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, analysis and testing of space systems, covering active and passive thermal control systems; Passive and active cryogenic cooling, heat transport, heat storage and heat rejection, thermal insulation, thermal
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computational and laboratory facilities. In particular, the Division is in charge of: performing design, development and verification of spacecraft structures, mechanisms, materials and manufacturing processes by
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stimulating multinational, interdisciplinary and open work environment; access to high-performance computing infrastructure and unparalleled EO and technology expertise; a unique opportunity to work
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definition of space missions, including system engineering, orbits and mission analysis, instruments, platforms, end-to-end performance, data flow, launcher interfaces, and ground processing to meet the
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better radar sensitivity and a shorter repeat-pass orbit interval for SAR interferometry) over the performance currently achievable with Sentinel-1 is possible by employing an envisioned new multi-channel
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Intern in the Science Engagement & Oversight Office, Constraining Io's dynamics via JUICE Astrometry
content of the Programme, interfacing with the scientific community and providing scientific expertise to studies, projects and missions, also in other Directorates as needed. Candidates interested
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of the science operations infrastructure under the Directorate responsibility, the operation of the Directorate’s missions once successfully commissioned, and the curation of all scientific data in the missions
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/transformative innovation to help develop innovative EO solutions. We offer: a stimulating multinational, interdisciplinary and open work environment; access to high-performance computing infrastructure and
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of the Department. Further information on your responsibilities: You will be responsible for the management, operation and development of ESA corporate and site-specific administrative and technical infrastructure
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implemented through a US-German fast-paced cooperation programme, maximising heritage from GRACE-FO to ensure continuity of observations. The second pair of satellites, P2 (i.e. NGGM), is to be implemented by