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focuses on instrumentation development for microgravity experiments and exploration, environmental control and life support system (ECLS) design, engineering and verification and in situ resource
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, aligned with a model-based system engineering paradigm; Developing and curating reference asset architectures, threat and control catalogues for instantiating space system risk assessments; Deriving formal
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for this position, the following is required: PhD in systems engineering, computer science or informatics, and the subject of the thesis should be relevant to the task description provided above (e.g. digital twin
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, the following is required: PhD in high-speed aerodynamics, turbulence, transition and combustion modelling, or another relevant aerospace engineering discipline. Additional requirements In addition to your CV and
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: autonomous and fault-tolerant systems (including health monitoring systems), advanced guidance, control, estimation and optimisation techniques and tools, and the technology development of GNC sensors with a
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Engineering, Flight Programmes, Directorate of Space Transportation. Under the authority of the Vega and Space Rider Launch System and Engineering Manager, you will be responsible for the definition and
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ESA payloads and research throughout the life cycle of the space activity or mission; Monitor associated technology developments and track scientific performance through the life cycle of space missions
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requirements associated with ESA payloads and research throughout the life cycle of the space activity or mission; Monitoring associated technology developments and tracking scientific performance through
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by candidates within five years of receiving their PhD. In particular for this position, the following is required: PhD in engineering (space engineering in particular) and/or a PA discipline
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Education A master’s degree in telecommunications, electrical or computer engineering is required for this post. A PhD in a relevant domain would be considered a plus. Additional requirements General