Military Transient Performance & Operability Lead Engineer

Job Description Summary
The Aero/Thermal Systems Propulsion Engineer demonstrates accountability for functional, business, and broad company objectives. In this
role you will be an integral part of the Transient Performance & Operability team supporting Military Next Generation engine architectures and
current fielded products.

Job Description

Roles and Responsibilities

• Analyze transient characteristics of engines, including running cycle models
• Conduct testing in rigs, ground tests and flight engines
• Match transient engine cycle model performance to test data
• Lead transient validation design reviews
• Execute with limited guidance the analysis / evaluation of assigned projects that meet business standards, practices and procedures and the product / program requirements
• Recommend approach to meet the technical and program requirements
• Provide technical guidance to other personnel and assigned teams; mentor others in the organization
• Assure proper documentation of technical data generated for the assigned projects and/or tasks consistent with engineering policies and procedures
• Monitor and communicate project status, business issues and significant developments
• Participate as a presenter or reviewer in technical and program reviews

Required Qualifications

• Bachelor of Science in Engineering from an accredited university or college
• Minimum of 3 years' experience in systems engineering
• Due to the nature of the duties of this position, this role requires the individual to obtain and maintain US Government Security Clearance; prerequisite for a security clearance is U.S. citizenship
• Legal authorization to work in the U.S. is required. We will not sponsor individuals for employment visas, now or in the future, for this job opening.

Desired Characteristics

• Current secret clearance desired.
• 2+ years of experience in one of Systems, Performance, Operability, or Transient disciplines
• MS in Engineering or Minimum of 2 years in gas turbine engineering position
• Skilled in aircraft engine system design and integration
• Experience with aerodynamic compression components (Fan, Booster, Compressor)
• Experience with gas turbine engine performance cycle design and analysis
• Experience with NPSS, Python or similar programming languages
• Strong oral and written communication skills
• Strong interpersonal and leadership skills
• Demonstrated cross functional team experience
• Ability to influence others
• Demonstrated process orientation in approach to work

Additional Job Description

Compensation Grade

LPB1

This role requires access to U.S. export-controlled information. Therefore, for applicants who are not U.S. lawful permanent residents, U.S. Citizens, or have been granted asylee or refugee status (i.e., not a protected individual under the Immigration and Naturalization Act, 8 U.S.C. 1324b(a)(3), otherwise known as a U.S. Person), employment will be contingent on the ability to obtain authorization for access to U.S. export-controlled information from the U.S. Government.

Additional Information

GE Aerospace offers a great work environment, professional development, challenging careers, and competitive compensation. GE Aerospace is an Equal Opportunities Employer. Employment decisions are made without regard to race, color, religion, national or ethnic origin, sex, sexual orientation, gender identity or expression, age, disability, protected veteran status or other characteristics protected by law.

GE Aerospace will only employ those who are legally authorized to work in the United States for this opening.

Relocation Assistance Provided: Yes