106 results found Selected 0 items No itemsClear selection Select / deselect all results (all pages, 106 total) Modelling of hot plume with particles for improved launcher applications The technical work will be organised in 2 phases. In Phase 1 a new model for hot plume with particles will be developed to include the necessary physics such that the combustion process can be computed, the evolution of the alumina can be calculated in the engine and the subsequent impact of the alumina in terms of heat radiation to the upper stages can be quantified. Finally, in Phase 2 the new model will be used in combination with any CFD code provided by the bidder and validated with experimental data provided by ESA. Switzerland GSTP G614-011MP CFS ENGINEERING SA 2015 - 2020 Modelling of hot plume with particles for improved launcher applications Improvement, Automated Source-code-based Testing State-of-the-art in automated unit/integration testing is a semi-automated approach for which the test environment is established manually, while execution of tests is automated. In contrast to that, the FAST approach already automates building of the test environment and the stimulation of the software, complemented by recording of input-output vectors, observed properties, anomalies and evaluation by metrics and filtering algorithms. Germany GSTP G617-154SW Dr. Rainer Gerlich BSSE System and Software Engineering 2015 - 2020 Improvement, Automated Source-code-based Testing Asteroid Touring by Electric-Sail technology The electric solar wind sail (E-sail) propulsion system, because it does not run out of propellant, can enable multi-target missions that can flyby or rendezvous with a larger number of asteroids or other celestial objects. Finland TDE T719-409MP FINNISH METEOROLOGICAL INST 2015 - 2020 Asteroid Touring by Electric-Sail technology Development of a high energy beam combination, ions and electrons, for radiation test of electronic components The test of electronic components under radiation is becoming increasingly difficult because of denser and more complex packaging of the state-of-art components, such as microprocessors, memories, FPGAs, packaged in plastic, ceramic or Flip- chip configurations.This implies a larger beam range of the irradiation beam combinations, in order to reach the active and radiation-sensitive semi-conductor die of the component. The larger beam range is obtained with a high energy beam combination. Finland GSTP G617-156QE UNIV JYVASKYLA 2014 - 2020 Development of a high energy beam combination, ions and electrons, for radiation test of electronic components Enabling technologies for piezo-based deformable mirrors in active optics correction chains The increasing need for higher resolution of space optical imaging has prompted the study of novel technologies that can improve the imaging performance beyond what is currently achievable by classical optical systems. Active/adaptive optics is a very promising example of such technologies, allowing to correct for in-flight effects (such as thermo-elastic deformations, radiation effects on optical materials, gravity release, microvibrations, etc.) which impact the optical quality of space instruments. Germany GSTP G617-276MM OHB System AG 2018 - 2020 Enabling technologies for piezo-based deformable mirrors in active optics correction chains De-risk assessment: Pico-RTU system - preliminary design activity ESA’s Technical Dossier on Data Systems and On-board Computers roadmap identifies trend going towards increasing the modularity level implemented at the individual equipment supplier. Modularity on suppliers’ RTU product portfolio is something that we often already see these days. Main issue with this approach is that each manufacturer wants to bound usage of its RTUs equipment by incorporating it into avionics stack, like OBC/CMDU, TM/TC, etc. Slovenia GSTP G617-241TAcv SKYLABS D.O.O. 2019 - 2020 De-risk assessment: Pico-RTU system - preliminary design activity Flat Loop Heat Pipe Evaporator based on Advanced Manufacturing Technologies Currently, the Loop heat pipe evaporators are mainly cylindrical in order to cope with the internal working pressure. All electronic units have a flat thermal interface. This means that an LHP requires an thermal interface adaptor from a rectangular flat surface to a cylindrical shape (e.g. saddle). Therefore, these additional thermal interfaces and the small contact area decrease the overall performance of the Loop heat pipe. Spain TDE T721-403MT IBERESPACIO 2016 - 2020 Flat Loop Heat Pipe Evaporator based on Advanced Manufacturing Technologies Passive damped deployment of full composite structures This study aimed to demonstrate the feasibility, use and functionality of carbon fibre-reinforced flexible epoxy (CFRFE) materials for self-deployable space structures (such as deployable tape-spring hinges) by designing, simulating, manufacturing, testing and correlating a classic (100% carbon fibre-reinforced plastic -rigid resin- CFRP) deployable tape-spring hinge and a CFRFE deployable tape-spring hinge and compare their mechanical and dynamic behaviours. Germany Discovery ITI76 INGENIERIA PROSIX SL 2018 - 2020 Passive damped deployment of full composite structures Maritime Adaptive GNSS Safety concept (MAGS) The MAGS project focused on developing a Maritime Adaptive GNSS Safety Concept to support mariners, particularly within the vicinity of ports. Germany Discovery 15/113 DLR 2018 - 2020 Maritime Adaptive GNSS Safety concept (MAGS) APEX (Hera Cubesat) Consolidation phase Within the Space Safety programme (S2P), under preparation for the Council at Ministerial Level (Space19+), Hera is the cornerstone mission of the planetary defence and it builds on extensive work done by the Agency and European industry between 2011 and 2019. In particular, the Hera mission in currently in Phase B1 which will be concluded by a System Requirements Review in Summer 2019 after which a prompt start of Phase B2 is planned to reach PDR by end of 2020. ; Sweden GSTP GT17-176SP SWEDISH INSTITUTE OF SPACE PHYSICS 2019 - 2020 APEX (Hera Cubesat) Consolidation phase Pagination « First First page ‹‹ Previous page … 3 4 5 6 7 8 9 10 11 ›› Next page Last » Last page Filter by Programme GSTP (58) TDE (27) Discovery (20) Preparation (1) Filter by Start Year 2018 (30) 2019 (29) 2017 (17) 2016 (12) 2015 (8) 2020 (8) 2014 (2) Filter by End Year (-) 2020 (106) Filter by Keywords Moon (5) 32-Clean Space (4) 4-Users (3) 10-Flight Dynamics and GNSS (3) Cave (3) Exploration (3) Lunar Surface (3) 0-Navigation Technologies (2) 1-On-board Data Systems (2) 46-HERA (2) 99-Others (2) Battery (2) Energy Storage (2) ISRU (2) Lunar (2) Regolith (2) 1-Onboard Data Systems (1) 1-Space Situational Awareness (1) 2-Ground segment and operations (1) 2-Optical Payloads (1) 2-Space System Software (1) 4-Ground Segment (1) 4-Spacecraft Environments and Effects (1) 7-Electromagnetic Technologies and Techniques (1) 14-Life & Physical Sciences (1) 19-Propulsion (1) 26-Spacecraft Avionic System (1) 27-End to End System Design Processes (1) 35-Technologies Enabling Breakthroughs in Science (1) 36-Collaborative Activities (1) 42-SABRE (1) 48-Cybersecurity (1) active debris removal (1) active optics (1) Additive Manufacturing (1) ADR (1) agency (1) Asteroid (1) autonomous (1) basalt (1) battery-less (1) bio-inspired (1) Blue Economy (1) Boom (1) Carbon Fiber (1) Cavity (1) CFRFE (1) CleanSpace (1) climatology (1) Code (1) Crane (1) DART (1) Deflector (1) Earth observation (1) ESA (1) functionally graded materials (1) geopolymer (1) GNSS (1) Greece (1) HERA (1) Hopper (1) Impact (1) Ionosphere (1) iSALE (1) Li-Ion (1) Light Absorption Enhancement (1) low temperature (1) lunar caves (1) Manufacturing (1) Maritime (1) Materials (1) MBSE (1) mechanisms (1) Modelling (1) Nanostructures (1) Navigation (1) Ocean (1) Ontology (1) Optics (1) Planetary (1) platform (1) Power (1) power generation (1) products (1) public (1) Quantum Physics (1) reinforced (1) Robotics (1) Safety (1) Sensors (1) services (1) shock physics (1) Simulation (1) skylight (1) Solar panels (1) space (1) Spacecraft (1) Space debris (1) space debris mitigation (1) SPH (1) study (1) system engineering (1) Telescope (1) Tether (1) Theory (1) value creation (1) Filter by Contractor AIRBUS DEFENCE AND SPACE SAS (4) GMV AEROSPACE AND DEFENCE, SA (4) THALES ALENIA SPACE ITALIA SPA (3) INGENIERIA PROSIX SL (2) OHB Digital Solutions GmbH (2) ONERA (2) RHP-TECHNOLOGY GMBH (2) SENER AEROESPACIAL, S.A. 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