Deputy Chief Engineer
Core
Lead the design, integration, and test of the engine system and turbomachinery for a next-gen high-thrust cryogenic rocket engine (LOX/LCH4) for a reusable space orbital vehicle.
Role type
Senior IC propulsion engineer (engine system & turbomachinery)
Builds
High-thrust cryogenic rocket engines (LOX/LCH4) for orbital vehicles
Domain
Aerospace propulsion, cryogenic rocket engines, turbomachinery
Required skills
liquid rocket engine development, turbopump design, rotordynamics, cryogenic propulsion systems, hot-fire testing, anomaly resolution, multi-disciplinary team leadership, requirements management, technical risk assessment
Preferred skills
engine system architecture, preburner/gas generator integration, test campaign planning, supplier/partner coordination, continuous improvement of design tools
Technologies
LOX/LCH4, turbopumps, rotordynamics, bearings, seals, preburners, gas generators
Responsibilities
Own detailed design and integration of engine system and turbomachinery; Lead engine system and turbomachinery test campaigns from component-level to hot-fire; Provide technical mentorship and oversight to engineering teams; Manage technical risks and support critical design reviews; Deputize for the Chief Engineer on technical matters and partner interactions; Drive continuous improvement in design tools and test methods.
Seniority
Senior, hands-on IC