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Provide senior technical leadership for the design justification, lay-out optimization, and testing of the MON/MMH propulsion system; Interface with structures, thermal, avionics, GNC, safety and operations teams to ensure consistent cross-domain
You will lead the thermal design, analysis, and testing of spacecraft systems and components. You’ll be responsible for developing thermal models, defining control strategies, and ensuring compliance with mission requirements. This role involves close
Ensure development and validation planning for system, spacecraft and Ground Segment in line with technical and programmatic constraints; Follow implementation phase ensuring successful execution of AIV/T phase; Oversee
Lead complex electrical integration and test activities, ensuring the technical excellence and reliability of satellite AIT operations. He/She acts as a technical reference within the AIT team, driving improvements in test methods automation, and system
This role requires a strong analytical background, with demonstrated experience in static and dynamic analysis, including modal, random vibration, shock, and coupled loads analysis (CLA). You will work closely with structural design, AIT, and systems