Propulsion Analyst, Chamber and Nozzle (Raptor)
Core
Conduct static, thermal, dynamic, and fatigue analyses for Raptor Chamber and Nozzle using FEA and first principles to ensure engine performance requirements are met.
Role type
Propulsion Analyst (Structural Analysis)
Builds
Raptor rocket engine chamber and nozzle components
Domain
Aerospace propulsion / Rocket engine design
Deliverable
production ML models | product features | dashboards & analysis | research | client delivery | infrastructure | physical/clinical work
Required skills
structural analysis, statics, mechanics of materials, fatigue analysis, dynamics, heat transfer, FEA setup and post-processing, hand-calculations
Preferred skills
experience with engine hardware, model anchoring, design improvement
Technologies
FEA
Responsibilities
Conduct and document static, thermal, dynamic, and fatigue analyses for Raptor Chamber and Nozzle; Output requirements and capabilities for engine/stage interfaces; Collaborate in driving necessary analyses throughout engine component design cycles; Ensure model predictions are grounded in reality through a practical hands-on approach; Work closely with hardware and test teams to drive model anchoring and design improvements
Seniority
Entry to Mid-level, hands-on IC