44 results found Selected 0 items No itemsClear selection Select / deselect all results (all pages, 44 total) Metabolic Characterisation of the MELiSSA Waste Compartment. Phase 1. The objective of the Metabolic Characterization of the MELiSSA Waste Compartment, Phase 1 project is to fully characterize, in terms of taxonomy and functional capacity, the microbial community present in the C1 Anaerobic Liquefaction Sub-System (ALSS). Belgium GSTP G513-057MM KATHOLIEKE UNIVERSITEIT TE LEUVEN 2014 - 2018 Metabolic Characterisation of the MELiSSA Waste Compartment. Phase 1. Concept Development of EVA Operationsin EAC Neutral Buoyancy Facility for Extra-terrestrial Surface Explorations. (Moondive) The International Space Station (ISS) is slowly approaching the end of its mission. The European Space Agency (ESA) and its international partners are considering new mission targets for the future of human space exploration in the post-ISS era. Highest ranked on the list of potential targets are a return to the Moon, Near-Earth Objects or asteroids, the moons of Mars (Phobos, Deimos) and, as the ultimate target, the surface of Mars. France Discovery 13-039 COMEX SA 2015 - 2018 Concept Development of EVA Operationsin EAC Neutral Buoyancy Facility for Extra-terrestrial Surface Explorations. (Moondive) Development of Thermal Insulation for Planetary Landers and Rovers Activity with GSTP and RUAG, Austria, to develop a thermal insulation suitable for planetary landers and rover. An extensive trade-off of on various materials was carried out and supported by full material characterisation tests. Two insulation concepts were selected: foam and a gas gap. The technical solutions are light weight, flexible and can be applied directly on the external/internal walls, wrapped around electrical cables and to mechanisms Austria GSTP G513-026MC RUAG SPACE GMBH 2012 - 2017 Development of Thermal Insulation for Planetary Landers and Rovers Focal Plane Assembly Technology Development for SPICA/SAFARI Cryogenic instruments based on imaging arrays of superconducting Transition Edge Sensor (TES) detectors operating at very-low temperature are proposed for future high- and low-energy astrophysics space missions, including the X-IFU instrument for Athena and the SAFARI instrument for SPICA. 2-D arrays of 1000's of TES detectors at 50 mK enable high-sensitivity imaging with high optical efficiency and fast response. Netherlands GSTP G512-010AP Stichting SRON Netherlands Institute for Space Research 2014 - 2016 Focal Plane Assembly Technology Development for SPICA/SAFARI Pagination « First First page ‹‹ Previous page 1 2 3 4 5 Filter by Programme Discovery (24) TDE (11) GSTP (8) Preparation (1) Filter by Start Year 2020 (10) 2018 (7) 2021 (6) 2022 (6) 2017 (4) 2014 (3) 2019 (3) 2015 (2) 2012 (1) 2016 (1) 2023 (1) Filter by End Year 2023 (21) 2018 (9) 2019 (6) 2022 (4) 2016 (1) 2017 (1) 2021 (1) 2024 (1) Filter by Keywords ISRU (10) Moon (8) lunar base (3) Lunar Lander (3) 2-Contamination and Radiation (2) 3-Habitation (2) 3-In-Situ Resource Utilisation (ISRU) (2) 3d printing (2) Ariadna (2) Exploration (2) 3-Human Spaceflight and Exploration Preparation (1) 4-Life Support and Medical (1) 22-Environmental Control & Life Support (ECLS) and In Situ Resource Utilisation (ISRU) (1) Analogue (1) Asteroid (1) Asteroids (1) Astronaut (1) astronaut training (1) Below Freezing Water Storage (1) EAC (1) Energy Storage (1) EVA (1) feeback (1) in-space manufacturing (1) inflatable (1) inflatable structure (1) Instrument (1) ISS (1) lunar caves (1) lunar habitat (1) Lunar Water Storage (1) Mars (1) Moon base (1) moon village (1) NBF (1) Off-Earth Habitats (1) Off-Earth manufacturing (1) Power (1) recycling (1) Robotics (1) Space debris (1) thermite (1) Filter by Contractor KATHOLIEKE UNIVERSITEIT TE LEUVEN (2) OHB System AG (2) SPACE APPLICATIONS SERV. 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