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The Software Integration Engineer - HIL is responsible for managing software configurations, integrating hardware, and developing systems for the launch vehicle Nova. The role includes collaborating with hardware teams and executing hands-on checkouts while supporting software development.

The Senior Propulsion Engineer will design and analyze rocket engine components, execute test plans, manage project schedules, and communicate results effectively.

As a Senior Structures Design Engineer, you will lead technical aspects and design of pressurized and primary structures for a reusable launch vehicle, from requirements to integration.

As a Test Engineer, you will design, build, and maintain test systems for rocket components. Responsibilities include troubleshooting, writing test procedures, and ensuring safe operations of mechanical systems.

Lead design, analysis, manufacture, and testing of reusable rocket fluids systems. Define requirements, perform incompressible/compressible flow sizing, create CAD models and drawings, manage suppliers, oversee integration, test and qualify hardware, and own schedule and budget for assigned systems.

Stage Test Engineer responsible for integrating rocket stages, preparing and leading ground tests, creating autosequences and procedures, analyzing test data, and designing, operating, maintaining, and troubleshooting fluid, mechanical, instrumentation, and control systems. The role also includes hazard analysis, schedule management, high-pressure and cryogenic system operation, and hands-on site support at an outdoor test facility.

As a Turbomachinery Engineer, you will design and test turbopumps for rocket engines, manage workflows, and improve turbomachinery performance.

Lead design, development, testing, and production of valves and actuators for a reusable launch vehicle. Define requirements, create CAD models, perform structural and fluid analyses, plan manufacturing, execute testing and qualification, coordinate suppliers, and work with vehicle teams to develop CONOPs and troubleshoot hardware.

Lead and grow a mechanical design team for stage fluids hardware on a reusable launch vehicle, owning technical roadmap, driving designs from concept through test and operations, creating design standards, mentoring engineers, and ensuring manufacturable, flight-ready fluid systems (cryogenic propellant, high-pressure gas, RCS, pressurization).

Design, manufacture, and test packaging for flight avionics and electromechanical systems. Perform thermal, structural, tolerance, and failure analyses (hand calculations and FEA). Design harness routing and secondary structures, create CAD models/drawings, interface with production and machine shops, lead design reviews, own hardware delivery from concept through integration, and drive continuous improvement to meet launch cadence.