Drive the pump mechanical design from architecture to component design
Ensuring that detailed mechanical analysis is performed on the pump components and assembly, reviewed and meets the required standards for life and reliability targets
Developing validation/verification tools dedicated to the mechanical design and development of pumps
Supporting pump components and assembly test campaigns (configuration definition, test execution and results reviews)
Supporting the resolution of issues encountered with the pump during development and qualification
To support design iterations to pump assemblies and/or components, including manufacturing improvements to reduce the cost and lead time of components
Requirements
Master’s degree or higher in aerospace engineering, mechanical engineering, or a related field
Strong knowledge of CAD design, drafting (including GD&T), mechanisms, structural analysis and thermodynamics
Proficiency in our software tools (Siemens NX, Ansys, Python)
Proven experience in the entire product life cycle, from design to commissioning
Experience with turbomachinery and cryogenic liquid propellant propulsion systems is a plus
Understanding of space-relevant standards (such as ECSS, MIL-STD, and NASA-HBK) and regulations
Fluency in English
Benefits
Relocation assistance is provided for those willing to relocate including visa sponsorship where applicable.
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