467 results found Selected 0 items No itemsClear selection Select / deselect all results (all pages, 467 total) 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 Physics based modelling of next generation mm-wave GaN technology Current European RF GaN power processes are optimised for up to K band, however the efficiency is less than is required to meet future planned missions. In order to meet the need for operation up to W band with up to 20% improvement in efficiency, together with improvements in linearity, a step change in device architecture is required. United Kingdom TDE T723-711ED University of Bristol 2021 - 2024 Physics based modelling of next generation mm-wave GaN technology 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 Active Battery management Active battery management is not currently used on ESA missions (apart from reducing End of Charge Voltage during the cruise of deep space missions to increase battery lifetime) but does see some limited use in cubesat programmes. Active battery management is used extensively in terrestrial energy storage. By monitoring the state of charge and voltage of the battery, the power in/out of the battery can be actively managed. This allows several benefits such as sizing a battery more conservatively because different operational modes can be accommodated more easily. Spain TDE T703-601EP ABENGOA INNOVACION SA 2019 - 2024 Active Battery management 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) 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 Development of a 40-80K vibration-free cooler With the development of vibration-free AOCS technologies (magnetic bearing reaction wheels, microthrusters), cryocoolers (Stirling, Pulse Tube) will become the main source of microvibrations. To overcome this difficulty and cope with missions (Science and Earth Observation) that have more and more stringent pointing requirements, it is necessary to develop alternate cooling solution or to adapt current technologies to generate no mechanical disturbances. France TDE T121-302MT ABSOLUT-SYSTEM 2015 - 2024 Development of a 40-80K vibration-free cooler 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 Fundamental techniques, models and algorithms for a Lunar Radio Navigation system The interest of having in the near future an available Position, Navigation and Timing (PNT) service supporting future missions to and at the Moon is currently supported by both institutional and commercial initiatives. On the commercial side, multiple companies are developing business solutions targeting the Moon and several major European companies are proposing to team up to build a communications network on the Moon compatible to terrestrial standards. In parallel, NASA has recently announced its plans to a ?Return to the moon? Italy TDE T606-701ES Sapienza University of Rome 2021 - 2024 Fundamental techniques, models and algorithms for a Lunar Radio Navigation system Pagination « First First page ‹‹ Previous page … 5 6 7 8 9 10 11 12 13 … ›› 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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