Staff Propulsion Engineer, Air Vehicles (Solid Rocket Motor Integration)

Own the solid rocket propulsion integration for air vehicles and missile platforms across the full development lifecycle—from concept and CAD-driven structural integration to prototype testing and flight integration. Lead key decisions on SRMs, ignition systems, thrust vector control, and associated ordnance, coordinating with vendors and executing static fire and environmental test plans. Provide technical authority on installed SRM performance predictions and propulsion test program troubleshooting.