Senior Combustion Devices Engineer II
Core
Design, analyze, and qualify combustion devices (preburners, injectors, thrust chambers, nozzles) for the Neutron rocket's Archimedes engine.
Role type
Senior IC combustion devices engineer (rocket propulsion)
Builds
Reusable medium-lift launch vehicle (Neutron) and its propulsion systems
Domain
Aerospace / Rocket Propulsion
Required skills
combustion device design, fluid dynamics, heat transfer, structural mechanics, manufacturing methods, test and flight qualification planning, trade studies
Preferred skills
reusable rocket engine design, high-speed data/video analysis, iterative development environment experience
Technologies
NX, ANSYS Mechanical, StarCCM, MATLAB, GD&T, TDK, ROCCID, PERCORP, CEA, ROCETS
Responsibilities
Define requirements and test/flight qualification plans; design and analyze components for manufacturability; collaborate with turbomachinery and engine systems teams; interpret test and flight data to enable high-cadence re-flights
Seniority
Senior, hands-on IC