Turbine Aerodynamics Engineer

About the Role

As a Turbine Aerodynamics Engineer, you will work closely with aircraft designers, systems leads, and test engineers to architect the hot section of the Symphony engine, from concept through certification. You will design, optimize, and build high-performance turbine systems that enable supersonic travel.

Key Responsibilities

• Involved in the development of the Symphony turbine system (High pressure and Low pressure), including performance and aerodynamic design.
• Design airfoils and flowpath via CFD analysis.
• Develop 1D meanline models, design blading for airfoils, develop performance maps, spec out and participate in rig tests, assess as-built hardware.
• Influence how these designs affect the overall Overture aircraft and Symphony integrated propulsion system.
• Advocate for component rigs when deemed necessary, analyze rig and engine test data, and recommend courses of action.
• Develop and integrate toolchains and processes, including multi-disciplinary workflows and automation that integrate engine and propulsion analyses with airframe development.
• Coordinate with leadership, team members, and suppliers to ensure designs support manufacturing metrics.
• Opportunities to get involved in all aspects of Symphony engine development and Overture propulsion system integration, including fabrication and testing.

Requirements & Tech Stack

• Bachelor’s or Master’s in Mechanical or Aerospace Engineering or related field.
• Self-motivated individual with strong interpersonal skills, able to be a team player and solve challenging problems.
• Design experience in axial turbomachinery leading various phases of the design process using different fidelities of tools such as meanline, 2D analyses, and 3D analyses (e.g., geometry creation, mesh, and execute CFD).
• Proficiency in CAD to support module integration efforts in the engine.
• Proficiency in Python or similar programming languages.
• Experience working with engine cycle analysis tools such as NPSS or PyCycle.
• Willingness to both speak and listen, give opinions and receive opinions, consider all data, and build team consensus.

What Will Set You Apart

• Component or module ownership experience in a turbomachinery program or product.
• Supersonic jet engine design experience.
• Part 33 commercial certification experience.
• Experience in life assessments of turbine systems driven by thermal and structure failures.
• Experience analyzing secondary flow systems inside engines.
• Background in developing design tools, methods, and processes.
• Testing and data-reduction experience.
• Experience with Axstream or ADS turbomachinery software.
• A strong desire to avoid bureaucracy and move fast in a dynamic environment.

Compensation

• P2 Level: Typically 0 - 4 years of experience. Base salary range: $117,000 - $158,000.
• P3 Level: Typically 5 - 10 years of experience. Base salary range: $137,000 – $184,000.
• P4 Level: Typically 10 - 15 years of experience. Base salary range: $153,000 – $205,000.
• P5 Level: Typically 15 + years of experience. Base salary range: $168,000 – $225,000.

Actual compensation will vary based on factors including, but not limited to, location, experience, and performance.

Benefits

• Competitive pay and meaningful equity.
• Medical coverage, with Boom paying 70% of medical premiums.
• Fully paid dental and vision premiums for employee-only coverage.
• A $100–$300 company HSA match on eligible medical plans.
• A 401(k) with a company match.
• Generous paid time off and company holidays.
• Paid parental leave.
• Confidential counseling, coaching, and therapy resources.
• Company-paid life and disability insurance.
• Pet insurance.
• A $1,000 contribution to Invest America accounts for Boom babies.
• Healthy meals, an on-site gym, and a fully stocked kitchen.
• Ongoing wellness events.
• Discounts on technology, concerts, and rental cars.
• A dedicated real estate team to help you find a home.

ITAR Requirement

To conform to U.S. Government aerospace technology export regulations (ITAR and EAR), applicant must be a U.S. citizen, lawful permanent resident of the U.S., protected individual as defined by 8 U.S.C 1324b(a)(3), or eligible to obtain the required authorizations from the U.S. Department of State.