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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
You will be leading the development of the thrust chamber and combustion devices of the Arcos aerospike engine and Kronos full-flow staged combustion engine. You will be supporting the development of the thrust chambers for the U-Nyx family of in-space