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-DEFIS) to specialised agencies such as the European Defence Agency (EDA), the EU Satellite Centre (EU SatCen), NATO, the European Maritime Security Agency (EMSA), Frontex, JRC, EU Space Programme Agency
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) of the Earth Observation Programme Directorate (D/EOP). EOP-FM’s role is to prepare the Earth observation (EO) missions and technologies of the future, encompassing a wide range of scientific missions (Earth
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require the application of novel methodologies based on modern Mission Engineering, new system modelling techniques and new methods to compute aggregated service performances; new test beds to validate
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Item to ESA and entails the involvement and collaboration of European institutes and industries as well as PRODEX (PROgramme de Développement d'Expériences scientifiques). The GRS houses the free-falling
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for implementation; participating in the evaluation of EO small mission proposals in the framework of the InCubed (Investing in Industrial Innovation) Earth Watch Programme Element in collaboration with EOP-S and with
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Location ESOC, Darmstadt, Germany Description Ground Station Engineer in the Station Subsystems and Configuration Control Section (OPS-GSS), reporting to the Head of Section, Ground Station Engineering Division, Ground Systems Engineering and Innovation Department, Directorate of Operations. The...
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for payloads and platforms, Computers and microelectronics, EEE component technologies, radiation, and associated standardisation, Guidance, Navigation and Control, Attitude and Orbit Control and pointing, Power
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Location ESTEC, Noordwijk, Netherlands Our team and mission The Optics Section, as part of the Optics, Robotics & Life Sciences Division, provides optical engineering support to ESA projects and carries out technological research in the areas of optical component technology, optical...
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Location ESA Headquarters, Paris, France Our team and mission As part of the ESA Directorate of Space Transportation, the Future Space Transportation Preparation team (under the FLPP programme
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high-trust transfer trajectories (including rocket ascent and descent trajectories), computation of atmospheric entry trajectories, launch window and target definition, fuel budget analysis, prediction