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Support Nyx system integration and verification: define test plans, prepare and execute functional and environmental test campaigns, coordinate subsystem integration, document results, process anomalies, and drive verification closure with multidisciplinary teams.

Lead end-to-end system integration and verification of mechanical and functional spacecraft elements. Define and execute verification plans, manage requirement traceability, run functional and environmental tests, coordinate anomalies and closure of verification evidence, and collaborate with subsystem leads, AIT teams, and external partners to ensure reliable mission performance.

Lead end-to-end system integration and verification for the Nyx orbital vehicle focusing on SIL/PIL/HIL and physical test campaigns. Define and execute test plans, manage requirement traceability, analyse and close verification evidence, coordinate with subsystem leads, AIT teams, and partners, resolve anomalies, and ensure safe, reliable mechanical performance across mission profiles.

Support flight software certification by performing V&V and IV&V, requirements tracing, test planning, and interfacing with system engineering and certification bodies. Prepare certification and NASA safety review documentation, apply formal standards, maintain software functional design, and plan integrated mission testing while collaborating with development, product assurance, and safety authorities. Use C++ and Python knowledge in design and test discussions.

Support flight software certification for the Nyx orbital vehicle through V&V and IV&V, requirements management and tracing, test planning, documentation for certification and NASA safety reviews, standards interpretation, interfacing with system engineering and product assurance, and contributing to software design and integrated mission testing using C++ and Python.

Define and evaluate propulsion system architectures for future launcher projects. Perform system/subsystem trade studies, requirements flow-down, operations and MAIT concepts, technical budgets, V&V and industrialization planning. Lead propulsion work packages, support proposals and bids, coordinate subcontractors, and run co-engineering sessions with partners.

Plan and execute qualification and acceptance test campaigns for solenoid isolation valves: develop procedures, run functional/leak/life/compatibility tests, operate DAQ and test benches, analyze data, investigate anomalies, maintain test GSE and safety for propellant-compatible operations.

Lead design and development of solenoid isolation valves for storable propulsion: define valve architecture, perform mechanical and electromagnetic sizing, select materials and seals, support qualification testing, coordinate with manufacturing and test teams, and investigate anomalies to improve reliability and manufacturability.

Lead design, build, and commission a remote lunar lander propulsion test facility. Responsibilities include defining system requirements, cryogenic and high-pressure fluid system design, P&IDs, GSE specification, automation and safety-critical controls, civil/infrastructure coordination, hazard analyses, test procedures, and on-site commissioning and operations support.

Design, analyze, and optimize combustion devices for cryogenic rocket engines using theory and CFD. Drive injector design, support hot-fire test instrumentation and data reduction, derive performance and stability metrics, maintain data-processing tools, and present technical justification in design reviews.