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Lead and execute EMI/EMC development and qualification testing for spacecraft and components using MIL-STD-461/DO-160/CISPR methods. Develop test procedures, perform measurements (bonding resistance, shielding effectiveness, fields, RF voltages/currents), manage test resources and calibration, support on-site and remote testing, and communicate test purpose and results to hardware teams.

The Mechanical Engineer II will design, manufacture, and test parts for artificial gravity space stations. Responsibilities include creating models, managing manufacturing processes, and supporting integration and testing.

Perform system-level reliability analyses (FTA, FMEA/FMECA, RBDs), reliability predictions, and develop/maintain spaceflight component reliability data. Support trade studies, identify critical components, assist root cause/failure investigations and risk characterization for human-rated space station systems.

Manage demand, supply, and fulfillment planning for avionics and electronic hardware. Maintain BOMs and master data, coordinate with stakeholders, drive procurement and production releases, update forecasts for ECOs, monitor obsolescence and lead times, and produce reporting (LOB, shortage, Clear-to-Build) to ensure material readiness.

Lead a multidisciplinary dynamics team to predict and verify spacecraft loads and environments across transport, ascent, docking, and on-orbit operations. Develop and validate system-level dynamic models, derive internal loads and requirements, support vibration/shock testing and qualification, correlate FEA with test/flight data, and provide technical leadership, risk management, and cross-functional coordination from concept through flight.

Lead and scale the Loads & Dynamics organization for human-rated space stations, owning technical strategy, analyses, testing, qualification, budgets, staffing, and cross-functional integration to ensure structural performance, launch certification, and on-orbit operations.

Lead and grow a dynamics engineering team to develop and verify dynamic models, load cases, and environments for spacecraft during transport, ascent, docking, and on-orbit operations. Oversee FEA model development and correlation, derive internal loads and environmental requirements, support vibration/acoustic/shock testing and qualification, coordinate across disciplines and suppliers, manage priorities and resources, mentor engineers, and contribute to analysis and process improvements.

The Integration Build Engineer will support building and testing artificial-gravity space stations, coordinating with engineers and technicians to resolve issues and develop efficient assembly practices.

The Integration Test Engineer will design and commission fluid system test stands, develop test plans, lead testing operations, and collaborate with engineers to resolve complex issues.

Provide functional support and process analysis for engineering and manufacturing systems. Act as liaison between TPMs, IT, vendors, and end users; gather requirements, map cross-system data/integrations, perform triage, support configuration reviews, create documentation and training, and assist post-go-live stabilization.