Job Description SummaryThe 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 modelsConduct testing in rigs, ground tests and flight enginesMatch transient engine cycle model performance to test dataLead transient validation design reviewsExecute with limited guidance the analysis / evaluation of assigned projects that meet business standards, practices and procedures and the product / program requirementsRecommend approach to meet the technical and program requirementsProvide technical guidance to other personnel and assigned teams; mentor others in the organizationAssure proper documentation of technical data generated for the assigned projects and/or tasks consistent with engineering policies and proceduresMonitor and communicate project status, business issues and significant developmentsParticipate as a presenter or reviewer in technical and program reviews

Required Qualifications

Bachelor of Science in Engineering from an accredited university or collegeMinimum of 3 years' experience in systems engineeringDue 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 disciplinesMS in Engineering or Minimum of 2 years in gas turbine engineering positionSkilled in aircraft engine system design and integrationExperience with aerodynamic compression components (Fan, Booster, Compressor)Experience with gas turbine engine performance cycle design and analysisExperience with NPSS, Python or similar programming languagesStrong oral and written communication skillsStrong interpersonal and leadership skillsDemonstrated cross functional team experienceAbility to influence othersDemonstrated process orientation in approach to work

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 Opportunity 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. Any offer of employment is conditioned upon the successful completion of a drug screen (as applicable).

Relocation Assistance Provided: Yes