115 computer-programmer-"https:"-"https:"-"https:"-"https:"-"https:"-"CSIC" positions at European Space Agency in Netherlands
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communication systems; supporting the promotion of the Directorate’s programmes and socioeconomic impact analysis; coordinating expert technical support provided by other ESA organisational units as required
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), Future Missions Department (SCI-F), Directorate of Science. Prodex is an optional programme dedicated to the development of scientific instruments and experiments for space science missions. Within
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well as by the Strategic Programme Lines; providing regular technical, programmatic and financial reporting to ESA management and ESA Member State delegations; managing the Section, including the preparation
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. The Future Missions Department oversees mission preparation activities for ESA’s science programmes, including mission definition studies (Phases 0/A/B1) and technology development activities
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within the Directorate and delegated by other directorates. The Unit also provides technical support to programme directorates as required in the area of CubeSat systems. Duties You will report to the Head
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performance evaluation of RF equipment, subsystems, components and technologies applicable to space and ground segments; providing expert technical support and consultancy to ESA projects, programmes and
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and execution of Agency standards and technology R&D programmes with special emphasis on mechanical system and configuration aspects, lightweight structures, structural dynamics and advanced structural
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, and ensure required mitigations are put in place; Contribute to the authoring of the Information Security Management Plan; Provide support to the information security and cyber security activities
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support and consultancy to ESA projects, programmes and general studies in the field of thermal control throughout all project phases; participating in feasibility studies, project reviews and the
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propulsion planetary and interplanetary trajectories, parametric optimisation, taking different configurations into account, computing atmospheric entry trajectories and launch windows, propellant budget