223 results found Selected 0 items No itemsClear selection Select / deselect all results (all pages, 223 total) Miniaturised distributed optical fibre sensors (DOFS) based on photonic integrated circuits (PICs) for space applications Distributed optical fibre sensors (DOFS) are highly suitable for monitoring temperature, vibration and strain using physical principles such as Raman, Rayleigh and Brillouin backscatter. They convert a standard telecom infrastructure to a sensor network providing thousands of virtual sensors per km using the intrinsic light/glass interaction during propagation. United Kingdom Discovery ETD 2020-03-b Worthy Photonics 2020 - 2023 Miniaturised distributed optical fibre sensors (DOFS) based on photonic integrated circuits (PICs) for space applications Development of high-accuracy millimeterwave components through lithography metal manufacturing The objectives of the DONE3D activities are the implementation of a novel additive manufacturing supply chain that is based on the through Lithography Metal Manufacturing (LMM) technology, and to assess its applicability to the development of RF components for SatCom and EO applications, such as multi-beam antennas. Germany Discovery ETD 2020-08-a Fraunhofer Gesellschaft 2021 - 2023 Development of high-accuracy millimeterwave components through lithography metal manufacturing Power sail disruptive PV power array technology to enable economic viability of SPS The goal of the Powersail project is to demonstrate the potential of amorphous silicon (a-Si) deposited on ultralight space-grade polyimide for solar power satellites (SPS). State of the art solutions are III-V compound semiconductor triple junction-based PV modules, which are 100 times too expensive and one order of magnitude too heavy to build a competitive SPS with terrestrial microwave energy collection infrastructure. Switzerland Discovery 21-D-T-TEC-01-a CSEM SA. Centre Suisse dElectronique et de Microtechnique SA 2021 - 2023 Power sail disruptive PV power array technology to enable economic viability of SPS Development of a Flexible Thermal Protection System for Deployable Inflatable Heatshields and Hypersonic Decelerators Deployable and inflatable heatshield concepts have a very high potential to extend European capabilities for future Martian lander missions. Such concepts would allow to approach landing zones in the Martian highlands which cannot be reached with current state-of-the-art entry, descent and landing (EDL) technology, mainly due to the very low density of the Martian atmosphere. Alternatively, a deployable or inflatable heatshield concept could allow for an increased landed mass in the Martian lowlands. ; ; United Kingdom TDE T721-615MT VORTICITY LTD 2020 - 2023 Development of a Flexible Thermal Protection System for Deployable Inflatable Heatshields and Hypersonic Decelerators Evaluation of heatshield CFRP and bonding materials to increased temperature limits OOne important constraint in the sizing process of an ablative TPS for atmospheric entry vehicles is the temperature limit of the supporting heatshield structure and of the bonding material used to attach the TPS. This temperature limit is typically in the range of 150-180degC. For the CFRP the limiting factor is typically the resin. New resin materials (like cyanate ester or bismaleimide) have commercially become available in recent years and relevant CFRP materials been qualified towards higher temperature limits for other space applications (like solar arrays or antenna reflectors). Spain TDE T924-004MT ACONDICIONAMIENTO TARRASENSE ASSOCI 2018 - 2023 Evaluation of heatshield CFRP and bonding materials to increased temperature limits Delaminations in plastic package:Evolution under constraints The various players in the space sector activities (equipment manufacturers, operators, and space agencies) believe that the future belongs to industrial components. Industrial components (such as Automotive-quality and commercial-quality components) have already been selected and used for launcher-type or short duration satellite missions. Metallographic cross sections made on plastic packages industrial components, in the frame of these programs, revealed delamination between the chip and the encapsulation resin. Belgium Discovery 20-D-S-TEC-05-b Thales Alenia Space 2021 - 2023 Delaminations in plastic package:Evolution under constraints Metallic Glasses for High Performance Mechanism Applications on Long Term Missions Metallic Glasses (MG) are a class of alloys which retain an amorphous structure in the solid state, when cooled from the liquid state. Formation of a fully amorphous structure for large cross sections (up to > 1 cm) is now possible for several alloying systems referred to as Bulk Metallic Glasses (e.g. Fe-base, Ti-base, Al-base, Mg-base, Ca-base, Zr-base). Ireland TDE T524-503QT UNIVERSITY COLLEGE DUBLIN 2018 - 2023 Metallic Glasses for High Performance Mechanism Applications on Long Term Missions Metallic Glasses for High Performance Mechanism Applications on Long Term Missions Metallic Glasses (MG) are a class of alloys which retain an amorphous structure in the solid state, when cooled from the liquid state. Formation of a fully amorphous structure for large cross sections (up to > 1 cm) is now possible for several alloying systems referred to as Bulk Metallic Glasses (e.g. Fe-base, Ti-base, Al-base, Mg-base, Ca-base, Zr-base). Austria TDE T524-503QT RHP-TECHNOLOGY GMBH 2018 - 2023 Metallic Glasses for High Performance Mechanism Applications on Long Term Missions De-risk assessment: RESTORE - RidEshare STructure fOr micRo-launchEr Germany GSTP G617-241TAjk SPACE STRUCTURES GMBH 2022 - 2023 De-risk assessment: RESTORE - RidEshare STructure fOr micRo-launchEr Damping behaviour in AM material based parts Vibration is one of the main issues when it comes to the design of space hardware and as such, it should be considered in the early phases of spacecraft design. When this factor is overlooked, a later identification of vibration and shock issues causes a deep impact on the performance of the spacecraft. Often the only solutions available, such as a dedicated damper, are detrimental for design, cost and schedule of the mission. ; Germany GSTP GT1A-007MS SPACE STRUCTURES GMBH 2020 - 2023 Damping behaviour in AM material based parts Pagination « First First page ‹‹ Previous page … 3 4 5 6 7 8 9 10 11 … ›› Next page Last » Last page Filter by Programme GSTP (105) TDE (75) Discovery (40) Preparation (3) Filter by Start Year 2018 (34) 2021 (33) 2020 (31) 2019 (21) 2015 (20) 2016 (20) 2022 (19) 2017 (17) 2014 (13) 2023 (6) 2012 (4) 2013 (3) 2011 (1) 2024 (1) Filter by End Year 2023 (61) 2021 (31) 2019 (26) 2020 (24) 2024 (23) 2022 (21) 2018 (14) 2017 (8) 2025 (6) 2016 (4) 2015 (3) 2014 (2) Filter by Keywords 38-Advanced Manufacturing (20) 32-Clean Space (10) Additive Manufacturing (9) ISRU (6) 2-Space Segment - Platform (4) 3-Platforms / Others (4) 3d printing (4) 32-Cleanspace (4) Off-Earth manufacturing (4) Regolith (4) 24-Materials and Processes (3) aerocapture (3) lunar base (3) Materials (3) Re-entry (3) 9-Technologies applicable to several Cosmic Vision Missions (2) 15-Mechanisms (2) 20-Structures & Pyrotechnics (2) 21-Thermal (2) 36-Collaborative Activities (2) aerobreaking (2) ALM (2) Ariadna (2) athmospheric drag (2) Biomimetics (2) Biomimicry (2) inflatable (2) LCA (2) Mars (2) Moon (2) moon village (2) Orbital capture (2) Orbit insertion (2) 0-Telecommunications Technologies (1) 1-Launchers (1) 1-Phootprint (1) 2-Athena (1) 2-Human Space Flight Oriented Technologies (1) 2-Space Segment (1) 3-Human Spaceflight and Exploration Preparation (1) 3-In-Situ Resource Utilisation (ISRU) (1) 3-Space Segment - Payload (1) 3D printer (1) 6-EnVision (1) 6-Robotics (1) 8-System Design & Verification (1) 9-Opportunity (1) 14-Life & Physical Sciences (1) 15-Mechanisms & Tribology (1) 20-Structures (1) 27-End to End System Design Processes (1) 33-Space & Energy (1) 35-Technologies Enabling Breakthroughs in Science (1) 46-HERA (1) 48-Cybersecurity (1) 99-Others (1) active debris removal (1) active optics (1) ADM (1) aerobraking (1) amorphous silicon (1) Antenna (1) Antifungal (1) Antimicrobial (1) atmospheric impact (1) basalt (1) Below Freezing Water Storage (1) bio-inspired (1) Boom (1) Carbon Fiber (1) CDF (1) CFRFE (1) CleanSat (1) CleanSpace (1) coating (1) Code (1) concurrent engineering (1) Cryocooling (1) DART (1) decelerator device (1) Distributed optical fibre sensors (1) DOFS (1) Energy Storage (1) flexible coating (1) flexible OSR (1) functionally graded materials (1) geopolymer (1) Habitats (1) HAPS (1) HERA (1) Human spaceflight (1) Impact (1) in-space manufacturing (1) inflatable structure (1) interplanetary transfer (1) iSALE (1) laser powder bed fusion (1) LCM (1) LISA Pathfinder (1) Lithography Metal Manufacturing (1) LMM (1) Lunar (1) lunar caves (1) lunar habitat (1) Lunar power (1) Lunar Surface (1) Lunar Water Storage (1) magnetic materials (1) magnetic shuttle pump (1) manufacture (1) Manufacturing (1) Mechanical Pumping Loop (1) mechanisms (1) Mission architecture (1) Modelling (1) Moon base (1) MPL (1) MSP (1) on-orbit manufacturing (1) Optical Systems (1) Optics (1) OSR (1) photonic integrated circuits (1) PICS (1) Power (1) radiator (1) REACH (1) recycle (1) recycling (1) refurbish (1) Regolith printing (1) reinforced (1) Robotics (1) SBSP (1) Selective laser melting (1) self-growing (1) shock physics (1) Simulation (1) smart OSR (1) solaris (1) space-grade polyimide (1) spacecraft demise (1) Space debris (1) space debris mitigation (1) SPH (1) SPS (1) Sustainability (1) Swarm (1) Telescope (1) thermite (1) thermo-optical (1) Thermodynamics (1) topological optimization (1) UAV (1) Filter by Contractor Fraunhofer Gesellschaft (7) THALES ALENIA SPACE FRANCE (6) HPS GMBH (5) OHB System AG (5) TWI LIMITED - THE WELDING INSTITUTE (5) CSEM SA. 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