Principal Turbomachinery Engineer
Core
Develop fuel and oxidizer turbopump assemblies for the Aeon-R engine family to power the Terran R rocket.
Role type
Principal Turbomachinery Engineer
Builds
Aeon-R engine turbopump assemblies for the Terran R launch vehicle
Domain
Aerospace propulsion / Rocket engine development
Deliverable
production ML models | product features | dashboards & analysis | research | client delivery | infrastructure | physical/clinical work
Required skills
Turbomachinery design and analysis, Structural analysis, Thermal analysis, Fluid analysis, Rotor balancing, Interference fits, Clearance checks, Structural proofing, Leak checks, Turbopump assembly procedures
Preferred skills
Bladed CFD, Modal analysis, Rotordynamics, Bladed turbopump component design, Startup/agile environment experience, Flight development program experience
Technologies
Siemens NX, Teamcenter
Responsibilities
Design fuel and oxidizer turbopump assemblies, Perform structural, thermal, and fluid analysis, Collaborate with propulsion development and manufacturing teams, Diagnose and resolve complex turbomachinery operational issues, Drive projects to completion in ambiguous environments
Seniority
Principal, hands-on IC