Thruster CAD and Stress Analyst
Core
Design and structurally justify propulsion hardware (specifically Thrust Chamber Assembly) from concept to qualified design for spacecraft.
Role type
Senior IC mechanical engineer (propulsion systems)
Builds
Thrust Chamber Assembly and injector hardware for spacecraft propulsion systems
Domain
Aerospace / Propulsion Systems
Deliverable
production ML models | product features | dashboards & analysis | research | client delivery | infrastructure | physical/clinical work
Required skills
CAD design, stress analysis (hand calculations and FEA), material selection, manufacturing process definition, interface definition, trade studies, technical documentation
Preferred skills
CFD experience, additive manufacturing knowledge, welding/brazing knowledge
Technologies
Ansys, Abaqus
Responsibilities
Design thrust chamber and injector hardware in CAD from concept to detailed design; Perform stress analysis to substantiate safety margins under mechanical, thermal, and pressure loads; Select materials and define manufacturing processes; Work with system engineers to translate functional requirements into part-level design; Establish and maintain interface definitions and drawings; Conduct trade studies on design options; Support manufacturing, assembly, and test phases including root-cause investigations; Update stress models based on test results; Produce structural analysis reports for design reviews.
Seniority
Mid-level, hands-on IC