135 results found Selected 0 items No itemsClear selection Select / deselect all results (all pages, 135 total) Fibre-steering for lightweight cost-efficient space structures RTS is currently being used to provide fast carbon-fibre-reinforced polymers (CFRP) manufacturing of aerospace grade demonstrators that are higher quality and lower mass than conventional auto tape laying (ATL) or auto fibre placement (AFP) processes. ; United Kingdom GSTP GT17-486MS ICOMAT limited 2023 - 2024 Fibre-steering for lightweight cost-efficient space structures 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 De-risk assessment: Multi-sources data correlator for commercial services The project successfully developed and demonstrated a multi-source data correlator (MSDC), advancing it from TRL 3 to TRL 7. The MSDC processes data from optical, laser and radar sources to perform high accuracy orbit determination. The MSDC was validated in an operational environment, tracking real targets for which high accuracy ephemeris were available, facilitating system validation and proving its effectiveness in accurate orbit determination. Portugal GSTP G617-241TAxb Neuraspace 2023 - 2024 De-risk assessment: Multi-sources data correlator for commercial services Passive Reflectometry and dosimetry (PRETTY) IOD CubeSat Mission: Phases C/D/E/F ;; Austria GSTP GT37-003SY RUAG SPACE GMBH 2019 - 2024 Passive Reflectometry and dosimetry (PRETTY) IOD CubeSat Mission: Phases C/D/E/F De-risk assessment: Development of large scale light-weighted HB-CESIC MIRROR - Supported Germany GSTP G617-241TAlk ECM ENGINEERED CERAMIC MATERIALS GM 2024 - 2024 De-risk assessment: Development of large scale light-weighted HB-CESIC MIRROR - Supported Chemical thruster valve test validation at engine level The proposed activity is built on the results of T119-604MP ? Chemical Thruster Valve (Dual) (CTV-D) Development, which has successfully completed a development programme, including a full qualification test campaign at valve level. ; Ireland GSTP GT17-471MP Nammo Ireland Limited 2022 - 2024 Chemical thruster valve test validation at engine level Digital Twin for (AOCS) hardware unit modelling: Definition of TRL scale A digital twin, like a virtual prototype, is a dynamic digital representation of a physical system. However, unlike a virtual prototype, a digital twin is a virtual instance of a physical system that is continually updated with the latter's performance, maintenance, and health status data throughout the physical system's lifecycle. France Discovery 21-D-S-TEC-03 THALES ALENIA SPACE FRANCE 2022 - 2024 Digital Twin for (AOCS) hardware unit modelling: Definition of TRL scale 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 Virtual reality AIT trainer Compared to current practices, where training of AIT procedures typically uses physical models of the actual hardware, manufactured at discrete moments in the spacecraft development life-cycle, the virtual reality AIT trainer, called ICARUS, shall offer substantial benefits by enabling realistic and immersive training scenarios. This shall provide more flexibility, as there is no need to have any physical models made available for the sole purpose of training. 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