467 results found Selected 0 items No itemsClear selection Select / deselect all results (all pages, 467 total) Application of surface functionalisation in space mechanisms Surface functionalisation (SF) by e.g. laser texturing, roughness modification, surface energy modification has been reported in the literature to be able to reduce coefficient of friction of steel contacts and reduce their wear by several orders of magnitude. Several universities and institutes in Europe have been developing methods of SF for application in tribology. United Kingdom TDE T715-604MS ESR TECHNOLOGY LTD 2020 - 2023 Application of surface functionalisation in space mechanisms Definition of process assessment and improvement approach for cybersecurity Security is becoming increasingly important in all of ESA's missions, rather than just in specific missions (Galileo, Copernicus) as was the case in the past. Therefore, the European space industry need to have a well-defined and standardized approach to assess the security processes of its suppliers, especially in terms of software development, where many security vulnerabilities can be introduced. Spain TDE T725-702QQ EVERIS SPAIN, SLU 2021 - 2023 Definition of process assessment and improvement approach for cybersecurity REACH obsolescence management for Materials Processes Increasing numbers of regulations in Europe (e.g. RoHS, REACH, CLP) are implemented targeting sustainable development, environmental impact and protection of human health. The most imminent implication is the possible obsolescence of qualified materials, processes and technologies, as manufacturers are forced to change materials compositions, alter manufacturing processes or take the decision to remove materials from the European market. Finland TDE T724-501QT REACHLAW OY (HEADQUARTERS) 2018 - 2023 REACH obsolescence management for Materials Processes Containment techniques to reduce spacecraft re-entry footprint Design for Demise is being applied in order to reduce the on-ground casualty risk. However, several parts of the spacecraft, due to performance requirements or long development cycles (e.g. Optical instruments, large mechanisms, etc.), may not be able to significantly change materials or design. During re-entry, each of these elements may generate several debris surviving re-entry increasing significantly the on-ground casualty risk. France TDE T711-604SY THALES ALENIA SPACE FRANCE 2020 - 2023 Containment techniques to reduce spacecraft re-entry footprint Feeder-link demonstration using Technology Demonstration Payload on Alphasat The technology demonstration payload (TDP#1) on the Alphasat GEO spacecraft is a coherent optical communication data relay demonstrator for optical inter-satellite links and Ka-band downlinks. It is a precursor development from the German Space Agency (DLR) for the European Data Relay System (EDRS), but not commercially utilized. It is therefore the ideal platform to test optical feeder-link technologies in a representative environment. Switzerland TDE T517-602MM SYNOPTA GMBH 2019 - 2023 Feeder-link demonstration using Technology Demonstration Payload on Alphasat Low distortion Thick disk amplifier at >400 mj Previously, a high power low optical distortion amplifier breadboard was developed and tested. It met all the performance requirements (similar to Aeolus booster amplifier), achieving 400+ mj at 100 Hz with an electrical to optical efficiency twice that of the Aeolus amplifier design. France TDE T117-603MM Cilas 2019 - 2023 Low distortion Thick disk amplifier at >400 mj Microwave heating of ISRU feedstock Microwave heating of regolith is a potential pathway to heat and achieve reaction temperatures in regolith. In this study different types of regolith analogs shall be heated by microwave energy and the process shall be optimized for power efficiency. Microwave heating is considered as an effective pathway to achieve necessary temperatures within the regolith for ISRU applications. Microwave heating of regolith has been studied on a basic level by NASA and is being applied in the mining industry on high value ores to enhance e.g. Italy TDE T314-607MM RINA CONSULTING SPA 2020 - 2023 Microwave heating of ISRU feedstock SpaceWire Network Management Service Suite Definition and Validation SpaceWire has become a de facto standard for payload systems (including for Command & Control) and its Real-Time derivatives are now being considered for avionics. The capability provided by SpaceWire to develop data handling systems based on high-speed networks allows much greater performance but implies implementing communication bus management techniques specific to SpaceWire. As network management is not part of the basic SpaceWire protocol ECSS-E-ST-50-12C (Rev.1), it must be provided to industry in the form of an additional standard. Greece TDE T701-501ED TELETEL SA 2020 - 2023 SpaceWire Network Management Service Suite Definition and Validation 120 W, 32 GHZ TWT for payload data transmitter New scientific missions require Ka-Band high power sources for the data return. Limitation on maximum antenna size and minimum required data rate can be overcome by increasing the transmitted power. At present, there is no off the shelf TWT(A) in the allocated frequency band (31800-32300 MHz) in Europe with 120W saturated output power. France TDE T206-015ES THALES AVS FRANCE SAS 2020 - 2023 120 W, 32 GHZ TWT for payload data transmitter Photon-Counting Ground-based Optical Communications Detector Future missions are currently being proposed / designed with existing (or moderately inproved) Space-to-Earth communication capabilities in mind. Optical communications technology offers the potential of a dramatic increase in data-rates, specifically in the down-link of science data, thereby allowing for a substantial increase in science return.Direct detection technology using pulse position modulation (PPM) is regarded as the preferred solution for "deep space" optical links. 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