217 results found Selected 0 items No itemsClear selection Select / deselect all results (all pages, 217 total) Space Weather Impact on Arctic Navigation (SWAN) The objective of the Space Weather impact on Arctic Navigation (SWAN) project has been todevelop and demonstrate new techniques, which are expected to improve on the currentstate-of-the-art space weather forecasting techniques and products related to space weathereffects for Positioning, Navigation and Timing (PNT) systems in the Arctic, with particularattention to the Greenland area. Denmark Preparation 19-P-O-NAV-01-a DTU Space 2020 - 2022 Space Weather Impact on Arctic Navigation (SWAN) Magnetic Powder as Propellant in Electrostatic Thrusters (MPEP) The main objectives of this project were to develop a thruster prototype based on magnetic powder electrostatic propulsion and to test it in vacuum with direct thrust measurements. The aim was to check the robustness of the concept and to measure and calculate important performance parameters such as thrust and specific impulse, to allow a comparison with other thruster technologies. This project demonstrated for the first time the feasibility of electrostatic propulsion based on powder emission. Austria Discovery S 2020-02-a FOTEC GmbH 2020 - 2022 Magnetic Powder as Propellant in Electrostatic Thrusters (MPEP) Elucidating modes of interaction of redox-active nanomaterials with biological systems exposed to microgravity Permanence in microgravity conditions is well known to have detrimental effects on biological systems and living organisms, limiting in particular human space operations and exploration both over short and long term periods, as it promotes/accelerates some degenerative processes associated to aging and often to pathology onset on Earth. Italy Discovery 19-D-R-TEC-06 Istituto Italiano di Tecnologia 2020 - 2022 Elucidating modes of interaction of redox-active nanomaterials with biological systems exposed to microgravity Characterization of light polarization properties of virgin and marine-harvested plastic litter toward remote-sensing mapping of ocean plastics - Ocean Plastics Polarization Properties OP³ Detecting, identifying, quantifying and tracking strategies for leakage plastic litter in terrestrial as well as aquatic environments using remote sensing technologies is expected to support future continuous monitoring of waste pollution at wide covering geo-spatial scales. The methodologies to detect plastic waste from airborne or satellite observations should be based on fundamental and well-characterised optical features. Germany Discovery 20-D-T-TEC-01 Carl von Ossietzky Universitat Oldenburg 2020 - 2022 Characterization of light polarization properties of virgin and marine-harvested plastic litter toward remote-sensing mapping of ocean plastics - Ocean Plastics Polarization Properties OP³ Multi-wavelength clock control unit MW-CCU Multiple narrow bandwidth lasers are required for quantum sensor systems. These systems rely on specific coherent sources for laser cooling and trapping, atomic state preparation and interrogation of the cold atomic samples. There is also a parallel requirement to deliver these specific lasers (at the experiment) for predefined periods. Wavelength knowledge to a high accuracy and precision, control and/or removal of the laser frequency drift are key additional attributes of the desired system. This system is known as the Clock Control Unit (CCU). United Kingdom GSTP GT17-203MM NATIONAL PHYSICAL LABORATORY - NPL Management Limited 2020 - 2022 Multi-wavelength clock control unit MW-CCU Artificial intelligence (AI) and natural language processing (NLP) to support space engineering activities Model based approaches have proved to be efficient in supporting engineering activities, models replacing traditional document-based approaches. Nevertheless even in most advanced deployments, a lot of engineering artifacts are textual either because the return on investment of introducing models is too low on this particular case or because the information is more efficiently expressed in natural language even if consistency and correctness issues appears. France Discovery 20-D-T-TEC-04-n Thales Alenia Space 2020 - 2022 Artificial intelligence (AI) and natural language processing (NLP) to support space engineering activities De-risk assessment: Model Based FDIR design Today, spacecraft FDIR (Fault Detection, Isolation and Recovery) design is a time-consuming and error prone paper-based workflow, which does not help mastering the growing complexity of the space systems, and which mostly prevents early validation and verification of the design. Adequacy of the FDIR design is often assessed very late in the process (integration and test phase), sometimes even after the launch of the spacecraft (FDIR parameter tuning). France GSTP G617-241TAeh THALES ALENIA SPACE FRANCE 2020 - 2022 De-risk assessment: Model Based FDIR design Open Standard for Inter Satellite Link A number of missions are being investigated, under development or even already flying that use the concept of multiple spacecraft interconnected with an intersatellite Link (ISL); they are mainly nano/smallsats (Proba-3 and Gomex-4a/b as current generation examples and AIM/HERA as future non-LEO case) but with clear interest also for regular mission. United Kingdom TDE T706-602ES QiNETIQ LTD. 2020 - 2021 Open Standard for Inter Satellite Link Marine Litter Aggregation Forecast Marine Litter Aggregation Forecast presents a new estimation of long-term global distribution of marine litter proceeding from land-based and from sea-based sources at global scale, taking advantage of numerical reanalysis databases of historical met-ocean conditions. Different machine learning techniques are applied to generate long-term climate-based series of those environmental variables that may affect the drift of marine litter over the sea surface such as currents, wind and wave-induced Stokes drift. Germany Discovery 20-D-S-TEC-01-f Deep Blues Globe 2020 - 2021 Marine Litter Aggregation Forecast Inflatable Systems for Aerocapture and Aerobraking This work has primarily focused on establishing scenarios where inflatable devices could be the most useful. Given that these missions rely on aerodynamic drag that results in (potentially significant) heating, the authors have sought to find solutions to minimize heat fluxes acting on the device surface, and especially keeping it within the limits of flexible/foldable TPS materials for the aerocapture scenario. 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