415 results found Selected 0 items No itemsClear selection Select / deselect all results (all pages, 415 total) Dynamic Latchup protection chip for COTS components The use of Commercial Off the Shelf (COTS) components is and will always be an option to achieve space system performances that cannot be achieved with available space qualified components. For such components that are not latchup proof by design the use of protection circuitry is essential. Belgium TDE T701-316ED NSILITION sprl 2015 - 2024 Dynamic Latchup protection chip for COTS components Quality Assessment of the new European Ultra BRAVE FPGA Software Tools (Queens3) FPGA are increasingly being used to implement complex and critical functions on-board satellites at both platform and payload level, for a diverse range of applications, including: micro-controller processors, data compression, image data processing and others. ;;The qualification of these programmed devices for use in space is based on an exhaustive Verification and Validation process that attempts to exercise a large set of Test Vectors to ensure that the device functionality, error handling and performance are correct. Spain TDE T725-705QQ GMV AEROSPACE AND DEFENCE, SA 2021 - 2024 Quality Assessment of the new European Ultra BRAVE FPGA Software Tools (Queens3) AI aided AR/VR applications and VR aided ML A number of AR/VR projects have been implemented so far within ESA. The main focus has been on the application of AR/VR/MR to human and robotic operations as well as teleoperations/ maintenance tasks and lately on Space Safety use cases. With an increasing volume of information being represented on AR/VR/MR applications, especially for use cases involving visualisation of large datasets (e.g. scientific data) and Big Data, choosing the right approach is critical to meet performance limitations and offer an intriguing experience with greater fidelity without overwhelming the user. United Kingdom TDE T709-706GD NOTTINGHAM SCIENTIFIC LTD 2022 - 2024 AI aided AR/VR applications and VR aided ML Test mass charging toolkit and LPF lessons learned One of the key disturbances to the test masses in space gravitational wave detectors and other free-fall experiments is the electrostatic charge induced in them through interactions with penetrating charged particles and their secondaries. The masses are normally behind heavy shielding and as charged particles penetrate, they slow, scatter and create a range of secondary particles through a variety of physical processes. As a consequence, the accurate tallying of the net charge is a complex and difficult problem. Italy TDE T204-125EP OHB Italia S.p.A. 2020 - 2024 Test mass charging toolkit and LPF lessons learned Conformal Antenna Array for Next Generation Launchers The telemetry (TM) system of a launch vehicle (LV) builds a communication link between a launch vehicle and a ground station (GS). It transfers the monitoring information to a ground station where the information could be (1) status of a launch vehicle resources, attitude and health and (2) scientific data, image or video. The purpose of the telemetry is provide reliable information on the status of the entire launch vehicle to a ground station. United Kingdom TDE T407-601EF Queen's University of Belfast 2020 - 2024 Conformal Antenna Array for Next Generation Launchers Spectrographic response of break-up fragments to the re-entry environment The few spectroscopic re-entry break-up observation campaigns which have taken place focused on data collection for meteoroids and space systems equipped with thermal protection shields. Those techniques perform well within their intended scope, but are not fully suited for analysing the re-entry of general artificial objects. ESA supported such data collection on ATV-1, Cygnus-OA6, and WT1190F via these methods but interpretation has been difficult. United Kingdom TDE T711-602SD FLUID GRAVITY ENGINEERING LTD 2020 - 2024 Spectrographic response of break-up fragments to the re-entry environment Model-Based Engineering Hub Space Projects suffer from cumbersome and poor information sharing among disciplines, lifecycle phases and supply chain partners. This causes inefficiencies, costly mistakes and slippages of schedule. Interoperability among heterogeneous models is needed. The need is to inject the acquired knowledge into a sustainable quot;hubquot;-like eco-system, enabling reliable sharing and analysis capabilities for all engineering information needed by multiple stakeholders. This activity encompasses the following tasks: Netherlands TDE T708-604SY RHEA SYSTEM B.V. 2019 - 2024 Model-Based Engineering Hub Very high data rate receiver for the Earth-Space link in the 22 GHz frequency for future moon exploration missions Future Moon exploration missions require very high data rates, in particular for the uplink, that are not supported by the current state-of-art on-board technology.This activity focuses on the design of a receiver capable of handling very high data rates and low SNR (Signal-to-Noise Ratio) values, making novel use of the 22GHz for TTC (Telemetry, Tracking Command) uplink.The activity encompasses the following tasks:1 - Consolidation of the high level requirements of a lunar communications architecture for the Earth-Space link 2 - Design the overall on-board receiver architecture based on th Germany TDE T306-501ET TESAT-SPACECOM GMBH & CO.KG 2019 - 2024 Very high data rate receiver for the Earth-Space link in the 22 GHz frequency for future moon exploration missions camera-STabilisation to Enhance Autonomous Driving Yield (STEADY) The limit of autonomous locomotion velocity of a rover is dictated by actuator speed, terrain perception and planning. The actuator speed limit can be overcome by simple sizing of the actuator, depending on the mission needs. The planning limit for a traversable path can be improved by CPU (Central Processing Unit) and FPGA (Field Programmable Gate Arrays) computing acceleration. Switzerland TDE T313-701MM ALMATECH SA 2022 - 2024 camera-STabilisation to Enhance Autonomous Driving Yield (STEADY) Additive Manufacturing for Frequency and polarization Selective Surfaces Science TTC systems, Earth observation instruments and Telecommunication system payloads are more and more calling for multi-frequency reflector-based high gain antennas. As examples, one may refer to altimeters, radiometers and SAR (e.g. COREH2O) for Earth Observation and high-gain data transmission antennas as for the JUICE mission requiring both X- and Ka-band frequencies. Multi-frequency and multi-polarisation operation is often required hence the need for Frequency/polarization Selective Surfaces(FSS) integrated with (sub)reflectors or partially reflective surface. Spain TDE T707-502EE SENER TAFS, S.A.U. 2019 - 2024 Additive Manufacturing for Frequency and polarization Selective Surfaces Pagination « First First page ‹‹ Previous page … 4 5 6 7 8 9 10 11 12 … ›› Next page Last » Last page Filter by Programme GSTP (1) (-) TDE (415) Filter by Start Year 2020 (58) 2019 (53) 2021 (53) 2018 (45) 2016 (35) 2015 (31) 2022 (31) 2017 (26) 2014 (19) 2012 (18) 2013 (18) 2011 (7) 2023 (7) 2009 (5) 2010 (5) 2008 (2) 2006 (1) 2024 (1) Filter by End Year 2023 (103) 2024 (74) 2021 (36) 2018 (34) 2019 (34) 2022 (33) 2020 (26) 2025 (21) 2017 (18) 2014 (11) 2015 (11) 2016 (5) 2013 (4) 2011 (2) 2012 (2) 2010 (1) Filter by Keywords 1-Microwave Payloads (15) 0-Navigation (11) 9-Technologies applicable to several Cosmic Vision Missions (11) 0-Navigation Technologies (10) 3-Platforms / Others (10) 32-Clean Space (9) 26-Spacecraft Avionic System (8) 1-Launchers (7) 5-Space System Control (7) 36-Collaborative Activities (7) 1-On-board Data Systems (6) 2-Optical Payloads (6) 2-Space Segment - Platform (6) 3-Space Segment - Payload (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) 19-Propulsion (5) 28-Electronic Components (5) 30-Deep Sub Micron Development (5) 32-Cleanspace (5) 35-Technologies Enabling Breakthroughs in Science (5) 3-Habitation (4) 4-Ground Segment (4) 38-Advanced Manufacturing (4) 40-Design to Produce (4) 0-Telecommunications (3) 1-Avionics and Processing (3) 1-Systems (3) 2-Ground segment and operations (3) 2-Space Segment (3) 3-In-Situ Resource Utilisation (ISRU) (3) 3-User Segment Technology (3) 4-Spacecraft Environment & Effects (3) 6-Robotics (3) 10-Flight Dynamics and GNSS (3) 1-Phootprint (2) 1-Robotic Assistance (2) 2-Athena (2) 2-Contamination and Radiation (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) 6-RF Systems, Payloads and Technologies (2) 6-Sample acquisition, analysis, handling and return (2) 7-Electromagnetic Technologies and Techniques (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) 24-Materials and Processes (2) 31-Miniaturisation (2) 33-Space and Energy (2) 37-Exploration Technology (2) 1-Onboard Data Systems (1) 1-System (1) 2-Ground Segment Technology (1) 2-Human Space Flight Oriented Technologies (1) 2-Novel Energy Systems (1) 3-LISA (1) 3-Technologies for Horizon 2030 (1) 4-System Tools (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) Augmented Reality (1) Closed loop (1) concurrent engineering (1) Fuel cell (1) Habitats (1) HT-PEM (1) Human spaceflight (1) Interference Detection (1) Mission (1) Performance (1) Receivers (1) Regenerative (1) Safe Mode (1) Science (1) Signals (1) Simulation (1) Star Tracker (1) Filter by Contractor GMV AEROSPACE AND DEFENCE, SA (23) THALES ALENIA SPACE FRANCE (19) ONERA (8) DLR - German Aerospace Center (7) Fraunhofer Gesellschaft (7) SENER AEROESPACIAL, S.A. 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