Senior Propulsion Systems Engineer

Support the definition of a “product baseline”, creating standard requirements, system architecture, ICDs, design and analysis goals, test plans and operations concepts.

Perform system level trade-offs, coordinating inputs from various disciplines within the team, to evaluate any proposed changes of the design baseline to satisfy the need of each individual mission.

Take ownership of the technical budgets, such as mass, propellant budget, pointing/landing accuracy for spacecraft performance.

Ensure internal interfaces between various spacecraft subsystems are maintained.

Contribute to requirements management ensuring all requirements are closed-out at the planned project landmarks.

Contribute to risk assessments during the spacecraft development and support the Project Manager in defining risk mitigation plans

Support Propulsion/AIT/Flight&Test Operations Groups and subsystem leads in defining test plans (i.e. ) and specifications which will successfully verify the spacecraft design.

Coordinate efforts between relevant subsystems and Operations Team in defining a spacecraft operational concept.

Contribute to the maintenance of our Model-Based Systems Engineering tools, esp. developing Propulsion-related models.