484 results found Selected 0 items No itemsClear selection Select / deselect all results (all pages, 484 total) Advanced Antenna Modelling Tool for Performance Verification and Diagnosis Some applications require a good assessment of the antenna performance in the presence of manufacturing and assembly tolerances. This is for example the case of radiometry, for which an accurate knowledge of the full pattern, even in the low side lobes, is required. This is also the case of radar systems where good knowledge of side lobe levels within determined angular ranges is required to ensure high resolution. In particular, when the antenna operates at lower frequencies, interaction with the platform cannot be neglected and has a non-negligible impact on side lobe level. Denmark GSTP GT11-020EF TICRA Fond 2020 - 2021 Advanced Antenna Modelling Tool for Performance Verification and Diagnosis De-risk assessment: 22N Thruster Maturation Achievements and status: During a hot fire campaign (TRL-6), the thruster engineering models (EM1 and SN2) have proven ability to perform within the nominal operational pressure box of a standard GEO CPS specification. The thruster demonstrated low thrust roughness and margin against combustion instabilities for a wide throughput range. The maximum recorded throat temperature, slightly above 1300°C, shows margin against the platinum-alloy limits. Germany GSTP G617-241TAfk ArianeGroup GMBH 2021 - 2021 De-risk assessment: 22N Thruster Maturation Surface Engineering for parts made by Additive Manufacturing (Step 1) Within this activity, the surface finish techniques that can be applied to AM build hardware will evaluated. The surface coating techniques will be evaluated, including electro and electroless depositions, surface conversion, anodising and paint for few widely used space materials (e.g. Ti6Al4V, AA316L, A357.0). The surface finishing techniques will also be evaluated including chemical milling, shot pinning, honing and electrochemical polishing. The combination of the two methods will also be investigated. Guideline on surface treatments for AM made parts will be established. Finland GSTP G61C-007QT VTT TECHNICAL RESEARCH CENTRE OF FINLAND LTD 2015 - 2021 Surface Engineering for parts made by Additive Manufacturing (Step 1) Radiation testing of optical coatings for space Optical coated elements are mainly optimized for their optical characteristics, such as transparency or reflectivity in a desired spectral region. However, for space missions in the near future it is fundamental to ensure the sustainability of these optical elements in the harsh conditions of the relevant space environment, preventing the occurrence of any critical radiation induced optical degradation of their performances. Italy GSTP G617-234MM CNR, CONSIGLIO NAZIONALE DELLE RICERCHE 2017 - 2021 Radiation testing of optical coatings for space Applicability of Mutation Testing method for Flight Software Test suites are typically designed and verified by hand. Having a systematic way of designing / verifying a test suite would be beneficial to improve the test quality of critical software. Mutation testing could be an alternative or complementary testing approach, that would help to improve the design amp; verification of a test suite. Mutation would provide a systematic and repeatable process for measuring the effectiveness of a test suite and it would provide a level of assurance beyond that offered by manual review. ; Luxembourg GSTP G617-206SW UNIVERSITE DU LUXEMBOURG 2019 - 2021 Applicability of Mutation Testing method for Flight Software Surface Engineering for parts made by Additive Manufacturing (Step 1) Within this activity, the surface finish techniques that can be applied to AM build hardware will evaluated. The surface coating techniques will be evaluated, including electro and electroless depositions, surface conversion, anodising and paint for few widely used space materials (e.g. Ti6Al4V, AA316L, A357.0). The surface finishing techniques will also be evaluated including chemical milling, shot pinning, honing and electrochemical polishing. The combination of the two methods will also be investigated. Guideline on surface treatments for AM made parts will be established. Belgium GSTP G61C-007QT CRM CENTRE DE RECHERCHES METALLURGIQUES ASBL 2015 - 2021 Surface Engineering for parts made by Additive Manufacturing (Step 1) Solar Cell Interconnector Design Optimization for Surviving Harsh Fatigue Environments Recent extended LEO qualification programs revealed marginalities heritage interconnect design. In order to overcome this issue new designs have to be developed and verified. Although nominal loop design already demonstrated to be suitable for several mission environment, it is also evident that when operated outside the nominal design range could fail earlier than expected. The activity will include analysis and experimental verification of the PVA and in particular of the solar cell interconnnector. Italy GSTP G611-031EP Leonardo S.p.a. 2015 - 2021 Solar Cell Interconnector Design Optimization for Surviving Harsh Fatigue Environments De-risk assessment: Powder Characterization Background and justification: The powder characterization method PowderGenetics forms the basis for later evaluation and correlation strategies. Among the numerous variables along the whole additive manufacturing chain, PowderGenetics is a way to allow powder material to become measured, compared and evaluated. It aims to become one constant within the process. Achievements and status: Germany GSTP G617-241TAch IABG MBH 2019 - 2021 De-risk assessment: Powder Characterization Powder Metallurgy Based Materials for High Wear Resistance, High Hardness and High Temperature This activity will consist of identifying and possibly modifying (composition, process parameters) powder metallurgy materials used in other industries with similar requirements (e.g. aeronautics, medical industry) or promising novel/advanced materials. United Kingdom GSTP G61A-006QT TWI LIMITED - THE WELDING INSTITUTE 2018 - 2021 Powder Metallurgy Based Materials for High Wear Resistance, High Hardness and High Temperature High Altitude Test Facility - Realization Phase The activity has been structured in two phases: The aforementioned first phase is the design phase where the full engineering drawings and plans will be finalized. This activity, ;is the second phase where those plans will be realized and the facility built. The facility consists of the following: A vacuum test cell sized for larger engines (at least 1.5kN but projected up to 6kN). A vacuum diffuser as part of the pumping and exhaust system sized for at least 1.5 kN United Kingdom GSTP GT17-122MP Nammo (U.K.) Limited 2019 - 2021 High Altitude Test Facility - Realization Phase Pagination « First First page ‹‹ Previous page … 20 21 22 23 24 25 26 27 28 … ›› Next page Last » Last page Filter by Programme TDE (2) (-) GSTP (484) Filter by Start Year 2019 (68) 2018 (63) 2020 (60) 2021 (54) 2022 (44) 2015 (39) 2016 (38) 2014 (30) 2023 (30) 2017 (27) 2011 (13) 2012 (10) 2013 (4) 2024 (3) 2009 (1) Filter by End Year 2023 (108) 2024 (71) 2021 (70) 2020 (58) 2019 (52) 2022 (34) 2018 (31) 2017 (21) 2016 (15) 2025 (9) 2014 (6) 2015 (4) 2013 (2) 2011 (1) 2012 (1) 2030 (1) Filter by Keywords 38-Advanced Manufacturing (15) 32-Clean Space (10) 48-Cybersecurity (9) 99-Others (5) 46-HERA (4) 47-OPS-INN (4) 1-Space Situational Awareness (2) 3-Platforms / Others (2) 39-Space Situational Awareness (2) 49-Artificial Intelligence (2) Quantum (2) 0-Space Situational Awareness (1) 1-Launchers (1) 2-Optical Payloads (1) 40-Design to Produce (1) 42-SABRE (1) 43-EGS Common Core (1) BBK (1) Communication (1) concurrent engineering (1) DeepCube (1) Earth observation (1) LEO (1) Liquid Crystal (1) Low Power PPU (1) MBSE (1) Optical (1) Payload (1) Radio Frequency (1) RF (1) Satellite (1) Space Links (1) Filter by Contractor THALES ALENIA SPACE BELGIUM (7) Airbus Defence and Space GmbH (6) Fraunhofer Gesellschaft (6) INDRA SISTEMAS (6) THALES ALENIA SPACE FRANCE (6) GMV AEROSPACE AND DEFENCE, SA (5) LENA Space (5) QINETIQ SPACE NV (5) SPACEBEL SA. 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