Senior Test Engineer

Sr. Test Engineer

This role will be responsible for technical ownership of gas turbine engine and subsystem testing. You will be the subject matter expert on all Engine model test procedures, and the owner of development test assets and procedures. You will work in close cooperation with members of the Engineering Group and other Divisions, including supporting Manufacturing Operations with production testing scopes, existing customers performing development flight testing, or New Product Introduction (NPI) initiatives.

Subject Matter Expert (SME) for engine operability and testing capabilities at on-site test cells

Develop, maintain, and improve tools and processes associated with evaluating and post-processing engine test data

Lead the development and execution of test plans for propulsion systems for the purposes of investigation, new component qualification, process validation, or optimization. These could include Sea-Level Static or specialized simulated altitude and flight condition tests at deployed test locations

Serve as customer's main POC as they undergo engine integration and vehicle flight testing campaigns, or require troubleshooting including replication of operability anomalies in Test Facilities or occasional on-site support

Own new testing component design or modification of existing testing component designs, flow benches, test fixtures, etc. including product definition, relevant analysis, manufacturing, and validation testing

Assist Engineering Leadership in evaluating and establishing the company's Technology Roadmap as it pertains to engine development and testing capabilities to assure remains at the forefront of gas turbine propulsion systems

BS in Mechanical, Aerospace, or related Engineering discipline. Advanced degree preferred.

7+ years of industry experience with Gas Turbines, with 5+ years of hands-on test environment experience and designing/operating fluid and mechanical systems

Expertise in testing instrumentation and measurement techniques, including designing and/or applying instrumentation to Unit Under Test (UUT) or test setups

Knowledge of drafting best practices – GD&T in accordance with ASME Standards

Demonstrated experience leading Propulsion Test best practices through review processes – Test Concept Reviews (TCR), Test Readiness Reviews (TRR), etc.

Strong engineering first principles related to turbomachinery design, operation and typical failure modes. Demonstrated ability to think critically and problem solve to achieve solutions.

Knowledge of Turbine Engine Control Units (ECUs), Full Authority Digital Engine Controller (FADEC) and relevant communication protocols

Must have strong written and verbal communication skills as well as multi-tasking abilities, strong analytical skills, strong interpersonal skills, organizational and time management skills

High-energy and passionate team player who is excited about solving complex, high-impact problems, and embraces a culture of trust, free-thought, and collaboration

Must be a U.S. Citizen. This position may require access to systems/tools that are restricted to individuals who possess US citizenship

Experience and familiarity with defense industry standards and designing propulsion systems for aerospace and defense platforms (eg. MIL-STD)

CAN Aerospace communication protocols

Experience with aviation fuels (JetA, JP-8, JP-10) and other hazardous operations experience

Electrical systems design and operational experience, both for testing infrastructure and engine component testing

<15% Travel, including occasional customer or supplier site visits

Competitive salary and performance-based bonuses

Employer-sponsored, comprehensive health, dental, and vision insurance

Retirement savings plan with company match

Opportunities for professional development and career advancement

Collaborative and innovative work environment