Senior Propulsion Engineer, Design (Combustion Devices)

What you’d do

Lead the design, analysis, and optimization of combustion chambers, injectors, regen cooling circuits, and nozzles for satellite and space vehicle thrusters, from concept through flight qualification. Includes combustion performance and stability analysis using CEA and related tools. Found on the employer's careers page on Oct 17, 2026. Apply through the link.

You’ll need

• Bachelor's in Mechanical or Aerospace Engineering
• 8+ years in liquid rocket engine or thruster development
• Hands-on injector, combustion chamber, regen nozzle design
• Regenerative cooling design and thermal/structural analysis
• CEA and combustion stability analysis tools