322 results found Selected 0 items No itemsClear selection Select / deselect all results (all pages, 322 total) LPSS-380 Separation System Development Activity addresses the necessity of developing a competitive European Sep Spain GSTP G627-083MS AIRBUS DEFENCE AND SPACE S.A.U. 2017 - 2023 LPSS-380 Separation System Development AI-powered Digital Assistant for space - system engineering The space mission development process tends to show several commonalities across projects. Indeed, systems often use the same generic set of technologies, with similar assumptions and requirements. The use of a Digital Assistant would be able to recognise such commonalities and propose suggestions during the early phase of system development based on previous projects. This would speed the definition stages, while also allowing to re-use potential lessons learned and hopefully to avoid simple mistakes/omissions. Netherlands TDE T708-706SY RHEA SYSTEM B.V. 2022 - 2023 AI-powered Digital Assistant for space - system engineering De-risk assessment: Elysium Space Trainer: Light-weight exoskeleton-based training device for countermeasure exercises in microgravity Background and justification: Germany GSTP G617-241TAid Elysium Industries UG 2022 - 2023 De-risk assessment: Elysium Space Trainer: Light-weight exoskeleton-based training device for countermeasure exercises in microgravity Robust and (semi) Autonomous Platform for Increased Distances (RAPID) In 50 years of Space Exploration, the total distance covered by rovers on Mars and the Moon is about 200km, an average of 4km per year. Future exploration rovers are expected to travel one or two orders of magnitude more.This requires designing rovers that are intrinsically faster than what has been built so far. Spain TDE T313-702MM GMV AEROSPACE AND DEFENCE, SA 2021 - 2023 Robust and (semi) Autonomous Platform for Increased Distances (RAPID) AstronauT HeaLtH EnhancemenT Integrated Countermeasure (ATHLETIC) Future human space exploration, including missions to the Moon and beyond, will require a paradigm shift in the current approach to in-flight exercise countermeasures, particularly when it comes to exercise devices (e.g. CEVIS, T2, ARED to name a few). Exploration vehicles will be significantly smaller, requiring exercise hardware to be smaller, lighter and less complex than current devices, and ideally multi-functional, capable of stressing the musculoskeletal (MSK) system, the cardiovascular (CV) system and other associated system (e.g. neuro-vestibular - NV). Belgium TDE T313-501MM SPACE APPLICATIONS SERV. S.A./N.V. 2018 - 2023 AstronauT HeaLtH EnhancemenT Integrated Countermeasure (ATHLETIC) HENON - Phases A and B . Italy GSTP GT37-001SYu ARGOTEC S.R.L. 2022 - 2023 HENON - Phases A and B LUnar Geology Orbiter (LUGO) The LUnar Geology Orbiter (LUGO) is a scientific and exploratory mission to study the thermal evolution of the Moon by characterizing Irregular Mare Patches, as well as lunar lava tubes. This will be accomplished by four payloads, a ground penetrating radar, a hyperspectral camera, LiDAR and narrow angle camera, which will produce images at a greater resolution than currently available. The scientific study will provide confirmation or refutation of current knowledge about the thermal evolution of the Moon. Czech Republic Discovery EISI_I-2022-05141 TRL Space 2023 - 2023 LUnar Geology Orbiter (LUGO) Spacecraft demise during re-entry expedited using various exothermic reactions Uncontrolled spacecraft re-entry requires the satellite to sufficiently demise in order to meet the casualty risk requirement. Heat generated during re-entry is not adequate to sufficiently demise some spacecraft equipment. - Equipment (e.g. Large mechanisms, magnetorques, optical equipment) is hard to demise without big design changes as the functionality requires using metals with high melting temperatures. - Earlier break-up of the interface of equipment to the structure, harness and pipework is beneficial for demisability. Germany TDE T711-601MS HTG- HYPERSCHALL TECHNOLOGIE Goettingen GmbH 2021 - 2023 Spacecraft demise during re-entry expedited using various exothermic reactions Process-Structure-Property Modelling of Powder-Bed Additive Manufacturing Parts for Space Applications Powder-bed metal additive manufacturing processes allow to build three-dimensional parts by successive formation of pools of molten metal, which solidify on the previously built layers. Multiple parameters influence the generated microstructure, including the power input on the deposited metal, the powder particle size, the printing pattern and the layer thickness. Changes in one or several of those parameters affect the grain structure of the material and therefore the resulting mechanical properties of the printed part. Finland TDE T724-610MS VTT TECHNICAL RESEARCH CENTRE OF FINLAND LTD 2021 - 2023 Process-Structure-Property Modelling of Powder-Bed Additive Manufacturing Parts for Space Applications DANOE Phase II (High Dynamic Absolute Nanometric Optical Encoder technology assessment for space) Combining all the features in a position encoder such as high-resolution, absolute, compact, high-speed is a challenge today. An optical absolute position encoder technology has the potential to combine all these attractive features. Nanometric resolution can be established using dedicated optical sensor, a transmissive scale, LED illumination, without the need for optics (shadow-imaging). Optic-less shadowimaging permits compact design and major cost reduction. 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