Mechanical Engineer, Propulsion

Firestorm is hiring a Staff Mechanical Engineer, Propulsion who will own the propulsion systems that power our sUAS platforms—from small piston and heavy-fuel engines to the fuel, induction, ignition, and exhaust architectures that surround them. You will be responsible for engine selection, integration, calibration, and qualification across Firestorm’s fuel-based aircraft, translating mission endurance and performance requirements into producible powerplant solutions.

This is a deeply hands-on, full-time role. You will spend time at the test stand, in the engine cell, and on the flight line. You will design and instrument test articles, develop ECU calibrations, investigate failures, and partner with airframe and systems engineering to make sure our propulsion systems deliver power, endurance, and reliability across the full operational envelope.

• Own development and integration of both small piston engines and micro turbojet propulsion systems, including engine selection, inlet/exhaust configuration, fuel and ignition architecture, thrust and power characterization, and ground/flight test campaigns tailored to each propulsion type.
• Develop and execute engine test plans on test stands and in-flight: power and torque mapping, BSFC characterization, endurance runs, vibration surveys, and altitude/temperature performance testing.
• Lead engine calibration and tuning, including AFR targets, EGT management, ignition timing, and injector strategy on EFI-equipped powerplants; identify and mitigate single-injector maldistribution and other cylinder-to-cylinder variability.
• Design and analyze fuel systems—tanks, lines, pumps, filters, regulators, and fuel pressure management—across the full flight envelope, including negative-G and altitude effects.
• Investigate and root-cause propulsion anomalies (RPM collapse, lean events, misfires, mechanical failures); develop structured multi-phase test plans and drive corrective action.
• Specify and qualify propellers in coordination with aerodynamics, balancing thrust, efficiency, ground clearance, acoustic signature, and vibration.
• Develop and maintain propulsion engineering documentation: interface control documents, test plans and reports, propulsion budgets (power, fuel burn, endurance), and configuration baselines.
• Partner with thermal engineering on engine cooling, exhaust routing, and heat rejection.
• Partner with electrical engineering on ECU integration, sensor selection, harnessing, and telemetry.
• Interface with engine OEMs, fuel system vendors, and propeller manufacturers as the technical lead for propulsion procurement and qualification.
• Travel to test sites and customer locations to support propulsion test events and field troubleshooting.
• Perform other duties as directed

• Bachelor's degree in Mechanical, Aerospace/Aeronautical Engineering or a related field.
• 'U.S. Person' as defined by 22 CFR
• 120.62 required due to ITAR regulations, which includes U.S. citizens, lawful permanent residents (Green Card holders), or protected individuals under asylee or refugee status
• 7+ years of experience in propulsion engineering small piston engines
• Deep working knowledge of internal combustion fundamentals: thermodynamic cycles, AFR, combustion, knock, ignition systems, and exhaust
• Hands-on experience designing and operating engine test stands, including dyno instrumentation, fuel flow measurement, EGT/CHT instrumentation, and data acquisition
• Experience with EFI Systems
• Experience with fuel system design across the full flight envelope including: altitude, attitude, and thermal effects on fuel delivery and pressure
• Experience running structured failure investigations (RCA, FMEA, FMECA or FTA) and translating findings into multi-phase test…