83 results found Selected 0 items No itemsClear selection Select / deselect all results (all pages, 83 total) De-risk assessment: Space Radiation Effects Nowcast (SREN) platform Background and justification: Space environment includes severe radiation and plasma storms - driven by solar activity and its effect on the Earth’s magnetosphere – affecting satellite systems. Greece GSTP G617-241TAcp SPARC: Space Applications and Research Consultancy 2019 - 2020 De-risk assessment: Space Radiation Effects Nowcast (SREN) platform Development of a high energy beam combination, ions and electrons, for radiation test of electronic components The test of electronic components under radiation is becoming increasingly difficult because of denser and more complex packaging of the state-of-art components, such as microprocessors, memories, FPGAs, packaged in plastic, ceramic or Flip- chip configurations.This implies a larger beam range of the irradiation beam combinations, in order to reach the active and radiation-sensitive semi-conductor die of the component. The larger beam range is obtained with a high energy beam combination. Finland GSTP G617-156QE UNIV JYVASKYLA 2014 - 2020 Development of a high energy beam combination, ions and electrons, for radiation test of electronic components Removal of the VESPA upper part The objective of the Landmark ClearSpace-1 mission will be to demonstrate the complete value chain of active debris removal by removing an ESA-owned object (a VESPA upper part orbiting at an altitude of 500 km) by 2025. Switzerland Discovery 19-D-S-TEC-03 ClearSpace 2019 - 2020 Removal of the VESPA upper part 3D Energetic Electron Spectrometer Phases C and D The 3DEES design established in the previous activity has multiple sensor stacks, each sampling a different direction. The detection techniques build on the technology from the general-purpose Energetic Particle Telescope (EPT) that is flying on Proba-V. To provide mechanical stability, low mass and compactness, a molded epoxy stack will hold both sensors and front-end electronics. In particular the following development will be done in each of the phases: Belgium GSTP G618-011EE QINETIQ SPACE NV 2015 - 2019 3D Energetic Electron Spectrometer Phases C and D Flight data analysis of TDP#8 radiation experiment on board Alphasat Under a previous ESA contracts a combined component technology demonstration and component radiation effects experiment in addition to a radiation environment instrument was designed, developed and manufactured. This equipment consists of a Component Technology Test Bed (CTTB) and the radiation monitoring instrument MFS. The first flight model, named Technology Demonstration Payload#8 (TDP#8), is currently flying on Alphasat since July 2013. The CTTB contains three radiation effects experiments. Portugal GSTP G617-146QE EFACEC 2015 - 2019 Flight data analysis of TDP#8 radiation experiment on board Alphasat Numerical Simulations for Spacecraft Catastrophic Disruption Analysis At present, the largest part of the catalogued space debris population consists of fragments originating from accidental explosions of spacecraft and upper stages, but it is expected that hypervelocity collisions involving large objects could become the primary source of new debris in the mid-term future. In this context, understanding the physical processes involved in spacecraft collisions is crucial, because these big impacts are one of the key drivers of the long-term evolution of the amount of space debris. Italy Discovery 15/716-a CISAS 2016 - 2019 Numerical Simulations for Spacecraft Catastrophic Disruption Analysis GreenSat Resulting from an ever increasing public pressure, the quest to be environmentally friendly is transforming the competitive landscape, as eco-friendly design results in a new frontier of innovation. As a public sector intergovernmental organisation, ESA is committed to prioritising environmental concerns in all its activities. Through its Clean Space initiative, the Agency is pioneering an eco-friendly approach to space activities. France Discovery 15/033-a Thales Alenia Space 2017 - 2019 GreenSat Environmental aspects of passive de-orbiting devices The technical objective of this study was to understand the net effect of using deorbiting technologies like sails or tethers over the future debris population around Earth. In principle, indeed, these attractive technologies will support the compliancy to post-mitigation disposal guidelines, for small missions. However, the increased cross section also increases the collision risk. Italy Discovery 15/095 Politechnico di Milano 2017 - 2018 Environmental aspects of passive de-orbiting devices Improvement of energetic solar heavy ion environment models Establish a reference ion data set and improve the Solar Energetic Particle Environment Modelling (SEPEM) model to include better prediction of ion composition and energy spectra, and transport across the geomagnetic field. This will include the ingestion of new data sets, the quality control and cleaning of the data (de-spiking, gap filling, saturation compensation, etc.), the interpolation to required energy values and augmentation with LET (Si, GaAs) values. United Kingdom TDE T704-302EE KALLISTO CONSULTANCY LTD 2012 - 2018 Improvement of energetic solar heavy ion environment models Game theoretic analysis of space debris removal dilemma The increase of space debris means that active space debris removal is becoming more relevant. An active debris removal mission would have a positive effect (or risk reduction) for all satellites in the same orbital band. This leads to a dilemma: each space agency has an incentive to delay its actions and wait for others to respond. We model this scenario as a non-cooperative game between self-interested agents in which the agents are space agencies. 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