Structural verification of the ESEO spacecraft: from launch loads analysis to composite panels verification

The present thesis work was performed in the frame of ESEO (European Student Earth Orbiter) project. The activities that are described in this document were carried out in the Microsatellites and Space Micro systems Lab led by Professor Paolo Tortora and in ALMASpace company facilities. The thesis deals with ESEO structural analysis, at system and unit level, and verification: after determining the design limit loads to be applied to the spacecraft as an envelope of different launchers load profiles, a finite element structural analysis was performed on the model of the satellite in order to ensure the capability to withstand the loads encountered during the launch; all the analyses were performed according to ESA standards and using the software MSC NASTRAN SIMXPERT. Amplification factors were derived and used to determine loads to be considered at unit level. In particular structural analyses were carried out on the GPS unit, the payload developed for ESEO by students of University of Bologna and results were used in the preparation of GPS payload design definition file. As for the verification phase a study on the panels and inserts to be used in the spacecraft was performed: different designs were created exploiting methods to optimize weight and mechanical behavior. The configurations have been analyzed and results compared to select the final design.

Evolution of the structural and fracture design of the ISS payloads due to the new launchers, specifically applied to Biolab IEC-2 projects

The relatively young discipline of astronautics represents one of the scientifically most fascinating and technologically advanced achievements of our time. The human exploration in space does not offer only extraordinary research possibilities but also demands high requirements from man and technology. The space environment provides a lot of attractive experimental tools towards the understanding of fundamental mechanism in natural sciences. It has been shown that especially reduced gravity and elevated radiation, two distinctive factors in space, influence the behavior of biological systems significantly. For this reason one of the key objectives on board of an earth orbiting laboratory is the research in the field of life sciences, covering the broad range from botany, human physiology and crew health up to biotechnology. The Columbus Module is the only European low gravity platform that allows researchers to perform ambitious experiments in a continuous time frame up to several months. Biolab is part of the initial outfitting of the Columbus Laboratory; it is a multi-user facility supporting research in the field of biology, e.g. effect of microgravity and space radiation on cell cultures, micro-organisms, small plants and small invertebrates. The Biolab IEC are projects designed to work in the automatic part of Biolab. In this moment in the TO-53 department of Airbus Defence & Space (formerly Astrium) there are two experiments that are in phase C/D of the development and they are the subject of this thesis: CELLRAD and CYTOSKELETON. They will be launched in soft configuration, that means packed inside a block of foam that has the task to reduce the launch loads on the payload. Until 10 years ago the payloads which were launched in soft configuration were supposed to be structural safe by themselves and a specific structural analysis could be waived on them; with the opening of the launchers market to private companies (that are not under the direct control of the international space agencies), the requirements on the verifications of payloads are changed and they have become much more conservative. In 2012 a new random environment has been introduced due to the new Space-X launch specification that results to be particularly challenging for the soft launched payloads. The last ESA specification requires to perform structural analysis on the payload for combined loads (random vibration, quasi-steady acceleration and pressure). The aim of this thesis is to create FEM models able to reproduce the launch configuration and to verify that all the margins of safety are positive and to show how they change because of the new Space-X random environment. In case the results are negative, improved design solution are implemented. Based on the FEM result a study of the joins has been carried out and, when needed, a crack growth analysis has been performed.

ALMASat-1, ALMASat-EO and beyond: evolution of structural concepts and technologies towards multifunctional structures for microsatellites

Multifunctional Structures (MFS) represent one of the most promising disruptive technologies in the space industry. The possibility to merge spacecraft primary and secondary structures as well as attitude control, power management and onboard computing functions is expected to allow for mass, volume and integration effort savings. Additionally, this will bring the modular construction of spacecraft to a whole new level, by making the development and integration of spacecraft modules, or building blocks, leaner, reducing lead times from commissioning to launch from the current 3-6 years down to the order of 10 months, as foreseen by the latest Operationally Responsive Space (ORS) initiatives. Several basic functionalities have been integrated and tested in specimens of various natures over the last two decades. However, a more integrated, system-level approach was yet to be developed. The activity reported in this thesis was focused on the system-level approach to multifunctional structures for spacecraft, namely in the context of nano- and micro-satellites. This thesis documents the work undertaken in the context of the MFS program promoted by the European Space Agency under the Technology Readiness Program (TRP): a feasibility study, including specimens manufacturing and testing. The work sequence covered a state of the art review, with particular attention to traditional modular architectures implemented in ALMASat-1 and ALMASat-EO satellites, and requirements definition, followed by the development of a modular multi-purpose nano-spacecraft concept, and finally by the design, integration and testing of integrated MFS specimens. The approach for the integration of several critical functionalities into nano-spacecraft modules was validated and the overall performance of the system was verified through relevant functional and environmental testing at University of Bologna and University of Southampton laboratories.

Rebranding feminism: An analysis of present-day feminism

The purpose of this dissertation is to reflect on the meaning of feminism in order to decide whether the movement needs a rebranding. The first part will focus on the history of feminism to clarify its beliefs and goals. The following part will highlight how feminism gained a bad reputation over time and will show Elle’s attempt in November 2013 to launch a project to rebrand the movement. The last part will explain what present-day feminism consists of by listing some of the latest projects and the most important issues the movement has to tackle. My analysis will finally show that the F-movement needs a rebranding and, in order to be effective, men should join women’s fight for equality. “We should all be feminists”.

Tradurre il genere documentario : Due proposte di sottotitolaggio del documentario Little Land a confronto

The aim of this thesis is to discuss the main translation issues encountered while performing a double version of the subtitles of the documentary “Little Land” from English into Italian. The main motivation behind my choice is a personal interest in the subtitling field applied to the documentary filmic genre. This project is divided into two parts. The first part constitutes the theoretical basis of the thesis and is divided in three chapters. The first chapter introduces the documentary “Little Land” and analyses its main features and characteristics. The second chapter is devoted to documentary studies and theory of documentary, including the historical overview of the changes of this filmic genre and an overview of its market potential in order to meet both the audience and the director’s requirements. The third chapter deals with audiovisual translation as a discipline, and analyses the main translation techniques adopted for the documentary genre: dubbing, voice-over and subtitling. The subtitling section is particularly rich, and a discussion of the use of double and pivot subtitles and the possibilities of subtitling for accessibility issues is included. The second part constitutes the practical development of the theories introduced and dealt with in the first part. Chapter four provides an overview of the history of the Cineteca di Bologna, for whom I worked as a subtitler, and explains the guide lines and equipment required in order to perform the manual launch of the subtitles during their festival Human Rights Nights. The fifth and final chapter provides an analysis of the second version of the subtitles, meant for TV broadcasting, and highlights the main issues encountered during the translation process, both from a structural and a lexical point of view. A discussion of the different translation strategies adopted is provided, in a constant comparison with the first version of the subtitles. The function of self-reflection and self-observation in translation is also examined. Appendix A and B contain the interviews with “Little Land”’s director and protagonist respectively, Appendix C contains the subtitles table.