467 results found Selected 0 items No itemsClear selection Select / deselect all results (all pages, 467 total) 120 W 32 GHz TWT for Payload Data Transmitter New scientific missions require Ka-Band high power sources for the data return. Limitation on maximum antenna size and minimum required data rate can be overcome by increasing the transmitted power. At present, there is no off the shelf TWT(A) in the allocated frequency band (31800-32300 MHz) in Europe with 120W saturated output power. Instead, a 250W TWT in the range 17700 - 20200 MHz is under qualification and the feasibility of 100W TWT in the range 37500 - 42500 MHz has been recently demonstrated by test in a breadboard. Italy TDE T206-015ES Leonardo S.p.a. 2020 - 2023 120 W 32 GHz TWT for Payload Data Transmitter Novel In-Vacuum Alignment and Assembly Technologies for Optical Assemblies Many astronomical space missions observe at wavelengths which are absorbed by the atmosphere, as for example some infrared, ultraviolet or x-ray bands. Especially UV and x-ray optics have very stringent alignment tolerances due to the small wavelengths. Consequently, telescopes and instruments can only be tested at their operational wavelengths under vacuum conditions. Traditional methods for fixing optical elements and subassemblies (eg. Germany TDE T216-103MM Fraunhofer Gesellschaft 2017 - 2023 Novel In-Vacuum Alignment and Assembly Technologies for Optical Assemblies Innovative Propulsion Systems for cubesats and microsats With the underway exploitation of cubesats and microsats for commercial, Science and Earth Observation missions and the ongoing development of super-constellations of Micro/minisats, it has become obvious the need to develop European, reliable, affordable and yet performing Propulsion Systems serving these class of satellites. The introduction of propulsion functions on these classes of satellites is dramatically enhancing their performances and utilisation perspectives. Austria TDE T719-602MP ENPULSION GmbH 2020 - 2023 Innovative Propulsion Systems for cubesats and microsats 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 Innovative Propulsion Systems for cubesats and microsats With the underway exploitation of cubesats and microsats for commercial, Science and Earth Observation missions and the ongoing development of super-constellations of Micro/minisats, it has become obvious the need to develop European, reliable, affordable and yet performing Propulsion Systems serving these class of satellites. The introduction of propulsion functions on these classes of satellites is dramatically enhancing their performances and utilisation perspectives. Italy TDE T719-602MP UNIVERSITA DI PISA 2020 - 2023 Innovative Propulsion Systems for cubesats and microsats 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 AOCS COTS hardware fostering AOCS architecture and functions innovation The use of equipment based on COTS for small/constellation/low-cost platforms is impacting the reliability, availability, performance and robustness of the commonly used AOCS [Attitude and Orbit Control System] equipment (e.g. Gyros, star trackers, GNSS receivers). This activity explores innovative solutions at AOCS functions and architecture level (incl. AOCS FDIR) to mitigate the changes introduced by the use of COTS hardware for AOCS equipment. Germany TDE T705-604SA Airbus Defence and Space GmbH 2020 - 2023 AOCS COTS hardware fostering AOCS architecture and functions innovation European Methods for Thermo-Elastic Verification Almost every Scientific and Earth Observation spacecraft has stringent thermo-elastic stability/alignment requirements for the spacecraft. During the reviews of almost all of these projects many discussions on verifyng these requirements. The criticality and the complexity to verify compliance has become evident from projects like Herschel telescope, GAIA, Bepi Colombo and Solar Orbiter. France TDE T708-601MS THALES ALENIA SPACE FRANCE 2020 - 2023 European Methods for Thermo-Elastic Verification Frequency stabilisation of a Quantum Cascade Laser for Supra-THz applications The supra-THz (>3 THz) bands have been recently proposed for low Earth orbit THz remote sounding missions such as LOCUS (Low-Cost Upper-atmosphere Sounder). In order to achieve coherent detection, heterodyne receivers at supra-THz frequencies are under development by integrating in a single waveguide cavity a Schottky based mixers fed by a Quantum Cascade Laser (QCL) as Local Oscillator (LO). Thanks to the QCL, enough LO power is available to drive the mixer. Germany TDE T107-505EE DLR - German Aerospace Center 2018 - 2023 Frequency stabilisation of a Quantum Cascade Laser for Supra-THz applications High pressure water electrolyser development for exploration surface missions Any manned exploration surface mission will rely on the availability of Oxygen for breathing, a power source that can operate independently of solar illumination and possibly, the ability to manufacture rocket propellant in-situ. All of these requirements can be met by the electrolysis of in-situ manufactured water. To achieve a highly reliable, light weight system, development of an electrolysis system that operates at high pressure is crucial. Norway TDE T322-602EP PROTOTECH A.S. 2019 - 2023 High pressure water electrolyser development for exploration surface missions Pagination « First First page ‹‹ Previous page … 15 16 17 18 19 20 21 22 23 … ›› 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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