Thermal Engineer, Thermal Protection Systems (TPS)

Anduril Industries

Confirmed live yesterday High trust

Quick summary

Work type
On-site
Location
Seattle, WA
Salary
$129,000–$171,000 / yr
Posted
6 days ago
Freshness
Confirmed live yesterday

Market check

Salary context

Below market

How this pay compares to similar roles

Similar $170k
This role $150k
$121k most similar roles pay here $202k

This role pays less than 68% of similar roles. Most pay $146,500–$194,300 — the shaded band above. At the midpoint, this role pays about $150k versus about $170k for comparable roles.

Based on 240 similar postings.

Employer

About Anduril Industries

Anduril Industries is a defense technology company that builds advanced hardware and software systems for national security, including autonomous drones, surveillance systems, and the Lattice AI command platform.

Anduril Industries currently has 1716 open roles on FindRole.

Listed pay typically runs $146,000–$194,000 across 1511 roles with salary data.

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View all roles at Anduril Industries

At a glance

TL;DR · Thermal Engineer, Thermal Protection Systems (TPS)

Thermal Engineer, Thermal Protection Systems (TPS) joins the Thermal Engineering team to manage the design, analysis, and validation of thermal protection for hypersonic and high-speed flight systems in extreme aerothermal environments. The role involves owning material selection and thermal analysis for missiles, reentry systems, and advanced platforms while managing trade-offs like mass and volume. Key responsibilities include performing aerothermal heating analysis using CFD and boundary-layer methods, conducting ablation modeling to predict recession, and executing characterization tests such as arcjet or furnace testing. Candidates must possess expertise in high-temperature materials like carbon phenolic, PICA, and ceramics. Required skills include proficiency with material response tools like FIAT or TITAN, and experience with CFD tools like DPLR or ANSYS Fluent. The role addresses critical thermal survival constraints for systems operating under intense aerothermal loads during flight.

What you'll do

  • Own the design, material selection, and thermal analysis for hypersonic and high-speed flight systems.
  • Perform aerothermal heating analysis using engineering correlations, boundary-layer methods, and CFD to define flight environments.
  • Conduct ablation and material response modeling to predict structural margins under mission-representative conditions.
  • Select appropriate TPS materials based on aerothermal loads, mass constraints, and manufacturability.
  • Integrate thermal protection systems into vehicle designs while managing trade-offs in mass, volume, and performance.
  • Execute thermal and material characterization tests including arcjet, furnace, and instrumented flight-article testing.
  • Build and maintain thermal models ranging from hand calculations to detailed FEA/CFD to establish design limits.
  • Lead technical reviews and root-cause investigations using test data and first-principles reasoning.

What we're looking for

  • MS or PhD in Aerospace Engineering, Mechanical Engineering, Applied Physics, or a related field focusing 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 in extreme aerothermal environments.
  • Ability to obtain and maintain a U.S. Top Secret security clearance.
  • Experience with aerothermal CFD tools such as DPLR, US3D, Loci-CHEM, CFD++, ANSYS Fluent, or STAR-CCM+ (preferred).
  • Experience with arcjet testing, thermal characterization testing, or flight-article thermal instrumentation (preferred).

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