Engines – Senior Propulsion Engineer

Engines – Senior Propulsion Engineer

Requirements

• Exceptional command of fundamentals
• Experience with detailed mechanical design including machined parts, additive parts, weldments, fasteners, seals, and translating/rotating assemblies
• Experience in designing, analyzing, and testing rocket engine components; thrust chambers, regenerative cooling channels and heatshields, injectors, turbomachinery, actuators, ignitors, gimbals, feed systems, engine layouts, etc.
• Experience in GD&T, axial/radial tolerance stackups, and material selections
• Experience post-processing test data to evaluate component performance and health
• Proficiency in heat transfer, compressible and incompressible flow, and cryogenics
• Proficiency with CAD tools (Siemens NX preferred)
• 8+ years of experience in design, build, and testing of rocket engine components
• Excellent written and verbal communication
• Bachelor’s degree in mechanical or aerospace engineering, or similar
• Willing to relocate to Seattle, WA

Responsibilities

• Own various component designs across Stoke’s engines. Examples may include: regeneratively cooled thrust chambers, reentry heat shields, injectors, turbomachinery, actuators, ignitors, cryogenic flexible feedlines, engine layouts, heat exchangers, engine gimbals, thrust structure, test rigs, etc.
• Create models, drawings, and coordinate manufacturing of various components for the engines team
• Develop and execute qualification test plans to ensure readiness for flight (proof, vibration, thermal cycle, life cycle, flow testing, hotfire, etc)
• Present and clearly communicate design, analysis, and test results
• Own root cause investigations and redesigns to improve reliability or manufacturing throughput.
• Track risks and execute appropriate mitigation plans.
• Develop and maintain test requirements and test plans
• Manage project schedules, risk, and budget

Preferred Qualifications

No preferred qualifications provided.