107 systems-science-"https:"-"https:"-"https:"-"https:" positions at European Space Agency
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of Technology, Engineering and Quality (D/TEC). Reporting directly to the Head of the Resource Management and Control Office, you will contribute to the smooth operation of the Directorate and the management
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, business administration or a related discipline is required for this post. Diversity, Equity and Inclusiveness ESA is an equal opportunity employer, committed to achieving diversity within the workforce and
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Centre (ESTEC). Alongside other site managers across Europe, you will be a member of the REFM Leadership Team, led by the Head of Department with the Heads of Division, who are responsible for optimising
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, Engineering and Quality. The System Security Section is responsible for the end-to-end system security engineering of the Agency’s missions, projects and activities in the space, ground and user segments and
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Location ESOC, Darmstadt, Germany with a resident assignment to the ESA Houston Office, Texas, USA. Description The Directorate of Human and Robotic Exploration Programmes (D/HRE) is a programme
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This job opening is for the purposes of Reserve list recruitment on multiple positions. ESA is initiating a Reserve list recruitment process to meet the consistently high demand for Contracts
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observation, human spaceflight and robotic exploration, navigation, telecommunications and space transportation. The Section is also a focal point for electrical harness engineering. The Section’s laboratory
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accounting, auditing or economics is required for this post. Additional requirements In addition, you should have: a minimum of three years’ cumulative experience in auditing activities. strong analytical and
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This is a fixed-term appointment with an initial duration of 4 years. Depending upon performance and organisational needs, the appointment may be extended up to a possible maximum duration of 8
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in telecommunications, electronics or RF/microwave engineering is required for this post. Additional requirements Very good understanding of TT&C and PDT subsystems for space applications, such as