415 results found Selected 0 items No itemsClear selection Select / deselect all results (all pages, 415 total) Chemical Compatibility and Wettability of various Materials with various Working Fluids for Two-Phase and Heat Pump Systems Material compatibility with ammonia is critical for the performance and lifetime of Two-Phase equipment. The generation of non-condensable gases can severally impact the performance of the two-phase equipment. Material compatibility testing is mandatory in all the development of two-phase equipment which uses new materials. However, the compatibility results are not publish and it remains at the manufacturer, hence it cannot be used by another manufacturer. Ireland TDE T521-601MT University of Limerick 2020 - 2023 Chemical Compatibility and Wettability of various Materials with various Working Fluids for Two-Phase and Heat Pump Systems Overlapped subarray fed reflector antennas for SAR instrument Several SAR future Earth Observation missions requires large reflector antennas generating highly directive overlapped beams. This has been done so far with high power waveguide Beam Forming Networks including ferrite switches as implemented for Core H2O pre-developments. In this activity, it is proposed to investigate reflector antennas fed by overlapped subarrays. This represents an extremely promising concept for on-board SAR instruments. Spain TDE T107-503EE AIRBUS DEFENCE AND SPACE S.A.U. 2019 - 2023 Overlapped subarray fed reflector antennas for SAR instrument High power (80 kW) X-band Uplink for DS Missions - Development of critical waveguide components Present ESA Deep Space Stations are equipped with a 20 kW X-Band High Power Amplifier (HPA). Switzerland TDE T212-059GS MIRAD MICROWAVE AG 2019 - 2023 High power (80 kW) X-band Uplink for DS Missions - Development of critical waveguide components Ionosphere impact and corrections for low frequency radars The use of low microwave frequencies for radars is key.: It enables radar signals from sub-surface sounders to penetrate deep under the Earth surface, it allows minimised temporal decorrelation in Synthetic Aperture Radars observations (e.g L-band SAR) and to generate high quality interferometric products, it opens up the bistatic use of signals of opportunity due to the presence of L-band navigation signals. However these VHF to L-band signals are highly sensitive to the state of the ionosphere which can create strong perturbations, or even block the signal. France TDE T107-605EF ONERA 2020 - 2023 Ionosphere impact and corrections for low frequency radars One Operation Data Systems Infrastructure for all ESA space assets There are a number of robotic missions in the definition phase at present, targeting the Moon and Mars, in orbit servicing, active debris removal and Lunar outpost . These mission scenarios require a new set of capabilities related to distributed, multi-asset mission operation concepts. Germany TDE T709-604GD TERMA GMBH 2021 - 2023 One Operation Data Systems Infrastructure for all ESA space assets Estimation of proton induced single event rate in very deep submicron technologies More and more space applications and missions are considering the use of deep submicron technologies. Digital CMOS technologies below 65nm are sensitive to proton induced Single Event Effects (SEE) by direct ionisation mechanism. The consequence is a significant increase of SEE rates in flight (up to several orders of magnitude). This effect will be the dominant cause of SEE in orbit for these technologies. This poses a very significant challenge to SEE mitigation methods used in spacecraft electronics. France TDE T723-605QE ALTER TECHNOLOGY TUV NORD FRANCE SAS 2020 - 2023 Estimation of proton induced single event rate in very deep submicron technologies Estimation of proton induced single event rate in very deep submicron technologies More and more space applications and missions are considering the use of deep submicron technologies. Digital CMOS technologies below 65nm are sensitive to proton induced Single Event Effects (SEE) by direct ionisation mechanism. The consequence is a significant increase of SEE rates in flight (up to several orders of magnitude). This effect will be the dominant cause of SEE in orbit for these technologies. This poses a very significant challenge to SEE mitigation methods used in spacecraft electronics. France TDE T723-605QE IROC TECHNOLOGIES SA 2020 - 2023 Estimation of proton induced single event rate in very deep submicron technologies Materials Selection for Surface EVA Suit development This work begins the material selection process for EVA suits based on initial inputs from the EAC team that is developing an ergonomic prototype space suit. France TDE T324-504QT COMEX 2018 - 2023 Materials Selection for Surface EVA Suit development Dust removal and cleaning of optical surfaces and seals in lunar environments The lunar environment has a challenging dust environment. The dust is highly abrasive and therefore can cause considerable damage in short time. For astronauts, the dust effects range from highly irritating to toxic. Many sample processing and sample analysis systems need reliable seals; spaceflight hardware must work reliably in the presence of dust. France TDE T314-602MM COMAT 2020 - 2023 Dust removal and cleaning of optical surfaces and seals in lunar environments Test methodology investigations and parameters influencing Passive InterModulation (PIM) interference Passive intermodulation is a real threat to all types of payloads. In some cases, it could even lead to total lost of the spaceship. Despite of this, there is very weak understanding of the parameters that generate this unwanted interference as well as their influence in the amplitude of the interfering signal. In addition, there is a total lack of agreed testing techniques, procedures and methodologies as well as justified test margins, as has already been recently stated by the European community (National Delegations, satellite operators and Eurospace). 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