467 results found Selected 0 items No itemsClear selection Select / deselect all results (all pages, 467 total) High Resolution Detector Prototype Characterisation for Star Trackers In order to support the European leadership in the field of Star Trackers, the development of a new detector supporting the high-end is required.Rather than engaging the design of a new image sensor, it is considered more efficient to characterize existing developments, either to engage directly a qualification or to identify needs in terms of delta functionality or performance.State-of-the-art Star Trackers are using today 1 mega-pixel detectors. A detector with 16 mega-pixels will aim at reducing by a factor 4 the angular resolution of one pixel. France TDE T717-702SA SODERN 2022 - 2024 High Resolution Detector Prototype Characterisation for Star Trackers Demonstrator of parallel kinematics compliant mechanism for robotic exploration One current research in industrial robots is the development of mechanisms based on parallel kinematics, with flexible elements instead of rigid bars. This allows fast robots to operate close to humans or other robots, with reduced risk of damage in case of collision.Future robotic exploration will benefit from the advantages of parallel kinematics and flexibility of its elements, such advantages being notably:- For parallel kinematics: actuators can be placed inside the robot, hence protected from the environment. Germany TDE T315-701MS Airbus Defence and Space GmbH 2021 - 2024 Demonstrator of parallel kinematics compliant mechanism for robotic exploration Material characterisation for surface and internal charging simulation and development of mitigation strategies Spacecraft charging (either surface or internal) is experienced to one degree or another by all spacecraft. The effects of high charging levels are electrostatic discharge and consequent damage to spacecraft equipment. Lower charging levels can also be a problem for scientific spacecraft because of the modification of the environment around the spacecraft and the interference of scientific measurements. As a result, simulations are used to make charging assessments as part of the spacecraft design process. France TDE T704-603EP ONERA 2021 - 2024 Material characterisation for surface and internal charging simulation and development of mitigation strategies Characterisation of contamination induced straylight With state-of-the-art polishing techniques straylight from surface roughness is decreased and straylight induced by contamination is becoming one of the main contributors to the straylight performance. It is then important to rely on representative models for contamination induced straylight. Typically, industry is using models coming from literature, which can lead to very different results. The activity shall include the following tasks : - A critical review of the existing models shall be performed. Germany TDE T116-501MM Fraunhofer Gesellschaft 2019 - 2024 Characterisation of contamination induced straylight High performance microvibration isolation system (continuation) Microvibrations are a critical issue to more and more ESA missions and represent a significant technical challenge due to the stringent stability requirements of the payloads. The ongoing TDE activity ?High performance microvibration isolation system? is developing a very promising semi-active isolation technology based on electro-magnetic shunt damper, which can be used to isolate either noise sources or payloads. United Kingdom TDE T215-017MS UNIVERSITY OF SURREY 2020 - 2024 High performance microvibration isolation system (continuation) Straylight LIDAR OGSE verification tool, hardware pre-development. Background and context: The aim of this activity is to breadboard the Straylight LIDAR instrument concept and to verify its performance experimentally. This activity aims to raise the TRL to 4 and follows the TDE activity (T216-104MM Verification of straylight rejection of optical science payloads using a pulsed laser source). The aim of this smooth follow-on is to verify the concept experimentally using an available flight spare space telescope baffle as a representative test object.Description of the concept: The technique is called ?straylight LIDAR? Switzerland TDE T208-022MM CSEM SA. Centre Suisse dElectronique et de Microtechnique SA 2021 - 2024 Straylight LIDAR OGSE verification tool, hardware pre-development. Integration Simplification of Capillary Driven Heat Transport Systems Capillary Driven Loops, as Loop Heat Pipes are currently assembled and filled at the loop heat pipe manufacturer. LHPs are used to transport heat from dissipative units where sometimes these units could be in an area that is difficult to access. In these cases, the LHP tubing routing could be very complex which makes the task of inserting these two-phase devices very challenging. Furthermore, the radiators used by LHPs could be an access panel which would need to be opened and closed multiple times. France TDE T221-111MT AIRBUS DEFENCE AND SPACE SAS 2019 - 2024 Integration Simplification of Capillary Driven Heat Transport Systems Assessment of collision avoidance manoeuvre planning for low-thrust missions In the last years, electric propulsion has become an interesting alternative to the traditional chemical propulsion for different applications, ranging from transfers to GEO to operations of (large) constellations of small satellites in LEO.The activity will first look at available data on flown hardware and their performance, together with a review of currently adopted operational concepts. Spain TDE T511-701SD GMV AEROSPACE AND DEFENCE, SA 2021 - 2024 Assessment of collision avoidance manoeuvre planning for low-thrust missions Highly Accelerated Life Test Pilot Supporting Agile Space Engineering Conventional bottom-up manufacturing and test methods are associated to a substantial portion of schedule and cost in the life cycle of a space product. Innovative methods that support agile development cycles, such as Highly Accelerated Life Testing (HALT) that started in non-space space domains are now becoming applicable for space product development and are already studied by many space companies, research institutions and space agencies. Spain TDE T723-604QE ALTER TECHNOLOGY TUV NORD S.A. 2021 - 2024 Highly Accelerated Life Test Pilot Supporting Agile Space Engineering Autonomous and optimized agile attitude control with CMGs for small satellites platforms Using an optimized control will enable not to oversize the CMGs and so to reduce the mission cost, but also the volume and mass, while benefiting of an enhanced agility. Sweden TDE T105-702SA OHB SWEDEN AB 2021 - 2024 Autonomous and optimized agile attitude control with CMGs for small satellites platforms Pagination « First First page ‹‹ Previous page 1 2 3 4 5 6 7 8 9 … ›› 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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