484 results found Selected 0 items No itemsClear selection Select / deselect all results (all pages, 484 total) GOMX4-B In-Orbit Demonstration Mission RACE is a GSTP Element 3 funded, in-orbit demonstration mission (IOD). The satellite will fly in low Earth orbit to demonstrate, for the first time, the capability of nano-satellite systems to perform close proximity operations (rendezvous, docking or close fly around) with different targets, using critical miniaturised technologies. These technologies are currently under development in Europe such as relative navigation sensors, control actuators, and docking mechanisms. Denmark GSTP G637-005SY GOMSPACE A/S 2016 - 2021 GOMX4-B In-Orbit Demonstration Mission De-risk assessment: Liquid Oxygen Turbopump The majority of large engine activity in Europe is hydrogen based and requires more costly pump technology, with deep cryogenic temperatures and complex sealing requirements. This activity was to demonstrate a low-cost LOX pump design, manufacture and test capability with view to enabling a LOX Kerosene 60kN engine program. These engines are more appropriate for the small launcher market than LOX/LH2. United Kingdom GSTP G617-241TAad LENA Space 2018 - 2021 De-risk assessment: Liquid Oxygen Turbopump Atmospheric Missions DAta packaging (AMIDA) The core of the activity is the development and demonstration of technologies to homogenize the data for joint use: this is highly relevant for Atmospheric Sciences data where a large variety of data in terms of sensing time and geometry and dimensionality (1D to 3D) prevent the combined use of various datasets. Nevertheless, the developed methodologies can be applied to other domains, to create meaningful subsets to cope with the growing of the data stream (large amount of EO data coming from different platforms for the same domain). Austria GSTP G611-049EO SISTEMA GMBH 2018 - 2021 Atmospheric Missions DAta packaging (AMIDA) Experimental characterisation of transient flow phenomena in cryogenic Fluids The activity focuses in particular when considering multiple re-ignition of upperstages. This entails waterhammer effects or pre-combustion phenomena where propellants undergo drastic changes due to sudden exposure to near-vacuum conditions. To allow proper modelling, detailed experiments need to be created for typical multi-phase, multi-component flow. Following activities are foreseen: Evaluation of the liquid front behaviour during waterhammer prior, during and after impact for different operational conditions. Belgium GSTP G614-004MP SAFRAN Aero Boosters 2016 - 2021 Experimental characterisation of transient flow phenomena in cryogenic Fluids De-risk assessment: Computer Module Maturation Campaign Onboard computers (OBCs) are a requirement for every spacecraft, from satellites to rovers. Planetary Transportation Systems (PTS) has taken on the task of developing their own OBC unit in-house, tailored to the company’s needs: the in-house development of CubeSats and cooperative avionics technology, as well as own missions at large scale. The development status was raised to TRL 4 within this de-risking activity. The follow-on developments are planned to reach TRL 6. Germany GSTP G617-241TAel Planetary Transportation Systems GmbH 2020 - 2021 De-risk assessment: Computer Module Maturation Campaign Cyber Safety and Security Operational Centre (CSOC) Phase 1 Belgium GSTP GT1Y-001IS RHEA SYSTEM S.A. 2020 - 2021 Cyber Safety and Security Operational Centre (CSOC) Phase 1 De-risk assessment: Lander 6KN Turbopump LENA space successfully built and demonstrated a 60kN Kerosene pump, developed internal manufacturing capabilities including specialist impeller manufacturing procedures. LENA have designed a technology development roadmap for the pump technology targeting the next critical steps towards flight qualification. United Kingdom GSTP G617-241TAbm LENA Space 2019 - 2021 De-risk assessment: Lander 6KN Turbopump Development of partitioned Prototype Application (IMA-SP application development and software maintenance) Integrated Modular Avionics (IMA) is a concept developed for the aeronautics industry to manage the growth in functionality and efficiency required as the industry grows. Integrated Modular Avionics for Space (IMA-SP) is a spin-in of the corresponding concept for spacecraft avionics. Czech Republic GSTP G617-150SW EVOLVING SYSTEMS CONSULTING S.R.O. 2016 - 2021 Development of partitioned Prototype Application (IMA-SP application development and software maintenance) De-risk assessment: Satellite Test bed for EGNSS based Vehicle Localization Validation (STEV) Achievements and status: Italy GSTP G617-241TAcb RADIOLABS 2019 - 2021 De-risk assessment: Satellite Test bed for EGNSS based Vehicle Localization Validation (STEV) Planar and encapsulated SMD inductive electronic component qualification It is proposed to develop and optimize encapsulation technology for the transformation of traditional Through Hole Mount electronic inductive components into Surface Mount Technology. This will involve the development and industrialization of encapsulation process and the development of mechanical elements for the integration of traditionally applied geometries of inductive components. The proposed activity is a continuation from a GSTP 4 activity (G604-11EP Study). The goal of that activity was to assess materials and technologies related to a series of planar inductive components. 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