment and disposal of sewage sludge is becoming an urgent need whereby different technologies were developed and integrated into the waste cycle all over the world. One of the most used technologies is the thermal drying of the sludge. Thermally dried sewage sludge has interesting properties that allow its use as an alternative fuel, but also needs some consideration from the point of view of its safe operation. The aim of this study was the research on the flammability properties of sewage sludge, including ignition sensitivity, explosion severity, thermal sensitivity and thermal stability. Furthermore relationships among those properties and composition parameters have been determined, added to the study of their variation depending on their origin or season. Finally, properties related to spontaneous combustion were determined. To study these relationships and characteristics sludge samples were selected from different locations in Spain and taken during different seasons.

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Colombia is one of the largest per capita mercury polluters in the world as a consequence of its artisanal gold mining activities. The severity of this problem in terms of potential health effects was evaluated by means of a probabilistic risk assessment carried out in the twelve departments (or provinces) in Colombia with the largest gold production. The two exposure pathways included in the risk assessment were inhalation of elemental Hg vapors and ingestion of fish contaminated with methyl mercury. Exposure parameters for the adult population (especially rates of fish consumption) were obtained from nation-wide surveys and concentrations of Hg in air and of methyl-mercury in fish were gathered from previous scientific studies. Fish consumption varied between departments and ranged from 0 to 0.3 kg d?1. Average concentrations of total mercury in fish (70 data) ranged from 0.026 to 3.3 lg g?1. A total of 550 individual measurements of Hg in workshop air (ranging from menor queDL to 1 mg m?3) and 261 measurements of Hg in outdoor air (ranging from menor queDL to 0.652 mg m?3) were used to generate the probability distributions used as concentration terms in the calculation of risk. All but two of the distributions of Hazard Quotients (HQ) associated with ingestion of Hg-contaminated fish for the twelve regions evaluated presented median values higher than the threshold value of 1 and the 95th percentiles ranged from 4 to 90. In the case of exposure to Hg vapors, minimum values of HQ for the general population exceeded 1 in all the towns included in this study, and the HQs for miner-smelters burning the amalgam is two orders of magnitude higher, reaching values of 200 for the 95th percentile. Even acknowledging the conservative assumptions included in the risk assessment and the uncertainties associated with it, its results clearly reveal the exorbitant levels of risk endured not only by miner-smelters but also by the general population of artisanal gold mining communities in Colombia.

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The study of the response of mechanical systems to external excitations, even in the simplest cases, involves solving second-order ordinary differential equations or systems thereof. Finding the natural frequencies of a system and understanding the effect of variations of the excitation frequencies on the response of the system are essential when designing mechanisms [1] and structures [2]. However, faced with the mathematical complexity of the problem, students tend to focus on the mathematical resolution rather than on the interpretation of the results. To overcome this difficulty, once the general theoretical problem and its solution through the state space [3] have been presented, Matlab®[4] and Simulink®[5] are used to simulate specific situations. Without them, the discussion of the effect of slight variations in input variables on the outcome of the model becomes burdensome due to the excessive calculation time required. Conversely, with the help of those simulation tools, students can easily reach practical conclusions and their evaluation can be based on their interpretation of results and not on their mathematical skills

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El presente proyecto muestra el estudio realizado para evaluar la capacidad de drenaje de la canalización construida en el río Forcón-Barranca, en la población de San Miguel de Reinante (Lugo), a consecuencia de las severas inundaciones acaecidas los días 9 y 10 de junio de 2010. Para evaluar y analizar la peligrosidad se ha seguido un método hidrometeorológico agregado, debido a la falta de aforos, pluviómetros y datos, y se han usado Modelos Digitales de Elevaciones como punto de partida. Todo ello ha llevado a la conclusión de la ineficacia del canal para un período de retorno de 500 años. ABSTRACT After severe flooding in San Miguel de Reinante (Lugo) the 9th and 10th June 2010, a concrete channel was built. This project assesses the drainage capacity of such channel, performing a flood hazard analysis. Because no flow measures or rain gauge data were available a lumped model was followed in order to evaluate flood hazard, using Digital Elevation Models as a starting point. This has led to the conclusion that the channel cannot effectively drain a flow after a rainfall with a return period of 500 years.

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El presente proyecto tiene como objetivo principal el análisis de la viabilidad de estacionamiento de vehículos propulsados por gas natural comprimido (GNC) desde el punto de vista de formación de atmosferas potencialmente explosivas en los garajes subterráneos. Además se ha realizado una breve introducción sobre el GNC explicando el origen, la composición y los diferentes usos que tiene. Se ha realizado la evaluación de riesgos asociados a la utilización de vehículos propulsados por gas natural y estimación de tasas de escape en el circuito de combustible de los vehículos propulsados por GNC. Para ello se ha aplicado la normativa UNE EN 60079-10 traspuesta en España mediante el Real Decreto del 681/2003 sobre la salud y la seguridad de los trabajadores y el Real Decreto 400/1996 sobre aparatos y sistemas de protección para su uso en atmósferas explosivas. Finalmente se han expuesto las medidas de prevención y protección necesarias para prevenir la generación de atmosferas potencialmente explosivas en los garajes subterráneos y se han detallado los procedimientos y las operaciones que han de realizarse. En las conclusiones se han explicado las acciones más importantes que deben emprenderse para mejorar la seguridad de personas e instalaciones en las áreas de riesgo por presencia de atmósferas potencialmente explosivas. ABSTRACT The main objective of this project is to analyze the viability of the parking of vehicles powered by compressed natural gas (CNG) in the underground garages from the point of view of generated of potentially explosive atmospheres in garages. A brief introduction about the CNG explaining the origin, composition and the different uses that it has is also included. An assessment of the risks associated with the use of vehicles powered by natural gas has been provided as well as an estimate of the exhaust rates on the gas circuit of CNG vehicles. In order to do that, the standard UNE EN 60079-10 transposed in Spain by the Royal Decree 681/2003 about the health and safety of workers and the Royal Decree 400/1996 about equipment and protection systems to be used in explosive atmospheres have been applied. Finally, the necessary preventive and protective measures to prevent the generation of potentially explosive atmospheres in underground garages have been presented and the procedures and operations to be performed have been detailed. In the conclusions, the most important actions to be taken in order to improve the safety of people and facilities in the areas at risk of having potentially explosive atmospheres have been described.

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El objetivo del presente proyecto es realizar el pre-diseño de una instalación solar mixta fotovoltaica-térmica para satisfacer la demanda eléctrica para iluminación y para parte de las necesidades de energía térmica para agua caliente de una vivienda. El proyecto define las condiciones técnicas de la instalación a partir de la radiación solar registrada en la localización elegida. Además de incluir el estudio económico y los planos correspondientes que indican la viabilidad del mismo. Como puntos a destacar en el proyecto, se puede tomar los datos obtenidos de generación eléctrica y térmica, la viabilidad técnica y económica y el análisis de la incipiente tecnología de paneles híbridos fotovoltaicos-térmicos. La incorporación de las energías renovables es ya una realidad para las viviendas de nueva construcción, en cambio son pocas las nuevas instalaciones en edificios o viviendas ya construidas. Es importante promover este tipo de tecnologías con objetivo de reducir la dependencia actual de los combustibles fósiles y evitar así sus efectos nocivos al medio ambiente. ABSTRACT The purpose of this project is to carry out the draft design of a solar mixed photovoltaic-thermal installation to satisfy the electrical and thermal demand in a building, for lighting as well as for some of the energy required for water heating. The project defines the technical conditions of the system, given the solar radiation registered in the chosen location. It also includes the economic analysis and the respective plans that indicates the viability of the project. The highlights of the project are the following: electricity and thermal energy generation data, the technical and financial viability and the analysis of the new technology of the Photovoltaic-Thermal hybrid solar collectors. The inclusion of renewable energies is already a living reality for newly constructed buildings. By contrast, they are rarely implemented in old buildings. In order to be able to reduce the fossil fuels dependency, and in doing so, avoid its damaging effects on the environment, it is very important to promote the use of these cleaner technologies.

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Este proyecto tiene por objeto desarrollar una sistemática de control metrológico para vigilar la exactitud de los medidores volumétricos de desplazamiento positivo que operan en las compañías logísticas de hidrocarburos para la transferencia de custodia que están en el cargadero y se ensayan in situ para obtener su meter factor. El punto de partida son las hojas primarias de las calibraciones generadas frente a sus patrones y el prover que nos facilitan las compañías. Dado el elevado número de ensayos y debido a que estos medidores no tienen gráficos de control estables, el enfoque del tratamiento ha sido un etiquetado para realizar un control de inestabilidad y calidad de los ensayos y así, determinar equipos anómalos. Para la búsqueda de equipos atípicos se ha desarrollado el filtro de Tukey para el estudio de la estadística descriptiva de los valores del meter factor. Entre los dos métodos se han obtenido una clasificación de equipos vigilables, recalibrables y sustituibles para facilitar a las compañías logísticas. ABSTRACT The aim of this project is to develop a systematic metrological control to monitor the accuracy of the positive displacement flow meters operating in oil logistics companies for custody transfer which are in the loading track facilities and it are tested in-situ to obtain the meter factor. Due to the high number of assays that meters don´t have stable graphics of control, the approach of data processing has been a labeled to perform an instability and quality control of assays for establish anomalous meters. To find outliers meters is developed the filter of Turkey to study the descriptive statistics of meter factor values. Between both analytical methods is obtained a classification of controllable, recalibrables and replaceable meters to provide to the logistic company.

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Following recent accounting and ethical scandals within the Telecom Industry like Gowex case, old cards are laid on the table: what kind of management and control are we doing on our businesses and what use do we give to the specific tools we have at our disposition? There are indicators, that on a very specific, concise and accurate manner, aside from brief, allow us to analyze and capture the complexity of a business and also they constitute an important support when making optimal decisions. These instruments or indicators show, a priori, all relevant data from a purely economic perspective, while there also exist, the possibility of including factors that are not of this nature strictly. For instance, there are indicators that take into account the customer?s satisfaction, the corporate reputation among others. Both kind of performance indicators form, together, an integral dashboard while the pure economic side of it could be considered as a basic dashboard. Based on DuPont?s methodology, we will be able to calculate the ROI (Return on Investment) of a company from the disaggregation of very useful and much needed indicators like the ROE (Return on Equity) or the ROA (Return on Assets); thereby, we will be able to get to know, to control and, hence, to optimize the company?s leverage level, its liquidity ratio or its solvency ratio, among others; as well as the yield we will be able to obtain if our decisions and management are optimal related to the bodies of assets. Bear in mind and make the most of the abovementioned management tools and indicators that we have at our disposition, allow us to act knowing our path and taking full responsibility, as well as, to obtain the maximum planned benefits, instead of leaving them to be casual. We will be able to avoid errors that can lead the company to an unfortunate and non-desirable situation and, of course, we will detect, way in advance, the actual needs of the business in terms of accounting and financial sanitation before irreversible situations are reached.

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Accommodation is a first need and one of the most important decisions that university students have to decide taking into account their limited budget. The satisfaction grade of these students is the relevant aspect for the administrators and managers of the university residences, because it allows assuring the viability and sustainability of this kind of accommodation. In a situation of decline in rate of retention of students into the residence, coupled with an environment of economic crisis. Hence, of disposable income reduction, it seems essential to get to know what factors affect the motivation to remain into the university residence more than others when it comes to the final choice. The offer?s increase of different kind of accommodation is another variable to be considered when taking the decision related to the management of this kind of accommodation. Thus, there is the need to know which are the key factors and to obtain information about these variables in order to go deep into the relevance grade with the aim to pursue the strategic objectives, that will allow to improve the relationship with the customer and to respond to his accommodation? needs. This article researches the motivation elements that lead the students to remain in a university residence or to abandon it in exchange or a different accommodation, as per example shared flats or individual apartments. This research work intends to be useful for the university residence?s managers in order to increase its incomes, to raise the satisfaction degree among its residents and to obtain better end results in the management of these properties. The fieldwork conducted in the Residencia Universitaria Gómez Pardo (RUGP), Universidad Politécnica de Madrid (UPM), for four semesters, which means students from 27 different grades (undergraduates) and 81 surveys finished, shows the following conclusions. Not only the relation with the residence?s personnel but also the quality and quantity of the feeding and the availability and quality of the internet service, constitute key factors when it comes to make the decision of remaining or of abandoning the residence when the semester comes to its end.

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When we look to perform a work for developing a framework to create a business and take it correctly, there are always some persons looking as a challenge those bases and finding a mistake. The way to work in these situations is not a matter of law, is a matter of devoting time to identify these situations. It is always said that the evil goes a step ahead. The business ethics have been altered for quite time by some would-be entrepreneurs. These people have learned to play with business ethics to show your business as prosperous as something that is sought to highlight and adulterate their results quickly. Once the company reaches an international dimension, many companies take on global responsibility and, in these cases where you can see if the objective has been to obtain a rapid capital increase or growth is in line with its proportions. A business ethics is based on establishing a strong base so that interest is encouraged from an early time. Good staff, organizational level should be achieved and not only at the company but, out of the company too. Thus, you can create a secure base to convince potential investors and employees about the business. There are no freeways in business ethics and all fast track can be or a genius or leads to failure. We must find where these jumps are occurring, such errors or corrections to business ethics and their rules. Thus we can differentiate a company or an entrepreneur who is working correctly from the cloaking. Starting from the basics of business ethics and studying the different levels from the personal to the prospect that the company shows in the world. Lets see where these changes are occurring and how we can fight against them and anticipate the market to possible cases of fraud or strange movements seeking to attract the unwary

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This paper shows the results of the study of physical, mechanic and chemical behaviour of some natural zeolite types sampled in different outcrops of the world, mainly from Mexico, Cuba and Spain, as well as their incidence in certain practical applications, by means of the utilization of its pozzuolanic properties. Results emphasize that every natural zeolite variety gives different answers in the assays, probably influenced by the subtle variability of their chemical composition. Key words: zeolites, pozzuolanic, density, geometric, strength

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La supervivencia de los pueblos en aislamiento (PIAs), Tagaeri? Taromenane en la Amazonia ecuatoriana, está influida por agentes externos y características culturales. El área definida como Zona Intangible para el desplazamiento de los PIAs presenta cierta debilidad geográfica, lo que alterna el funcionamiento de estas comunidades. El objetivo de este trabajo es conocer el comportamiento de las comunidades aisladas en relación con las fronteras de contactos. Se ha utilizado el software libre NetLogo versión 5.0.3, para simular la evolución durante 100 años de dos comunidades. Las poblaciones estimadas iniciales de indígenas en asilamiento fue de 100, 500, 1000 individuos por escenario. El comportamiento está condicionado por las variables: individuos Taromenane, individuos Tagaeri, tasa de nacimientos, disponibilidad de alimento en la Amazonía, crecimiento de la vegetación, valor energético de la alimentación, y energía de la vegetación. Las características guerreras por la protección de territorio propias de los PIAs, han permitido concluir que la intensificación de las presiones externas sumadas a los enfrenamientos entre grupos aislados genera su propia extinción en un espacio temporal de 100 años.

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Esta tesis se ha realizado en el contexto del proyecto UPMSat-2, que es un microsatélite diseñado, construido y operado por el Instituto Universitario de Microgravedad "Ignacio Da Riva" (IDR / UPM) de la Universidad Politécnica de Madrid. Aplicación de la metodología Ingeniería Concurrente (Concurrent Engineering: CE) en el marco de la aplicación de diseño multidisciplinar (Multidisciplinary Design Optimization: MDO) es uno de los principales objetivos del presente trabajo. En los últimos años, ha habido un interés continuo en la participación de los grupos de investigación de las universidades en los estudios de la tecnología espacial a través de sus propios microsatélites. La participación en este tipo de proyectos tiene algunos desafíos inherentes, tales como presupuestos y servicios limitados. Además, debido al hecho de que el objetivo principal de estos proyectos es fundamentalmente educativo, por lo general hay incertidumbres en cuanto a su misión en órbita y cargas útiles en las primeras fases del proyecto. Por otro lado, existen limitaciones predeterminadas para sus presupuestos de masa, volumen y energía, debido al hecho de que la mayoría de ellos están considerados como una carga útil auxiliar para el lanzamiento. De este modo, el costo de lanzamiento se reduce considerablemente. En este contexto, el subsistema estructural del satélite es uno de los más afectados por las restricciones que impone el lanzador. Esto puede afectar a diferentes aspectos, incluyendo las dimensiones, la resistencia y los requisitos de frecuencia. En la primera parte de esta tesis, la atención se centra en el desarrollo de una herramienta de diseño del subsistema estructural que evalúa, no sólo las propiedades de la estructura primaria como variables, sino también algunas variables de nivel de sistema del satélite, como la masa de la carga útil y la masa y las dimensiones extremas de satélite. Este enfoque permite que el equipo de diseño obtenga una mejor visión del diseño en un espacio de diseño extendido. La herramienta de diseño estructural se basa en las fórmulas y los supuestos apropiados, incluyendo los modelos estáticos y dinámicos del satélite. Un algoritmo genético (Genetic Algorithm: GA) se aplica al espacio de diseño para optimizaciones de objetivo único y también multiobjetivo. El resultado de la optimización multiobjetivo es un Pareto-optimal basado en dos objetivo, la masa total de satélites mínimo y el máximo presupuesto de masa de carga útil. Por otro lado, la aplicación de los microsatélites en misiones espaciales es de interés por su menor coste y tiempo de desarrollo. La gran necesidad de las aplicaciones de teledetección es un fuerte impulsor de su popularidad en este tipo de misiones espaciales. Las misiones de tele-observación por satélite son esenciales para la investigación de los recursos de la tierra y el medio ambiente. En estas misiones existen interrelaciones estrechas entre diferentes requisitos como la altitud orbital, tiempo de revisita, el ciclo de vida y la resolución. Además, todos estos requisitos puede afectar a toda las características de diseño. Durante los últimos años la aplicación de CE en las misiones espaciales ha demostrado una gran ventaja para llegar al diseño óptimo, teniendo en cuenta tanto el rendimiento y el costo del proyecto. Un ejemplo bien conocido de la aplicación de CE es la CDF (Facilidad Diseño Concurrente) de la ESA (Agencia Espacial Europea). Está claro que para los proyectos de microsatélites universitarios tener o desarrollar una instalación de este tipo parece estar más allá de las capacidades del proyecto. Sin embargo, la práctica de la CE a cualquier escala puede ser beneficiosa para los microsatélites universitarios también. En la segunda parte de esta tesis, la atención se centra en el desarrollo de una estructura de optimización de diseño multidisciplinar (Multidisciplinary Design Optimization: MDO) aplicable a la fase de diseño conceptual de microsatélites de teledetección. Este enfoque permite que el equipo de diseño conozca la interacción entre las diferentes variables de diseño. El esquema MDO presentado no sólo incluye variables de nivel de sistema, tales como la masa total del satélite y la potencia total, sino también los requisitos de la misión como la resolución y tiempo de revisita. El proceso de diseño de microsatélites se divide en tres disciplinas; a) diseño de órbita, b) diseño de carga útil y c) diseño de plataforma. En primer lugar, se calculan diferentes parámetros de misión para un rango práctico de órbitas helio-síncronas (sun-synchronous orbits: SS-Os). Luego, según los parámetros orbitales y los datos de un instrumento como referencia, se calcula la masa y la potencia de la carga útil. El diseño de la plataforma del satélite se estima a partir de los datos de la masa y potencia de los diferentes subsistemas utilizando relaciones empíricas de diseño. El diseño del subsistema de potencia se realiza teniendo en cuenta variables de diseño más detalladas, como el escenario de la misión y diferentes tipos de células solares y baterías. El escenario se selecciona, de modo de obtener una banda de cobertura sobre la superficie terrestre paralelo al Ecuador después de cada intervalo de revisita. Con el objetivo de evaluar las interrelaciones entre las diferentes variables en el espacio de diseño, todas las disciplinas de diseño mencionados se combinan en un código unificado. Por último, una forma básica de MDO se ajusta a la herramienta de diseño de sistema de satélite. La optimización del diseño se realiza por medio de un GA con el único objetivo de minimizar la masa total de microsatélite. Según los resultados obtenidos de la aplicación del MDO, existen diferentes puntos de diseños óptimos, pero con diferentes variables de misión. Este análisis demuestra la aplicabilidad de MDO para los estudios de ingeniería de sistema en la fase de diseño conceptual en este tipo de proyectos. La principal conclusión de esta tesis, es que el diseño clásico de los satélites que por lo general comienza con la definición de la misión y la carga útil no es necesariamente la mejor metodología para todos los proyectos de satélites. Un microsatélite universitario, es un ejemplo de este tipo de proyectos. Por eso, se han desarrollado un conjunto de herramientas de diseño para encarar los estudios de la fase inicial de diseño. Este conjunto de herramientas incluye diferentes disciplinas de diseño centrados en el subsistema estructural y teniendo en cuenta una carga útil desconocida a priori. Los resultados demuestran que la mínima masa total del satélite y la máxima masa disponible para una carga útil desconocida a priori, son objetivos conflictivos. En este contexto para encontrar un Pareto-optimal se ha aplicado una optimización multiobjetivo. Según los resultados se concluye que la selección de la masa total por satélite en el rango de 40-60 kg puede considerarse como óptima para un proyecto de microsatélites universitario con carga útil desconocida a priori. También la metodología CE se ha aplicado al proceso de diseño conceptual de microsatélites de teledetección. Los resultados de la aplicación del CE proporcionan una clara comprensión de la interacción entre los requisitos de diseño de sistemas de satélites, tales como la masa total del microsatélite y la potencia y los requisitos de la misión como la resolución y el tiempo de revisita. La aplicación de MDO se hace con la minimización de la masa total de microsatélite. Los resultados de la aplicación de MDO aclaran la relación clara entre los diferentes requisitos de diseño del sistema y de misión, así como que permiten seleccionar las líneas de base para el diseño óptimo con el objetivo seleccionado en las primeras fase de diseño. ABSTRACT This thesis is done in the context of UPMSat-2 project, which is a microsatellite under design and manufacturing at the Instituto Universitario de Microgravedad “Ignacio Da Riva” (IDR/UPM) of the Universidad Politécnica de Madrid. Application of Concurrent Engineering (CE) methodology in the framework of Multidisciplinary Design application (MDO) is one of the main objectives of the present work. In recent years, there has been continuing interest in the participation of university research groups in space technology studies by means of their own microsatellites. The involvement in such projects has some inherent challenges, such as limited budget and facilities. Also, due to the fact that the main objective of these projects is for educational purposes, usually there are uncertainties regarding their in orbit mission and scientific payloads at the early phases of the project. On the other hand, there are predetermined limitations for their mass and volume budgets owing to the fact that most of them are launched as an auxiliary payload in which the launch cost is reduced considerably. The satellite structure subsystem is the one which is most affected by the launcher constraints. This can affect different aspects, including dimensions, strength and frequency requirements. In the first part of this thesis, the main focus is on developing a structural design sizing tool containing not only the primary structures properties as variables but also the satellite system level variables such as payload mass budget and satellite total mass and dimensions. This approach enables the design team to obtain better insight into the design in an extended design envelope. The structural design sizing tool is based on the analytical structural design formulas and appropriate assumptions including both static and dynamic models of the satellite. A Genetic Algorithm (GA) is applied to the design space for both single and multiobejective optimizations. The result of the multiobjective optimization is a Pareto-optimal based on two objectives, minimum satellite total mass and maximum payload mass budget. On the other hand, the application of the microsatellites is of interest for their less cost and response time. The high need for the remote sensing applications is a strong driver of their popularity in space missions. The satellite remote sensing missions are essential for long term research around the condition of the earth resources and environment. In remote sensing missions there are tight interrelations between different requirements such as orbital altitude, revisit time, mission cycle life and spatial resolution. Also, all of these requirements can affect the whole design characteristics. During the last years application of the CE in the space missions has demonstrated a great advantage to reach the optimum design base lines considering both the performance and the cost of the project. A well-known example of CE application is ESA (European Space Agency) CDF (Concurrent Design Facility). It is clear that for the university-class microsatellite projects having or developing such a facility seems beyond the project capabilities. Nevertheless practicing CE at any scale can be beneficiary for the university-class microsatellite projects. In the second part of this thesis, the main focus is on developing a MDO framework applicable to the conceptual design phase of the remote sensing microsatellites. This approach enables the design team to evaluate the interaction between the different system design variables. The presented MDO framework contains not only the system level variables such as the satellite total mass and total power, but also the mission requirements like the spatial resolution and the revisit time. The microsatellite sizing process is divided into the three major design disciplines; a) orbit design, b) payload sizing and c) bus sizing. First, different mission parameters for a practical range of sun-synchronous orbits (SS-Os) are calculated. Then, according to the orbital parameters and a reference remote sensing instrument, mass and power of the payload are calculated. Satellite bus sizing is done based on mass and power calculation of the different subsystems using design estimation relationships. In the satellite bus sizing, the power subsystem design is realized by considering more detailed design variables including a mission scenario and different types of solar cells and batteries. The mission scenario is selected in order to obtain a coverage belt on the earth surface parallel to the earth equatorial after each revisit time. In order to evaluate the interrelations between the different variables inside the design space all the mentioned design disciplines are combined in a unified code. The integrated satellite system sizing tool developed in this section is considered as an application of the CE to the conceptual design of the remote sensing microsatellite projects. Finally, in order to apply the MDO methodology to the design problem, a basic MDO framework is adjusted to the developed satellite system design tool. Design optimization is done by means of a GA single objective algorithm with the objective function as minimizing the microsatellite total mass. According to the results of MDO application, there exist different optimum design points all with the minimum satellite total mass but with different mission variables. This output demonstrates the successful applicability of MDO approach for system engineering trade-off studies at the conceptual design phase of the design in such projects. The main conclusion of this thesis is that the classical design approach for the satellite design which usually starts with the mission and payload definition is not necessarily the best approach for all of the satellite projects. The university-class microsatellite is an example for such projects. Due to this fact an integrated satellite sizing tool including different design disciplines focusing on the structural subsystem and considering unknown payload is developed. According to the results the satellite total mass and available mass for the unknown payload are conflictive objectives. In order to find the Pareto-optimal a multiobjective GA optimization is conducted. Based on the optimization results it is concluded that selecting the satellite total mass in the range of 40-60 kg can be considered as an optimum approach for a university-class microsatellite project with unknown payload(s). Also, the CE methodology is applied to the remote sensing microsatellites conceptual design process. The results of CE application provide a clear understanding of the interaction between satellite system design requirements such as satellite total mass and power and the satellite mission variables such as revisit time and spatial resolution. The MDO application is done with the total mass minimization of a remote sensing satellite. The results from the MDO application clarify the unclear relationship between different system and mission design variables as well as the optimum design base lines according to the selected objective during the initial design phases.