Enter a job title or keyword

Senior Aerospace Engineer Aerothermal & Hypersonics

Mach Industries


Job Location:

Huntington Beach, CA - USA

Yearly Salary: USD 120000 - 210000
Posted: 8 August 2026 (28 days ago)
Application Deadline: 5 November 2026
Vacancies: 1 Vacancy

Job Summary

About Mach Industries

Founded in 2022 Mach Industries is a rapidly growing defense technology company focused on developing next-generation autonomous defense platforms. At the core of our mission is the commitment to delivering scalable decentralized defense systems that enhance the strategic capabilities of the United States and its allies. With a workforce of approximately 350 employees we operate with startup agility and ambition.

Our vision is to redefine the future of warfare through cutting-edge manufacturing innovation at speed and unwavering focus on national security. We are dedicated to solving the next generation of warfare with lethal systems that deter kinetic conflict and protect global security.

The Role

Mach Industries is seeking a Senior Aerospace Engineer Aerothermal & Hypersonics to own high-speed aerodynamic and aerothermal design for next-generation hypersonic and atmospheric entry systems. This role is for an engineer with 57 years of experience who has taken complex aerospace work from concept through design analysis test and implementation and who can help stand up aerothermal and TPS test capability as the company scales.

You will lead hypersonic vehicle shaping and aero/aerothermal trades predict aerodynamic heating and related high-temperature flight environments and contribute to Thermal Protection System (TPS) / heat-shield evaluation in partnership with materials structures and Thermal Engineers. You will also support lower-speed aero work in conjunction with other aerodynamicists when programs require it.

Key Responsibilities
  • High-speed aero and aerothermal design: Lead or co-own aerodynamic and aerothermal design activities for hypersonic and atmospheric entry vehicles vehicle shaping performance stability and thermal environment definition and support lower-speed aero work in conjunction with other aerodynamicists when the program requires it.

  • Aerothermal environments: Predict and analyze aerodynamic heating environments (convective and radiative where relevant) including engineering (first-order / closed-form) heating methods and higher-fidelity aerothermal analysis as needed to support vehicle TPS and structural design.

  • TPS / heat-shield contribution: Develop and evaluate Thermal Protection System concepts materials architectures and margins for hypersonic flight and atmospheric entry vehicles including material selection support and thermal performance assessment in close partnership with materials and structures.

  • Trajectory-coupled environments: Perform or closely support entry descent and re-entry (and hypersonic mission) trajectory-informed aerothermal environment prediction and vehicle performance assessments.

  • Multidisciplinary integration: Partner with structures Thermal Engineers propulsion GNC and systems engineering to close vehicle-level trades among aero heating TPS mass/thickness and mission performance.

  • Analysis trades and documentation: Build and maintain engineering models run trade studies and document assumptions margins and recommendations for design reviews across the product lifecycle.

  • Test and validation (stand-up execute): Help establish and then support ground aerothermal/TPS test approaches and flight-test planning execution data analysis and post-flight validation including correlation of predicted environments and TPS performance to test evidence.

Required Qualifications
  • Bachelors or Masters degree in Aerospace Engineering Mechanical Engineering or a related field.

  • 57 years of professional aerospace engineering experience.

  • Demonstrated experience contributing to or leading a project from initial concept through implementation (design analysis test and fielding or equivalent closure).

  • Demonstrated experience in hypersonic aerodynamic design vehicle shaping aerodynamic performance optimization and computational or experimental analysis for high-speed flight or atmospheric entry vehicles.

  • Strong working understanding of:

  • Hypersonic flight and atmospheric entry environments

  • Aerodynamics for high-speed vehicles with ability to support lower-speed aero alongside aero teammates

  • Aerothermal analysis and aerodynamic heating (including engineering heating methods and high-temperature gas dynamics)

  • TPS materials architectures and thermal performance evaluation (working fluency; deep heat-shield ownership is a plus)

  • Experience with CFD aerothermal and aerodynamic analysis tools; familiarity with several of: STAR-CCM FUN3D LociCHEM US3D CFD DATCOM OpenVSP MATLAB and Python.

  • Experience working in fast-paced multidisciplinary engineering environments.

  • Strong analytical documentation and communication skills; ability to mentor and provide technical leadership appropriate to a senior IC.

  • Must be a U.S. person (U.S. citizen or permanent resident / as defined for export-control compliance).

Preferred Qualifications
  • Hands-on experience designing and/or selecting Thermal Protection Systems (TPS) / heat shields for high-speed flight or atmospheric entry applications.

  • Depth in heat-shield design: material selection stack-up/architecture trades recession/insulation performance and margin definition against mission heating.

  • Experience with both hypersonic atmospheric flight and atmospheric entry / re-entry aerothermal problems.

  • Experience standing up or maturing ground test capability for aerothermal or TPS validation (e.g. arcjet plasma or equivalent high-enthalpy / material test pathways) and/or flight-test aerothermal instrumentation and post-flight reconstruction.

  • Experience delivering aerothermal environments and TPS recommendations into structures and systems design reviews under schedule pressure.

  • Familiarity with defense or dual-use high-speed vehicle development and production-minded design constraints.

  • Advanced degree with thesis or professional focus in hypersonics aerothermodynamics or TPS.

Disclosures

This position may require access to information protected under U.S. export control laws and regulations including the Export Administration Regulations (EAR) and the International Traffic in Arms Regulations (ITAR). Please note that any offer for employment may be conditioned on authorization to receive software or technology controlled under these U.S. export control laws and regulations without sponsorship for an export license.

Mach participates in E-Verify and will provide the federal government with your Form I-9 information to confirm that you are authorized to work in the U.S.

The salary range for this role is an estimate based on a wide range of compensation factors inclusive of base salary only. Actual salary offers may vary based on (but not limited to) work experience education and training critical skills and business considerations. Highly competitive equity grants are included in most offers and are considered part of Machs total compensation package. Mach offers benefits such as health insurance retirement plans and opportunities for professional development.

Mach is an equal opportunity employer committed to creating a diverse and inclusive workplace. All qualified applicants will be treated with respect and receive equal consideration for employment without regard to race color creed religion sex gender identity sexual orientation national origin disability uniform service Veteran status age or any other protected characteristic per federal state or local law including those with a criminal history in a manner consistent with the requirements of applicable state and local laws. If youd like to defend the American way of life please reach out!


Required Experience:

Senior IC


About Company

Company Logo

Mach Industries is building faster, smarter defense infrastructure for the modern era.

View Profile View Profile