467 results found Selected 0 items No itemsClear selection Select / deselect all results (all pages, 467 total) Technology to quantify and qualify microbial contamination on surfaces Microbial contamination is a generic risk concerning flight hardware degradation, Planetary Protection and potentially crew health. Material surface requires a proper control and monitoring of the microbial cleanliness level. Today, contact plates, swabs and wipes are used for surface sampling. Swabs and wipes samples include mandatory liquid transfer to further extract and detect microorganism. Today, automated miniaturized system, molecular-based, has been developed and offers the possibility to perform multiple laboratory functions on a complete integrated system (i.e. Spain TDE T722-501MM SENER AEROESPACIAL, S.A. 2019 - 2023 Technology to quantify and qualify microbial contamination on surfaces Artificial Intelligence techniques for GNC design, implementation and verification The performance of currently available Guidance Navigation and Control (GNC) systems for space is limited by unmodelled effects or uncertain parameters (e.g. sensor/actuator performances and performance degradations). Artificial Intelligence (AI) techniques based on machine learning could be integrated in GNC systems in order to enable on-line learning of the properties of dynamics, environment, sensors and actuators that limit the available performances. Spain TDE T705-605SA SENER AEROESPACIAL, S.A. 2020 - 2023 Artificial Intelligence techniques for GNC design, implementation and verification Optical fibre-based ignition technology for launcher RCS Current launcher RCS thrusters operate with storable, hypergolic propellants. They do not need an ignition system, but these propellants have a negative environmental impact and, due to the high and therefore expensive effort for safe handling and fuelling of the tanks, alternatives have to be found to replace them. One alternative is the use of cryogenic propellants available in the launcher for the RCS thrusters, or storable green propellants for thrusters on long-duration missions, combined with a laser ignition system. Germany TDE T419-606MP DLR - German Aerospace Center 2019 - 2023 Optical fibre-based ignition technology for launcher RCS Verification and Validation of Autonomous Systems Contrary to a traditional system, in which input A should provide expected results B, an adaptive and evolving system needs different acceptance criteria. Besides this, the traditional process for doing the verification and validation is not sufficient anymore and needs rethinking. For example; it might no longer be possible to run-through all the possible test-scenarios before launch. Germany TDE T708-608SW Solenix Engineering GmbH 2021 - 2023 Verification and Validation of Autonomous Systems Re-usable concepts for space transportation flight vehicle engineering A reusable space transportation system is a space system intended to allow for recovery of all or part of the system for later reuse. The term ?reusable space transportation vehicle? refers to several different levels of reuse ranging from the entire vehicle to only parts of it. Reusable space transportation systems present the opportunity to reduce the cost of transportation and to provide capabilities that are not available right now. Germany TDE T418-601MP DLR - German Aerospace Center 2019 - 2023 Re-usable concepts for space transportation flight vehicle engineering Innovative scalable large deployable antenna reflectors Despite different attempts performed in the past two decades, Europe is lacking a competitive product for a large reflector with the requested TRL level to embark on a commercial program. Need is identified to cover antenna applications from 4 up to 18 meter and for frequencies from UHF up to Ka band.. American companies are leaders in this domain and are commercially dominating the worldwide market. Italy TDE T515-301MS THALES ALENIA SPACE ITALIA SPA 2012 - 2023 Innovative scalable large deployable antenna reflectors Deep Learning for Space The activity foresee the assessment of several different deep learning architectures and deep learning algorithms. Initial use cases, for evaluation, will be selected from Operations and AIT data, supporting tasks such as spacecraft performance assessment, diagnostics and forecasting. Germany TDE T708-609OS Solenix Engineering GmbH 2021 - 2023 Deep Learning for Space Aerothermodynamics Tools for System Integration Assembly, Integration, and Testing (AIT) processes occur during the phases C and D of the engineering processes of a given flight vehicle. System integration processes take place at the level of engineering models, structural and thermal models, and qualification models of flight vehicles.The current ATD tools cover the phases 0, A, and part of the phase B (B1) for design, and development of flight vehicles. Beyond those phases, the current toolset is not able to cover tasks of system integration and testing (phases C, D). Spain TDE T718-702MP DEIMOS ENGINEERING AND SYSTEMS SLU 2021 - 2023 Aerothermodynamics Tools for System Integration Cost efficient indoor positioning with sparse local infrastructure Indoor positioning technologies are primarily driven by 2 sets of use cases (e.g. 5G positioning use cases of 3GPP-standardization body for 3G, 4G and 5G): - Very high accuracy (<1m) in bounded service areas (e.g. Industry automation). - Coarse accuracy (<10m) with quasi-ubiquitous coverage (e.g. To support emergency call and ehealth, as identified in 3GPP TR22.872 and by firstnet, the authority managing first responders network in the USA, asset tracking for instance on factory floors). Ireland TDE T606-610ES Danalto Limited 2021 - 2023 Cost efficient indoor positioning with sparse local infrastructure 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 Pagination « First First page ‹‹ Previous page … 13 14 15 16 17 18 19 20 21 … ›› Next page Last » Last page Filter by Programme GSTP (2) (-) TDE (467) Filter by Start Year 2020 (75) 2021 (63) 2019 (61) 2018 (52) 2016 (37) 2022 (34) 2015 (32) 2017 (26) 2014 (19) 2012 (18) 2013 (18) 2023 (10) 2011 (7) 2009 (5) 2010 (5) 2008 (2) 2024 (2) 2006 (1) Filter by End Year 2023 (122) 2024 (84) 2021 (44) 2022 (44) 2019 (36) 2018 (35) 2020 (27) 2025 (21) 2017 (18) 2014 (11) 2015 (11) 2016 (5) 2013 (4) 2011 (2) 2012 (2) 2010 (1) Filter by Keywords 1-Microwave Payloads (19) 9-Technologies applicable to several Cosmic Vision Missions (14) 3-Platforms / Others (12) 0-Navigation (11) 0-Navigation Technologies (10) 26-Spacecraft Avionic System (10) 32-Clean Space (10) 1-Launchers (9) 2-Optical Payloads (8) 3-Space Segment - Payload (8) 36-Collaborative Activities (8) 5-Space System Control (7) 1-On-board Data Systems (6) 2-Space Segment - Platform (6) 19-Propulsion (6) 28-Electronic Components (6) 35-Technologies Enabling Breakthroughs in Science (6) 0-Telecommunications Technologies (5) 2-Space System Software (5) 4-Users (5) 6-EnVision (5) 15-Technologies applicable to several Cosmic Vision Missions (5) 16-Optics (5) 30-Deep Sub Micron Development (5) 32-Cleanspace (5) 38-Advanced Manufacturing (5) 40-Design to Produce (5) 1-Systems (4) 2-Contamination and Radiation (4) 3-Habitation (4) 3-User Segment Technology (4) 4-Ground Segment (4) 6-Robotics (4) 0-Telecommunications (3) 1-Avionics and Processing (3) 2-Ground segment and operations (3) 2-Space Segment (3) 3-In-Situ Resource Utilisation (ISRU) (3) 4-Spacecraft Environment & Effects (3) 10-Flight Dynamics and GNSS (3) 24-Materials and Processes (3) 1-Phootprint (2) 1-Robotic Assistance (2) 2-Athena (2) 2-Ground Segment Technology (2) 2-Life and Physical Sciences (2) 3-Human Spaceflight and Exploration Preparation (2) 3-Spacecraft Electrical Power (2) 3-Spacecraft Power (2) 4-Life Support and Medical (2) 4-Spacecraft Environments and Effects (2) 4-System Tools (2) 6-RF Systems, Payloads and Technologies (2) 6-Sample acquisition, analysis, handling and return (2) 7-Electromagnetic Technologies and Techniques (2) 7-Sensing & Positioning (2) 8-System Design & Verification (2) 9-Opportunity (2) 14-Life & Physical Sciences (2) 15-Mechanisms (2) 17-Optoelectronics (2) 20-Structures & Pyrotechnics (2) 21-Thermal (2) 31-Miniaturisation (2) 33-Space and Energy (2) 37-Exploration Technology (2) 1-L-Mission Candidate: JUICE (1) 1-Onboard Data Systems (1) 1-Space Segment Technology (1) 1-System (1) 2-Human Space Flight Oriented Technologies (1) 2-New Space Transportation Services (1) 2-Novel Energy Systems (1) 3-Ground Segment (1) 3-LISA (1) 3-Technologies for Horizon 2030 (1) 5-Disruptive Concepts on Positioning, Navigation and Timing (1) 5-Propulsion & Landing (1) 6-RF Payload and Systems (1) 6-RF Payload Systems (1) 9-Mission Operation and Ground Data Systems (1) 10-Communications & Navigation (1) 11-Space Debris (1) 11-Subsurface sampling/deep drilling (1) 12-Guidance Navigation and Control (1) 12-MSR (1) 15-Mechanisms & Tribology (1) 16-Mission Operations Data Systems (1) 18-Aerothermodynamics (1) 18-Artificial Intelligence (1) 20-Structures (1) 22-Environmental Control & Life Support (ECLS) and In Situ Resource Utilisation (ISRU) (1) 25-Quality, Dependability and Safety (1) 27-End to End System Design Processes (1) 33-Space & Energy (1) Antifungal (1) Antimicrobial (1) AOCS (1) Augmented Reality (1) Closed loop (1) Combustion (1) concurrent engineering (1) Developments (1) Doh (1) Doherty Power Amplifier (1) Fuel cell (1) Gyroscope (1) Habitats (1) High Performance (1) HT-PEM (1) Human spaceflight (1) Interference Detection (1) Ka-band (1) Latch Valve (1) LOX/H2 (1) Mission (1) Performance (1) Propulsion (1) Receivers (1) Regenerative (1) Safe Mode (1) Satellite (1) Science (1) Signals (1) Simulation (1) Star Tracker (1) Filter by Contractor GMV AEROSPACE AND DEFENCE, SA (25) THALES ALENIA SPACE FRANCE (19) DLR - German Aerospace Center (9) SENER AEROESPACIAL, S.A. 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