91 computer-"https:"-"https:"-"https:"-"https:"-"BBMRI-ERIC" positions at European Space Agency
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/artificial intelligence, forward error correction, filters, data compression and cryptography, etc. Very good knowledge of modern computer systems, simulation and modelling tools, programming languages, signal
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programmes with such institutions and fostering coherence between the objectives of EU policies and ESA’s programmes, notably through monitoring of EU policy and programme implementation and evolution
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Location ESTEC, Noordwijk, Netherlands Description Head of the Analysis Centre Control and Support Services Unit in the Business Control and Programme Management Support Office in the Directorate
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Location ESTEC, Noordwijk, Netherlands Description Copernicus Space Segment Technical Coordinator in the Copernicus Space Segment Programme, Projects Department, Directorate of Earth Observation
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to research that strengthens the resilience of European space systems. Reporting to the Head of Section, you will collaborate across the wider ESA matrix organisation, work closely with programme teams, and
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ESTEC, Noordwijk, Netherlands Description IPMA Senior Manager in the Independent Programme Management Authority, Inspector General’s Office, Director General’s Services. The Independent Programme
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Programme Manager, within the Earth Observation Programmes Department. You will be responsible for managing the WIVERN implementation (Phases B1/B2/C/D/E1), covering space and ground segments. Duties Your
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provides programme directorates with an entry point to TEC and its systems engineering support for projects. In particular, the Systems Department is responsible for providing engineering expertise in
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Projects Department: Sterna project: Sterna is the operational follow-on to the Arctic Weather Satellite (AWS) and forms part of the EPS-Sterna programme implemented in cooperation with EUMETSAT
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trajectories, including surface descent and ascent; parametric optimisation, taking different configurations into account; computing atmospheric entry trajectories and launch windows; propellant budget analysis