126 results found Selected 0 items No itemsClear selection Select / deselect all results (all pages, 126 total) De-risk assessment: Threat Risk Assessment on LEO Satellite Constellation (TRALEO) n/a Belgium GSTP G617-241TAdd RHEA SYSTEM S.A. 2019 - 2020 De-risk assessment: Threat Risk Assessment on LEO Satellite Constellation (TRALEO) De-risk assessment: Terrestrial Thermal Infra Red camera for space For imaging in the thermal infrared spectrum, microbolometer detectors offer an opportunity for cheaper space missions, because of their low size and power consumption and because they don’t require special cooling. They offer the possibility of a constellation of cubesats, for earth observation. The major conclusion of the project is that the microbolometer technology can be suitable for space flight. Based on tests performed in other projects, no show stoppers were identified. A breadboard was built to test and quantify performance. Belgium GSTP G617-241TAbs OIP NV 2019 - 2020 De-risk assessment: Terrestrial Thermal Infra Red camera for space De-risk assessment: Black-box re-entry capsule for satellites The performed de-risk study revealed that space players are aware of the D4D constraints that one day may be standard rules for Space Agencies. The need to acquire in-flight data is considered of primary importance. However, costs and benefits of in-flight experiments shall be compared. From the analysis conducted by VKI it emerged that recurrent low-cost experiments could be a winning strategy considering i) the intrinsic stochastic nature of the space-debris phenomenon; ii) the reduced measurement capabilities compared to ground experiments; iii) the high risk of a big single experiment. Belgium GSTP G617-241TAbv VON KARMAN INSTITUTE 2019 - 2020 De-risk assessment: Black-box re-entry capsule for satellites High Speed Deterministic Polishing of Strongly Aspherical Mirrors The activity was able to develop and improve technologies and processes (such as polishing) that will enable manufacture and production of lightweight, highly aspherical, metallic optical mirrors with the accurate surface shape and low roughness needed for high performance optical systems, such as telescopes and high-resolution spectrometers. Belgium GSTP G617-087MM AMOS, ADVANCED MECHANICAL AND OPTICSYSTEMS 2015 - 2020 High Speed Deterministic Polishing of Strongly Aspherical Mirrors Battery-Less Low Temperature Avionics and System Study Many types of science missions focus on Solar System targets with harsh thermal environments, such as Mars, the Moon, asteroids, comets, and other bodies at the fringes of the Solar System. Traditional spacecraft avionics rely on the storage of electrical energy in electrochemical systems (typically secondary batteries) for covering peak energy demands and periods where no electrical energy is generated (Lunar/Martian/cometary night, etc.). Belgium Discovery 15/002 SPACE APPLICATIONS SERV. S.A./N.V 2017 - 2020 Battery-Less Low Temperature Avionics and System Study CubeSat Technology Pre-developments - QB50: SIMBA Mission n/a Belgium GSTP GT37-001SYd INST ROYAL METEOROLOGIQUE 2018 - 2020 CubeSat Technology Pre-developments - QB50: SIMBA Mission De-risk assessment: RAM Electrical Propulsion for low altitude satellites This activity was aiming to support in-orbit demonstration mission for the validation of ram electric propulsion technologies. It shall provide a plan for the development of an intake system for air-breathing thrusters. Belgium GSTP G617-241TAbu VON KARMAN INSTITUTE 2019 - 2020 De-risk assessment: RAM Electrical Propulsion for low altitude satellites 3D Energetic Electron Spectrometer Phases C and D The 3DEES design established in the previous activity has multiple sensor stacks, each sampling a different direction. The detection techniques build on the technology from the general-purpose Energetic Particle Telescope (EPT) that is flying on Proba-V. To provide mechanical stability, low mass and compactness, a molded epoxy stack will hold both sensors and front-end electronics. In particular the following development will be done in each of the phases: Belgium GSTP G618-011EE QINETIQ SPACE NV 2015 - 2019 3D Energetic Electron Spectrometer Phases C and D Lunar spectral irradiance measurement and modelling for absolute calibration of EO optical sensors Earth observation by satellites provides essential datasets for a wide range of commercial, societal and scientific applications. Satellites have been observing the state of the environment since the launch of the radiation balance instrument on Explorer 8 in October 1959, and over the last 60 years the range of observation types and applications has grown exponentially. Today operational long-term sustained Earth observation programmes, exemplified by the Copernicus Sentinels, give a wide range of users reliable environmental information services. Belgium Discovery 15/026 Vito 2017 - 2019 Lunar spectral irradiance measurement and modelling for absolute calibration of EO optical sensors Aerodynamic of Hypervelocity Bodies ESA has long experience with LEO entry missions like Hermes, ARD, MSRO, and more recently EXPERT and IXV among others. Based on an experience of more than 4 decades of aerodynamic assessment, which have supported most of European space related projects, it is the opportunity to extend the prediction capability to the upper range of the hypersonic, the hypervelocity, to adapt the European Industry to the need of future missions and events. 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