Sr. Propulsion Engineer – Thermo-Mechanical Analysis
Core
Own thermo-mechanical modeling of large-scale rotating hardware (engines/pumps) to predict metal temperatures, structural margins, and running clearances for safe human spaceflight.
Role type
Senior IC propulsion engineer (thermo-mechanical analysis)
Builds
2D axisymmetric whole-engine models and secondary-flow network integrations for next-gen rockets
Domain
Aerospace propulsion / turbomachinery
Deliverable
production ML models | product features | dashboards & analysis | research | client delivery | infrastructure | physical/clinical work
Required skills
transient thermal analysis, nonlinear structural FEA, 2D axisymmetric modeling, convective heat-transfer correlation derivation, life assessment (LCF/HCF/creep), cross-disciplinary collaboration, technical documentation
Preferred skills
rotordynamics literacy, tip-clearance prediction, scripting/automation (Python/MATLAB/ANSYS APDL), 1D fluid-network tools, component design (blisks/seals/joints), AI-assisted engineering tools
Technologies
ANSYS, Flownex, LabVIEW, MATLAB
Responsibilities
Develop and maintain 2D axisymmetric thermo-mechanical whole-engine models; translate 3D geometry to 2D representations; implement transient operating profiles; develop conjugate thermal-fluid models; apply thermal boundary conditions to predict clearances; perform structural margin and interference-fit assessments; synthesize results for operability guidance; collaborate across disciplines; develop analysis-driven design requirements.
Seniority
Senior, hands-on IC
