Lead the development of advanced hypersonic propulsion systems, overseeing technical objectives to ensure successful delivery of program requirements
Execute design and analysis of high-speed propulsion systems and subsystems in support of engine testing
Apply knowledge of high-speed propulsion and operability principles, fluid dynamics and aero-thermal mechanical systems to make informed decisions
Generate complete mechanical designs using 3D CAD of prototype systems
Perform thermal-structural analysis using ANSYS
Support the fulfillment of technical milestones of the project to meet program schedule and deliver test articles on time
Ensure that quality and safety standards are addressed and exceeded
Support engine testing activities through pre-test analysis, engine design, performance predictions, and post test data reduction
Requirements
An undergraduate degree in Mechanical Engineering or Aerospace Engineering
Minimum of 5 years of experience in related Propulsion/Missile/Prototype Development and flight test articles
Strong understanding of engineering principles and applying them to technical tasks
Skilled with Microsoft Office Suite, specifically Excel and PowerPoint
Ability to obtain and maintain a DoD Security Clearance
Master's degree is preferred
Experience with experimental setups and equipment in a hands-on environment
Skilled in CFD, preferably using Pointwise, iCFD++ and Tecplot is highly preferred
Benefits
Healthcare benefits include medical, dental, vision, and prescription drug coverage
Access to a Health Coach from GE Aerospace
Employee Assistance Program, which provides 24/7 confidential assessment, counseling and referral services
Retirement benefits include the GE Aerospace Retirement Savings Plan, a 401(k) savings plan with company matching contributions and company retirement contributions
Access to Fidelity resources and planning consultants
Tuition assistance
Adoption assistance
Paid parental leave
Disability insurance
Life insurance
Paid time-off for vacation or illness
Applicant Tracking System Keywords
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