Sr. Propulsion Analyst, Chamber and Nozzle (Raptor)
Core
Conduct static, thermal, dynamic, and fatigue/fracture analyses for Raptor Chamber and Nozzle using Finite Element Analysis (FEA) and first principles to ensure engine performance requirements are met from liftoff to landing.
Role type
Senior IC structural propulsion analyst (rocket engines)
Builds
Raptor engine components for Starship
Domain
Aerospace propulsion / Rocket engine design
Deliverable
production ML models | product features | dashboards & analysis | research | client delivery | infrastructure | physical/clinical work
Required skills
Finite Element Analysis (FEA), statics, mechanics of materials, fatigue analysis, dynamics, heat transfer, hand-calculations, model validation, FEA post-processing
Preferred skills
Master's degree in mechanical/aerospace/materials engineering or physics, experience with rocket engines or complex fluid/structural systems, ability to work on tight schedules
Technologies
FEA software (implied by setup/post-processing context)
Responsibilities
Conduct and document static, thermal, dynamic, and fatigue/fracture analyses for Raptor Chamber and Nozzle; Output requirements and capabilities for assemblies for all phases of flight; 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; Mentor less experienced engineers on analysis best practices
Seniority
Senior, hands-on IC