Magnetic cleanliness verification approach on tethered satellite

Magnetic cleanliness testing was performed on the Tethered Satellite as the last step of an articulated verification campaign aimed at demonstrating the capability of the satellite to support its TEMAG (TEthered MAgnetometer) experiment. Tests at unit level and analytical predictions/correlations using a dedicated mathematical model (GANEW program) are also part of the verification activities. Details of the tests are presented, and the results of the verification are described together with recommendations for later programs

SEEDS - THE INTERNATIONAL MASTER PROGRAM FOR PREPARING THE YOUNG SYSTEMS ENGINEERS FOR SPACE EXPLORATION

The SEEDS initiative originated by Politecnico di Torino and Thales Alenia Space Italy in 2005. It aimed at establishing a Post Graduate International Master Course in Space Exploration and Development Systems "SEEDS", to offer an opportunity to young engineers to get prepared for the future of Europe in space exploration. The SEEDS project has been shared with Supaero Toulouse in France and with University at Bremen (together with ZARM) in Germany, as the three European towns (Torino, Toulouse and Bremen) have a long common tradition of space activities at both the industrial and academic level and represent three poles of the European cooperation in space programs. The SEEDS course comprises two different steps in sequence: an initial Learning Phase and a Project Work Phase. Both the Learning and the Project Work Phase pursue a multidisciplinary approach, where all specialized disciplines are blended together and integrated to enable the students to acquire the system view and then to accomplish the conceptual design, through the Systems Engineering approach, of a selected case-study. The distinguishing feature of SEEDS is without any doubt the Project Work activity, performed by all students together under the supervision of academic and industrial Tutors, coordinated by the Education Project Manager. Main objective of the Project Work is to train the students on the basic principles of the System Engineering Design, through their application on a well defined project related to a specific space exploration mission. The Project Work includes the Preparatory Work, during which the students, starting from the definition of the mission statement, focus on the identification of the complete architecture of the space exploration mission, and the Conceptual Design activities, performed in the three European sites to develop a limited number of building blocks identified during the Preparatory Work. The first year of activity started in November 2005, with a Plenary Opening which took place at the ESA-ERASMUS Centre, Noordwijk, with the full support of the Human Space-Flight Microgravity and Exploration Directorate of ESA. Five years of activities have passed since then and five project works have been successfully completed, dealing with various space exploration themes. This paper focuses on the description of the SEEDS course and on the main results achieved in terms of project work activities and development of the future space workforce. The positive experience of five years of SEEDS is brought to evidence and the lessons learned are discussed in view of the SEEDS continuatio

FUTURE SPACE EXPLORATION: FROM REFERENCE SCENARIO DEFINITION TO KEY TECHNOLOGIES ROADMAPS

The human exploration of multiple deep space destinations (e.g. Cis-lunar, NEAs), in view of the final challenge of sending astronauts to Mars, represents a current and consistent study domain especially in terms of its possible scenarios and mission architectures assessments, as proved by the numerous on-going activities about this topic and moreover by the Global Exploration Roadmap. After exploring and analysing different possible solutions to identify the most flexible path, a detailed characterization of one out of several Design Reference Missions (DRM) represents a necessity in order to evaluate the feasibility and affordability of deep space exploration missions, specifically in terms of enabling technological capabilities. A human expedition to a NEA, milestone of the GER ‘Asteroid Next' scenario, is considered the mission that would offer the largest suite of benefits in terms of scientific return, operational experience and familiarity on human deep space missions, test of technologies and assessment of human factors for future long-duration expeditions (including planetary bodies), evaluation of In-Situ Resource Utilization (ISRU) and, more specifically, opportunity to test asteroid collision avoidance techniques. The study started from the identification and analysis of feasible evolutionary scenarios for Deep Space Exploration. Different destinations were considered as targets, with particular attention to Earth-Moon Lagrangian points, NEA and Mars as an alternative path to a Moon campaign. In the frame of the scenario selected as the preferable one, a DRM to a NEA (reference target) was defined in detail in terms of architecture and mission elements, as well as of the subsystems composing them. Successively, the critical subsystems and the relevant key technologies were investigated in detail, from their status-of-the-art up to an assessment of their development roadmaps. They shall enable the DRM and support the whole scenario. The paper describes the process that was followed within the study and reports the major obtained results, in terms of scenarios and mission analysis. Furthermore the key technologies that were identified are listed and described highlighting the derived roadmaps for their development according to the reference scenario

A methodology to support strategic decisions in future human space exploration: from scenario definition to building blocks assessment

The human exploration of multiple deep space destinations (e.g. Cis-Lunar, NEAs), in view of the final challenge of sending astronauts to Mars, represents a current and consistent study domain especially in terms of its possible scenarios and mission architectures assessments, as proved by the numerous on-going activities about this topic and moreover by the global exploration roadmap. After exploring and analysing different possible solutions to identify the most flexible path, a detailed characterisation of several Design Reference Missions (DRMs) represents a necessity in order to evaluate the feasibility and affordability of deep space exploration missions, specifically in terms of enabling technological capabilities. The study presented in this paper was aimed at defining an evolutionary scenario for deep space exploration in the next 30 years with the final goal of sending astronauts on the surface of Mars by the end of 2030 decade. Different destinations were considered as targets to build the human exploration scenario, with particular attention to Earth-Moon Lagrangian points, NEA and Moon. For all the destinations selected as part of the exploration scenario, the assessment and characterisation of the relative Design Reference Missions were performed. Specifically they were defined in terms of strategies, architectures and mission elements. All the analyses were based on a pure technical approach with the objective of evaluating the feasibility of a long term strategy for capabilities achievement and technological development to enable future space exploration. This paper describes the process that was followed within the study, focusing on the adopted methodology, and reports the major obtained results, in terms of scenario and mission analysi

The international post-graduate Master programme for space exploration, SEEDS: education and training from a System Engineering perspective

The SEEDS (SpacE Exploration Development Systems) initiative was initially conceived and promoted by Politecnico di Torino and Thales Alenia Space-Italy in 2005. It aimed at establishing a post-graduate International Master Program in space exploration to offer an opportunity to young engineers to get prepared for the future of Europe in space and specifically in human space exploration. ISAE-Supaero in France and University of Leicester in UK participate to SEEDS together with Politecnico di Torino (Italy). Turin, Toulouse and Leicester have a long common tradition of space activities at both the industrial and academic level and within the SEEDS initiative they represent three poles of European cooperation in space programs. The Master course comprises two different steps in sequence: an initial learning phase and a Project Work phase. Both phases pursue a multidisciplinary approach, where all specialized disciplines are integrated to make the students able to acquire the system view and then to accomplish the conceptual design of a selected case-study. The distinguishing feature of SEEDS is the Project Work activity, performed by all students together under the supervision of academic and industrial tutors. Main objective of the Project Work is to train the students on the basic principles of the system engineering design, through their application to a well-defined project related to a specific human space exploration mission. The Project Work includes the Preparatory Work, during which the students identify the complete architecture and overall scenario of the mission, and the conceptual design activities, performed in the three European sites to develop a limited number of building blocks. Seven academic years of activities have passed and seven project works have been successfully completed, dealing with various space exploration themes. The eighth edition is currently under way with the aim of designing a “Transit and return habitable Mars orbital port”. The paper focuses on the description of the Master Program, both from the point of view of its contents, structure and multidisciplinary design methodologies, and on the main results achieved in terms of Project Work activities. The positive experience of seven years of SEEDS is brought to evidence and the lessons learned are discussed

Materials and Textile Architecture Analyses for Mechanical Counter-Pressure Space Suits using Active Materials

Mechanical counter-pressure (MCP) space suits have the potential to improve the mobility of astronauts as they conduct planetary exploration activities. MCP suits differ from traditional gas-pressurized space suits by applying surface pressure to the wearer using tight-fitting materials rather than pressurized gas, and represent a fundamental change in space suit design. However, the underlying technologies required to provide uniform compression in a MCP garment at sufficient pressures for space exploration have not yet been perfected, and donning and doffing a MCP suit remains a significant challenge. This research effort focuses on the novel use of active material technologies to produce a garment with controllable compression capabilities (up to 30 kPa) to address these problems. We provide a comparative study of active materials and textile architectures for MCP applications; concept active material compression textiles to be developed and tested based on these analyses; and preliminary biaxial braid compression garment modeling results.United States. National Aeronautics and Space Administration (OCT Space Technology Research Fellowship Grant NNX11AM62H)MIT-Portugal Progra