- Robot type
- Drone · Defense
- Location
- SeattleWashingtonUSA
- Job type
- Hardware
- Posted
- Sep 15, 2026
- Salary
- $175,000–$263,000 a year
Full-time
Staff Engineer, Fuel Systems (R5900)
Job description
Shield AI — Staff Engineer, Fuel Systems (R5900) (Seattle, Washington).
Job responsibilities
- Serve as the Responsible Engineer for the aircraft fuel system, owning requirements, architecture, interfaces, hardware, and technical decisions from concept through operational deployment.
- Design, size, and integrate fuel tanks, pumps, valves, plumbing, venting and pressurization systems, filtration, level sensing, and associated fuel system hardware.
- Analyze fuel system performance across the aircraft operating envelope, including pressure and flow requirements, transient engine demand, elevated-G maneuvering, tank depletion, slosh, vapor pressure, cavitation,…
- Lead technical design reviews, supplier engagements, and hardware procurement while ensuring the fuel system meets performance, mass, thermal, reliability, safety, and mission requirements.
- Plan and execute component, subsystem, and vehicle-level testing, including instrumentation, procedures, data acquisition, performance validation, and flight readiness.
- Analyze ground and flight data to validate system performance, quantify margin, identify anomalies, and drive hardware or operational improvements.
- Lead failure investigations and root cause efforts using analysis, inspection, testing, and data to develop effective corrective actions.
- Work hands-on with design engineers, technicians, propulsion, controls, airframe, manufacturing, supply chain, test, and flight teams to build, integrate, troubleshoot, and iterate flight hardware.
Job requirements
- Bachelor's degree in Aerospace Engineering, Mechanical Engineering, or a related engineering discipline.
- 7+ years of experience in aerospace fuel systems, fluid systems, propulsion, or related aircraft system development, with demonstrated ownership of complex aerospace hardware.
- Strong understanding of thermodynamics, fluid mechanics, heat transfer, and compressible and incompressible flow.
- Strong understanding of aerospace fuel system design, including pressure losses, pump performance, venting, vapor pressure, cavitation, transient flow behavior, and thermal effects.
- Hands-on experience with fluid system hardware integration, instrumentation, testing, flight support, and technical failure investigations.
- Strong proficiency in Python or similar tools for engineering analysis, data reduction, and model correlation.
- Demonstrated ability to independently drive ambiguous technical problems to measurable results in a fast-paced development environment.
- U.S. Citizenship and active security clearance.
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