Manager, Propulsion (Engine) (R5086)

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• Lead propulsion engineering efforts related to engine and TVC development, integration, testing, and flight operations.

• Support and mentor propulsion REs responsible for engine modules, nozzles, actuators, vectoring hardware, and associated propulsion systems.

• Drive technical execution, staffing, prioritization, and schedule alignment across propulsion activities.

• Guide teams through propulsion trade studies involving thermodynamics, transient behavior, thermal management, structural integration, and operability limits.

• Coordinate closely with controls, airframe, and mission teams to ensure propulsion integration supports aircraft maneuverability, survivability, and CONOPS requirements.

• Support root cause investigations, performance anomalies, design reviews, and flight readiness activities.

• Drive technical rigor, accountability, and measurable execution across the propulsion organization.

• Collaborate with suppliers and external partners supporting propulsion hardware and testing.

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• Bachelor's degree in Aerospace Engineering, Mechanical Engineering, or related engineering discipline.

• 7-10+ years of experience in propulsion system development, integration, test, or flight operations.

• Experience leading engineering teams or large cross-functional technical efforts.

• Strong understanding of thermodynamics, fluid mechanics, heat transfer, and aerospace propulsion fundamentals.

• Deep understanding of gas turbine engine operation, transient response, thrust production, operability limits, and thermal constraints.

• Hands-on experience supporting propulsion hardware development and test programs.

• Strong communication and organizational skills.

• U.S. Citizenship or ability to comply with ITAR requirements.

• Ability to obtain a S//SAR level security clearance desired.

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• Experience with fighter-class or low-bypass turbofan propulsion systems.

• Familiarity with engine controls, TVC systems, transient response, and actuator integration.

• Experience with GFSSP, REFPROP, ANSYS, FEA, or propulsion performance analysis tools.

• Background in rocket propulsion or thrust vector control systems.

• Experience operating in hardware-centric, test-driven aerospace environments.

• M.S. or Ph.D. in Aerospace Engineering or related discipline

#LI-MS1 #LD

Full-time regular employee offer package: Pay within range listed + Bonus + Benefits + Equity

Temporary employee offer package: Pay within range listed above + temporary benefits package (applicable after 60 days of employment)

Salary compensation is influenced by a wide array of factors including but not limited to skill set, level of experience, licenses and certifications, and specific work location. All offers are contingent on a cleared background and possible reference check. Military fellows and part-time employees are not eligible for benefits. Please speak to your talent acquisition representative for more information.

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