415 results found Selected 0 items No itemsClear selection Select / deselect all results (all pages, 415 total) Advanced glass cell technology for extended GNSS atomic clocks lifetime Glass cells are typically used in Frequency Standard, both as reference cell, in the lamps for atomic pumping and as dissociator bulbs.When used in a lamp (RAFS or Mercury ion trap), the cell must be sufficiently resilient for avoiding limitations in the lifetime due to diffusion of material (i.e. Rubidium or Mercury) inside the bulb walls, given the combination of dissociation mechanisms and high temperatures. Switzerland TDE T606-502ET OROLIA SWITZERLAND SA 2018 - 2021 Advanced glass cell technology for extended GNSS atomic clocks lifetime Trade-off for very large space telescope mirrors Currently the size limit for primary mirrors of large telescopes is - due to the available Ariane-5 fairing - typically at 3.5m (Herschel). Future science (and most likely also Earth observation missions) will call for larger telescope sizes due to more demanding requirements on the light collecting efficiency and angular resolution. France TDE T716-403MM AIRBUS DEFENCE AND SPACE SAS 2018 - 2021 Trade-off for very large space telescope mirrors Development of Friction Welding Processes to Add External features to Spacecraft and Launchers Systems During the manufacturing of large structures such as launch vehicles, spacecraft, and propellant storage systems, it is often necessary to add external features such as brackets during the manufacturing process. Depending on the material used for the structure, features such as brackets can be attached using traditional techniques such as TIG welding. However during conventional fusion welding, there is always a danger that distortion can occur, or that the poor weldability of the material can result in a significant loss in mechanical performance or weld integrity. United Kingdom TDE T724-404QT TWI LIMITED - THE WELDING INSTITUTE 2016 - 2021 Development of Friction Welding Processes to Add External features to Spacecraft and Launchers Systems New electrical contact materials selection and assessment for sliding electrical transfer applications Electrical contact materials used today for sliding electrical transfer applications have been developed in the 60/70th and are procuredfrom USA.It is believed that the latest manufacturing capabilities available in Europe are able to manufacture some new class of sliding contact material alloys. This activity propose to test the most promising European materials developed for sliding electrical contact applications. Austria TDE T715-402MS AEROSPACE AND ADVANCED COMPOSITES GMBH - AAC 2015 - 2021 New electrical contact materials selection and assessment for sliding electrical transfer applications Impact of anomalies and non-conformances on future requirement formulations A systematic implementation of lessons learned for the definition and specification of projects is currently missing and relying on availability of experienced engineers in the early design phases. This jeopardizes the possibility to prevent production delays generated by specific requirements and design solutions adopted in the early project phases. Spain TDE T708-606MX GMV SOLUCIONES GLOBALES INTERNET SA 2019 - 2021 Impact of anomalies and non-conformances on future requirement formulations Utilisation of a Heavy and Light Ion Facility at UCL for Component Radiation Studies This activity concerns execution of regular irradiation test campaigns on EEE components for flight on ESA and European space missions. Up to 360 hours per year of beam time is available free of charge on a priority basis for ESA. Additionally, a minimum of 500 hours per year is available for ESA sub-contractors, research institutes and other interested users at preferential hourly rates. The agency provides the facility with a detailed work programme of the test campaigns. Subsequently, the facility performs test campaign scheduling (in agreement with the Agency). Belgium TDE T723-F09QE Universite catholique de Louvain 2018 - 2021 Utilisation of a Heavy and Light Ion Facility at UCL for Component Radiation Studies Water propulsion system Current chemical propulsion systems rely on the hypergolic reaction of dangerous, corrosive and toxic chemicals. The selection of these chemicals was driven by a range of needs including performance, storability and reliability. They have also driven up the sub-system design justification cost. Current ''green'' propulsion options can offer some mitigation of these issues however most alternatives are not benign chemicals and continue to have safety and cost concerns. Electrolysis (ECLSS heritage) technology in Europe is at a high TRL. Germany TDE T519-413MP OMNIDEA-RTG GMBH 2016 - 2021 Water propulsion system Environmentally friendly corrosion protective hybrid coating as substitute of chromium based conversion coatings for space applications IRUCOAT is an eco-friendly hybrid sol-gel coating based on SiO2-Zr02-organic epoxy interconnected network, developed by TECNALIA and already tested for corrosion protection and other performance requirements applicable to the aerospace sector. Spain TDE B02017085 FUNDACION TECNALIA RESEARCH & INNOVATION 2018 - 2021 Environmentally friendly corrosion protective hybrid coating as substitute of chromium based conversion coatings for space applications Development of a high performance microvibration isolation system Typical isolation systems currently used are limited to passive isolators, based on viscoelastic elements. Other passive existing technologies include eddy-current dampers, the so-called D-struts and shunted piezo electric transducers. Active systems include voicecoil and piezo actuators and active eddy current dampers. This proposal is prompted by recent developments in the frame of TEC Technology Assessment supported work on electromagnetic shunt dampers connected to a negative resistance circuit showing promising performances. United Kingdom TDE T215-011MS UNIVERSITY OF SURREY 2018 - 2021 Development of a high performance microvibration isolation system Magnetically Clean Reaction Wheel Reaction wheels exhibit dominant magnetic field emissions that shall be reduced to allow the reaction wheel use on magnetically susceptible missions without negative impact on scientific objectives. Conventional reaction wheels use brushless DC motors with relatively high magnetic flux densities in large air gaps without any dedicated compensation or 'magnetic balancing' of the motor magnets. The motor external magnetic field together with contributions from further components, (ball bearings), combine to a significant magnetic dipole moment. 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