223 results found Selected 0 items No itemsClear selection Select / deselect all results (all pages, 223 total) European Methods for Thermo-Elastic Verification Almost every Scientific and Earth Observation spacecraft has stringent thermo-elastic stability/alignment requirements for the spacecraft. During the reviews of almost all of these projects many discussions on verifyng these requirements. The criticality and the complexity to verify compliance has become evident from projects like Herschel telescope, GAIA, Bepi Colombo and Solar Orbiter. France TDE T708-601MS THALES ALENIA SPACE FRANCE 2020 - 2023 European Methods for Thermo-Elastic Verification 6U LV-POD EQM Maximising the heritage of the existing ISIS ISIPOD cubesat deployers family, and building on past studies performed within ESA GSP such as LV-POD, (Low-Velocity deployer),the main task of this TFO activity will be to :-Design a Low-Velocity 6U deployer suitable for deep space missions, compatible with the low separation velocity (order cm/s) and rotation error needed for deep space mission such as Hera, taking into account a series of requirements injected by the agency -Define interfaces w.r.t. Netherlands GSTP G637-001TFy ISIS-INNOVATIVE SOLUTIONS IN SPACE 2019 - 2023 6U LV-POD EQM Toward next generation 3D printed materials for space applications: hierarchical nano-porous structures with engineered macro-architectures The main goal of this project was to fabricate porous electrodes used in fuel cells. A porous electrode consists of a catalyst layer (CL), microporous layer (MPL) and gas diffusion layer (GDL). GDLs are conventionally made of carbon paper or cloth. However, there are several drawbacks, including degregation in alkalin media, deformation, and consequently, closure of pores under compression, and randomness of pore charactristics (e.g., pore size and distribution). As an alternative, metallic GDLs with much greater mechanical strengths have recently been introduced for alkalin environements. The Netherlands Discovery ETD 2020-09 UNIVERSITY OF TWENTE 2023 - 2023 Toward next generation 3D printed materials for space applications: hierarchical nano-porous structures with engineered macro-architectures Thruster Pointing Mechanism Development The increasing interest for Deep-Space cubesat is leading in the near future to the need of adequate deployment systems (``Cubesat Dispensers``) suitable for deep space applications, taking into account all the environmental (e.g. radiation) and mission constraints (e.g. need for power supply to the cubesat, possibility to upload SW updates, need for accurate release conditions). Canada GSTP GT27?111MS MacDonald, Dettwiler and Associates Corporation 2021 - 2023 Thruster Pointing Mechanism Development Advanced aluminium alloys tailored for Additive Manufacturing space applications, targeting high end structural spacecraft parts Additive Manufacturing is rapidly emerging as an advanced manufacturing technique, which will be adopted by the European Space Industry. Since the method involves the process of melting and solidification, it is particularly suited to those materials that are readily weldable and have good castability. Since titanium and its alloys are readily weldable by a number of fusion welding techniques, it is not surprising that in the majority of current activities, titanium is the material of choice. Belgium GSTP G61A-019QT CRM CENTRE DE RECHERCHES METALLURGIQUES ASBL 2018 - 2023 Advanced aluminium alloys tailored for Additive Manufacturing space applications, targeting high end structural spacecraft parts Mobile – Selective Laser Melting (M-SLM) for Construction on the Moon When setting up a lunar station, technologies for the use of locally available materials are crucial. Such technologies drastically reduce the need for transportation from Earth. This project idea aims to provide proof of a key technology, namely Mobile – Selective Laser Melting (M-SLM) for building large structures on the Moon. Germany Discovery 20-D-T-TEC-03-f Technische Universität Berlin 2021 - 2023 Mobile – Selective Laser Melting (M-SLM) for Construction on the Moon GE⊕ Lunar Power Station The main objective of the study is to investigate the technological feasibility of implementing the GE⊕-LPS concept, and its role as a prototype for proposed cislunar scenarios supplying electric power to Earth. The methodological approach to the study has been to identify and validate the most simple and effective solutions which ould be practically implemented with known and existing technologies and approaches. Switzerland Discovery 21-D-S-TEC-01-d Astrostrom GmbH 2021 - 2023 GE⊕ Lunar Power Station Material Properties under cryogenic conditions (LH2/GH2 and LOx/GOx) Test data on material properties and material performance under cryogenic conditions are increasingly required or current and future research, development and application activities (e.g. launcher propulsion systems). The very limited available data base does currently not cover new advanced metallic alloys, composite materials or materials manufactured with new processes e.g. Additive Manufacturing as selected and required for the next generation launcher and spacecraft missions. Germany TDE T724-509QT ENERGIE TECHNOLOGIE GMBH 2017 - 2023 Material Properties under cryogenic conditions (LH2/GH2 and LOx/GOx) De-risk assessment: Improvement of Reliability and Lifetime for Rotary Type Stirling Coolers Background and justification: Slovenia GSTP G617-241TAgs Le-tehnika do.o. 2021 - 2023 De-risk assessment: Improvement of Reliability and Lifetime for Rotary Type Stirling Coolers Water Storage System for Lunar Life Support and Exploration A system is researched and developed to store water in its liquid state at temperatures below the freezing point using a passive unfreezing method. This is achieved by mixing it with phytantriol, a commercially available non-toxic, non-volatile, non-corrosive, non-inflammable lipid. Both, the scale up of the enrichment process from laboratory scales, and the separation of water from phytantriol, are demonstrated experimentally. 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