Chief Engineer – Turbine Propulsion Systems

We are seeking a visionary and technically accomplished Chief Engineer to lead the design, development, and integration of advanced turbine propulsion systems for aerospace or high-performance industrial applications. This senior leadership role combines deep technical expertise with strategic oversight, ensuring the successful execution of propulsion programs from concept through certification. The ideal candidate will possess a robust background in thermodynamics, turbomachinery, system integration, and regulatory compliance within the aerospace or energy sectors.

Key Responsibilities:

• • Serve as the highest technical authority for turbine propulsion system architecture, design, performance, and integration.

  • Provide strategic direction and technical oversight to multidisciplinary engineering teams (aerothermal, mechanical, controls, structural, and systems engineers).

  • Drive development of gas turbines, including compressors, combustors, turbines, gearboxes, and associated control systems.

  • Ensure compliance with relevant certification standards (e.g., FAA, EASA, DoD, ISO) and customer requirements.

  • Lead technical reviews, design audits, and risk assessments across all stages of product lifecycle.

  • Collaborate with program managers, supply chain, manufacturing, and quality teams to ensure design feasibility, cost-effectiveness, and producibility.

  • Guide performance analysis, CFD/FEM modeling, engine testing, and validation efforts.

  • Serve as a technical liaison with customers, regulatory authorities, and executive leadership.

  • Mentor senior engineers and drive organizational capability through technical training and knowledge sharing.

  • Support proposal development, R&D initiatives, and long-term technology roadmapping.

Key Focus Areas:

• • Propulsion System Architecture: Lead conceptual and detailed system-level design of turbine engines, balancing performance, weight, cost, and reliability.

  • Thermodynamic Optimization: Oversee performance modeling, cycle analysis, and thermal integration for maximum efficiency.

  • Mechanical Integrity & Durability: Ensure component strength, fatigue resistance, and thermal/material compatibility under extreme operating conditions.

  • Regulatory Compliance & Certification: Guide certification efforts aligned with aerospace safety standards (FAA/EASA Part 33, MIL-STDs, etc.).

  • Cross-Functional Collaboration: Integrate engineering disciplines and ensure alignment with manufacturing, supply chain, and program objectives.

  • Technology Leadership: Drive innovation in propulsion technologies, including hybrid-electric, additive manufacturing, and novel cooling/combustion techniques.

  • Testing & Validation: Oversee test planning, instrumentation strategies, and data analysis for development and qualification testing.

Qualifications:

• • Master’s or PhD in Aerospace, Mechanical, or Propulsion Engineering.

  • 15+ years of experience in turbine engine design and development (aerospace, defense, or industrial gas turbines).

  • Proven experience in leading multidisciplinary engineering teams and managing complex technical programs.

  • Deep knowledge of turbomachinery design, combustion systems, heat transfer, materials, and control integration.

  • Familiarity with tools such as ANSYS, Fluent, NPSS, MATLAB/Simulink, CATIA/SolidWorks.

  • Demonstrated success with propulsion system certification and interaction with regulatory bodies.

  • Strong leadership, communication, and decision-making skills.

  • US Citizenship or equivalent may be required for defense-related programs.