The Propulsion Engineer owns the design of solid rocket motor primary and secondary structures and key propulsion components. The role is central to delivering technically sound designs that meet aggressive schedule, affordability, and production goals. The engineer translates project objectives into cost-effective designs suitable for production at scale; develops solid rocket motor designs with autonomy; and supports prototype and production assembly, testing, and troubleshooting. The position uses rapid iteration to validate performance and make design adjustments, produces and authorizes CAD models and drawings to internal standards and ASME Y14.5-2009 guidelines, assesses and resolves hardware discrepancies, and collaborates with supply chain to mitigate availability risks and delays. The role requires a relevant bachelor's or advanced degree and at least two years of mechanical or fluids design, analysis, or build experience. Student project team, university rocketry club, and internship experience count. Candidates should communicate effectively across teams and document their work. Preferred qualifications include experience with test methods, aerospace materials, propulsion systems, fluid components, CAD and GD&T, rocket motors and solid propulsion, rapid product development, and a current active DoD Secret clearance or higher. A master's degree or PhD in a technical discipline is also preferred. The role may require extended hours or weekends with minimal notice to meet critical deadlines, and ongoing travel of up to 30%. Access to classified information or restricted government sites may be required depending on role designation, and employment may then depend on obtaining and maintaining required government clearance or authorization and satisfying applicable eligibility requirements. The position also requires access to export-controlled information without additional export licensing.
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Job Type
Full-time
Career Level
Mid Level