63 results found Selected 0 items No itemsClear selection Select / deselect all results (all pages, 63 total) 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 Phase 2 of GREAT2 phase 3 GaN process performance validation and space evaluation (GH 50-20 ) (EEE409) N/A Germany TDE EEE 409 United Monolithic Semiconductors GmbH 2021 - 2023 Phase 2 of GREAT2 phase 3 GaN process performance validation and space evaluation (GH 50-20 ) (EEE409) Online detection and diagnosis for radiation-induced errors in COTS microprocessors Microprocessors (uPs) are the backbone of digital electronic systems commonly present in spacecraft. Spain Discovery 20-D-T-TEC-05-e ARQUIMEA INGENIERIA SLU 2021 - 2023 Online detection and diagnosis for radiation-induced errors in COTS microprocessors Magnetic Shields for Quantum Sensors in Space The activity investigated a novel hybrid magnetic shielding system that uses both passive and active cancelation. The design and simulations used, along with the characterisation and measurements taken on the optimised system, are summarised in the executive summary report, and described in more detail in the Final Report. This activity was divided in two main work packages: study of optimisation and magnetic shield prototype. United Kingdom Discovery S 2021-05-b RAL (Rutherford Appleton Laboratory) 2021 - 2023 Magnetic Shields for Quantum Sensors in Space Definition of Radiation Effects Mitigation Techniques for Ultra-Deep Submicron Technologies There is a growing request coming from next generation telecom payloads for a major increase of on-board payload flexibility, processing capabilities and large data volumes. Ultra Deep Submicron technology (UDSM) is a key to achieve those needs at affordable cost, while ensuring compatibility with satellite platform mass/power constraints. In this context, Ultra Thin Body and BOX Fully-depleted Silicon-On-Insulator (UTBB-FD-SOI) technology appears as a particularly suitable solution demonstrating excellent Performance/Power/Area trade-off. France TDE T523-601ED IROC TECHNOLOGIES SA 2019 - 2023 Definition of Radiation Effects Mitigation Techniques for Ultra-Deep Submicron Technologies MOSFET Commercial plastic components survey and its SEE characterization The aim of this activity is to: Spain Discovery 20-D-S-TEC-05-e ALTER TECHNOLOGY TUV NORD S.A.U. 2021 - 2023 MOSFET Commercial plastic components survey and its SEE characterization X-Band Feed 80 kW Breadboard for ESA Deep Space Antennas The ESA Deep Space Network consists of three 35m beam waveguide antennas located around the globe. The 35m beam waveguide antennas employ an X-Band feed covering the Deep Space uplink band near 7.2 GHz and down-link band near 8.45 GHz. Simultaneous uplink commanding at 20 kW and low noise reception (Generation #2) is supported. In order to increase the transmit power capability of ESA Deep Space antennas it is currently considered to add a new high power feed and associated 80 kW High Power Amplifier. Switzerland TDE T212-054GS MIRAD MICROWAVE AG 2017 - 2022 X-Band Feed 80 kW Breadboard for ESA Deep Space Antennas R2D2 (Reliable Robust Dust Deflecting) Plug and Socket To develop large-scale infrastructure on the Moon, many different systems will have to be shipped to the Moon to produce the necessary components. This means that the traditional design of systems cannot be assumed and a production machine cannot be expected to provide its own power especially when power demand is in the 100 kW – 1 MW range. Luxembourg Discovery 20-D-T-TEC-03-e MAANA Electric 2021 - 2022 R2D2 (Reliable Robust Dust Deflecting) Plug and Socket Compact K-band Up-converter / Solid-State Power Amplifier for LEO missions Payload data transmitters in Earth Observation (EO) missions are moving from X-band to K-band (i.e. 25.5 to 27 GHz), where the downlink data rates can be increased due to the four times higher availability of bandwidth than in X-band. In addition, an interest is certainly growing in the field of small-size satellites and cube-sats. Therefore, there is a need to reduce the size/mass of the K-Band transmitter while increasing the DC-to-RF efficiency in order to relax the constraints of the thermal management systems at platform level. United Kingdom TDE T106-504ET VIPER RF LIMITED 2020 - 2022 Compact K-band Up-converter / Solid-State Power Amplifier for LEO missions Sub nano-g MEMS accelerometer for high precision orbital manoeuvres To realize the next generation of gravitational wave detectors, Nikhef, the Dutch National Institute for Subatomic Physics started developing a novel seismic sensor: An ultra-sensitive miniaturised accelerometer made in micro-electro- mechanical system (MEMS) technology. The goal was to develop an affordable accelerometer that was as sensitive as conventional seismometers, but significantly smaller and cheaper. Innoseis, a spin-off company, has been licensed to bring this cutting-edge technology to market. The Netherlands Discovery ETD 2020-07-d Innoseis 2021 - 2022 Sub nano-g MEMS accelerometer for high precision orbital manoeuvres Pagination « First First page ‹‹ Previous page 1 2 3 4 5 6 7 ›› Next page Last » Last page Filter by Programme GSTP (22) Discovery (21) TDE (19) Preparation (1) Filter by Start Year 2021 (17) 2020 (12) 2018 (6) 2022 (5) 2015 (4) 2016 (4) 2019 (4) 2023 (4) 2014 (3) 2017 (3) 2013 (1) Filter by End Year 2023 (26) 2021 (10) 2024 (8) 2019 (6) 2022 (5) 2020 (4) 2025 (2) 2016 (1) 2018 (1) Filter by Keywords 28-Electronic Components (4) 3-Space Segment - Payload (3) 32-Clean Space (2) COTS (2) 1-Microwave Payloads (1) 36-Collaborative Activities (1) accelerometer (1) amorphous silicon (1) Ariadna (1) ARM Cores (1) Battery (1) battery-less (1) BLDC (1) Distributed optical fibre sensors (1) DOFS (1) EEE component (1) EMC (1) Energy Storage (1) GaN transistors (1) gravity waves (1) ISRU (1) low temperature (1) Lunar power (1) magnetic shielding (1) MEMS (1) millimeter-wave applications (1) Moon base (1) moon plug (1) Moon solar power (1) MOSFET (1) Off-Earth manufacturing (1) photonic integrated circuits (1) PICS (1) Processors (1) quantum sensors (1) Radiation (1) space-grade polyimide (1) SPS (1) Filter by Contractor IMEC VZW. 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