484 results found Selected 0 items No itemsClear selection Select / deselect all results (all pages, 484 total) Flexible and reconfigurable TT C Transponder with Payload Data Transmission Satellites in all application domains include a communication subsystem with similar core functions, specific features, and different operating frequencies. ;;Central to this subsystem is the Transponder equipment. ;Its current implementations already include flexibility in terms, e.g. of modulation and coding schemes. ;However missions placing specific requirements must still bear the cost of adaptations. ;Moreover the accommodation (power, mass) of such equipment is a burden for smaller missions. Belgium GSTP GT17-111ES Antwerp Space N.V. 2018 - 2021 Flexible and reconfigurable TT C Transponder with Payload Data Transmission De-risk assessment: Experimental Feasibility Study of the Conical Pump as a Satellite Propulsion Booster n/a United Kingdom GSTP G617-241TAbc Vert Rotors UK Ltd 2018 - 2021 De-risk assessment: Experimental Feasibility Study of the Conical Pump as a Satellite Propulsion Booster De-risk assessment: Generic flexible Nanosat platform for IOD and IOV services - Scenario 1 In the framework of the GENA-SAT project, German Orbital Systems has developed a new commercial IOD/IOV service approach. It allows to fly technology demonstration and in orbit verification payloads into space for a fraction of today’s costs. To achieve this, a novel platform, together with the corresponding ground infrastructure and sustainable business model are developed based on the company’s heritage project GROOVE. Germany GSTP G617-241TAds German Orbital Systems GmbH 2020 - 2021 De-risk assessment: Generic flexible Nanosat platform for IOD and IOV services - Scenario 1 De-risk assessment: Next Generation Remote Interface Unit Arquitecture N/A Finland GSTP G617-241TAdp RUAG SPACE FINLAND OY AB 2020 - 2021 De-risk assessment: Next Generation Remote Interface Unit Arquitecture WeatherCubes demonstrator . Sweden GSTP GT17-137TIf OMNISYS INSTRUMENTS AB 2019 - 2021 WeatherCubes demonstrator De-risk assessment: Generic flexible Nanosat platform for IOD and IOV services - Scenario 3 Future CubeSat platforms for IOD/IOV missions will require improved capabilities at an equal or reduced price as currently available platforms. Two important drivers for such a platform are computational power and flexibility to adapt to different missions. OroraTech has developed a computational powerful processing unit, in form of a GPU and a new modular and flexible bus architecture, called SmartPanels, for this purpose. Equipped with this technology, OroraTech will enter the IOD/IOV market. Germany GSTP G617-241TAdu Orbital Oracle Technologies GmbH 2020 - 2021 De-risk assessment: Generic flexible Nanosat platform for IOD and IOV services - Scenario 3 De-risk assessment: Generic flexible Nanosat platform for IOD and IOV services - Scenario 4 Cost effective opportunities for in-orbit demonstration and verification (IOD/IOV) of non-space qualified products and components should be made more easily accessible for customers. This activity is aiming at the development of a customer oriented and cost effective IOD/IOV full service based on a generic NanoSat platform. Germany GSTP G617-241TAdv S4 - Smart Small Satellite Systems GmbH 2020 - 2021 De-risk assessment: Generic flexible Nanosat platform for IOD and IOV services - Scenario 4 De-risk assessment: u-Control Moment Gyroscope Achievements and status: Belgium GSTP G617-241TAbz VEOWARE SPRL 2019 - 2021 De-risk assessment: u-Control Moment Gyroscope Development of a flight Electric Propulsion Diagnostic Package (EPDP) for EP satellite Platforms So far a growing number of satellites is using electric propulsion systems for orbit raising and/or station keeping to save propellant mass with respect to chemical propulsion systems. Therefore, understanding the plasma plume of the electric thrusters and its interference with the spacecraft surfaces is of high importance. To account for this effect, extensive on ground experimental campaigns are conducted assessing the plasma plume of different thrusters. However, it is still under debate, how the plasma plume will change under space conditions. Germany GSTP GT17-144MP VON HOERNER & SULGER GMBH 2018 - 2021 Development of a flight Electric Propulsion Diagnostic Package (EPDP) for EP satellite Platforms De-risk assessment: LEROS ACE-25 Engine Development Current main engine strategy for space craft is a single point failure. NAMMO customers have requested a multiple engine capability. 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