- Job type
- Full-time
- Work mode
- Not listed
- Level
- Not listed
- Department
- Engineering
- Experience
- 2+ years experience
- Posted
- Sep 19, 2026
About the role
About the Team
The Thermal Engineering team enables Anduril's rapid hardware development cycle by ensuring advanced defense systems perform reliably in demanding real-world environments. The team works across high-power, tightly integrated products where thermal architecture, analysis, testing, and cross-functional design decisions directly affect product performance, reliability, and mission success.
About the Role
We are looking for a Thermal Engineer specializing in Thermal Protection Systems (TPS) to join our team. In this role, you will own the design, analysis, and validation of thermal protection for hypersonic and high-speed flight systems operating in extreme aerothermal environments.
This role is ideal for someone with deep expertise in aerothermal heating, ablative material response, and high-temperature thermal analysis — someone who can work across first-principles hand calculations, material response modeling, and detailed CFD to guide fast, high-consequence design decisions for systems where thermal survival is the critical constraint.
What You'll Do
- Own TPS design, material selection, and thermal analysis for hypersonic and high-speed flight vehicles, including missiles, reentry systems, and advanced flight platforms.
- Perform aerothermal heating analysis using engineering correlations, boundary-layer methods, and CFD to define the thermal environment across flight trajectories.
- Conduct ablation and material response modeling to predict TPS recession, in-depth thermal response, and structural thermal margins under mission-representative conditions.
- Evaluate and select TPS materials, including carbon phenolic, PICA, silicone-based ablators, ceramics, and high-temperature composites, based on aerothermal loads, mass constraints, and manufacturability.
- Partner with aerodynamics, structures, propulsion, and systems engineers to integrate TPS into vehicle design while managing mass, volume, and performance tradeoffs.
- Define and execute thermal and material characterization tests, including arcjet testing, furnace testing, and instrumented flight-article thermal testing.
- Build and maintain thermal models spanning hand calculations through detailed FEA/CFD to predict system performance, establish design limits, and support qualification.
- Present TPS status, risks, tradeoffs, and recommendations in internal design reviews and customer-facing technical reviews.
- Support failure reviews and root-cause investigations using test data, thermal analysis, and first-principles reasoning.
Required Qualifications
- MS or PhD in Aerospace Engineering, Mechanical Engineering, Applied Physics, or a related field with a focus on aerothermodynamics, heat transfer, thermal sciences, or materials science.
- 2+ years of experience in TPS design, aerothermal analysis, or high-temperature material response for aerospace or defense systems.
- Strong first-principles understanding of aerodynamic heating, ablation, high-temperature heat transfer, and material thermal response.
- Experience with material response modeling tools such as FIAT, CMA, TITAN, or equivalent ablation/thermal response codes.
- Experience supporting thermal design for hypersonic vehicles, reentry systems, missiles, rocket nozzles, or other systems operating in extreme aerothermal environments.
- Ability to obtain and maintain a U.S. Top Secret security clearance.
Preferred Qualifications
- Experience with aerothermal CFD tools such as DPLR, US3D, Loci-CHEM, CFD++, ANSYS Fluent, or STAR-CCM+ for high-speed reacting flow analysis.
- Experience with arcjet testing, thermal characterization testing, or flight-article thermal instrumentation.
- Experience with high-temperature materials including carbon phenolic, carbon-carbon, PICA, SLA-561V, silicone-based ablators, or ceramic matrix composites.
- Experience with radiation modeling tools such as NEQAIR, HARA, or equivalent nonequilibrium radiation solvers.
- Experience using MATLAB, Python, or similar tools for trajectory-based heating analysis, thermal margin assessment, or engineering trade studies.
- Familiarity with NASA TPS heritage tools and databases (TPSX, CEA, CBAero).
- Experience supporting PDR/CDR, qualification testing, or flight programs.
- Strong motivation to support Anduril's mission of defending the United States and allied partners.