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Field
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in all phases of the project; participating in programme reviews of the projects, assessing and being responsible for the security design, implementation, qualification and validation of space systems
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completed a Bachelor and is currently in a Master programme, Enjoys taking ownership of written content and maintaining quality standards, Works carefully and conscientiously, with strong attention to detail
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including grants advisors and project/program managers within SBD and beyond. At present, the domain Safety & Security concentrates on R&I developments in Artificial Intelligence & Data Science, notably
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of the Belastingdienst (Dutch tax agency), and with our Dual Career Programme we will also help your partner find the right job for them. Employer Erasmus University Rotterdam (EUR) is an internationally oriented
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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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that will employ a wide range of methods, including biochemical, biophysical, cell biological, computational, and genetic approaches. This cutting-edge research spans from computational analyses and single
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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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national and international consultation forums, ensuring that interoperability standards, secure computing architectures and AI-enabled research workflows developed within ODISSEI align with broader European
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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