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Aerothermal Engineer

Job in Irvine, Orange County, California, 92713, USA
Listing for: Canopy A&D
Full Time position
Listed on 2026-08-08
Job specializations:
  • Engineering
    Aerospace / Aviation / Avionics, Mechanical Engineer, Systems Engineer
Salary/Wage Range or Industry Benchmark: 90000 - 140000 USD Yearly USD 90000.00 140000.00 YEAR
Job Description & How to Apply Below

About Canopy Aerospace & Defense

Canopy A&D is built to accelerate the future of advanced materials for space, defense, and maritime systems. Canopy delivers specialized materials and components that carry customers from concept through sustainment. Canopy A&D’s advanced signal attenuation technologies and production-scale manufacturing accelerate the fielding of platforms that are faster, cooler, and quieter. Our adaptive approach ensures solutions evolve at the pace of shifting challenges, keeping our customers ahead of the curve.

Role Overview

In this role on the Canopy engineering team, you will join the aerothermal team and working with external customers to refine TPS requirements through modeling and simulation. You will work closely with both the TPS design and manufacturing teams to develop effective TPS solutions for Canopy’s customers with platforms across space and hypersonics. You will join a small core team with combined experience managing nuclear weapons systems, starting companies, creating new materials, and flying things to space.

To be successful in this role, you must be self‑motivated, thrive in ambiguity, and be able to lead your own projects to completion.

Key Responsibilities
  • Engage with external customers to complete trade studies considering aerothermal environment and TPS material response
  • Assess ablation and heat transfer for TPS stackups at different levels of fidelity
  • Create, mesh, run, and post process computational fluid dynamics (CFD) models
  • Responsible for all external and internal flow field simulations
  • Calculate pressure, heat flux, and aero buffet/vibration loads for thermal and structures teams
  • Participate in the research and development process for new reentry vehicles
  • Collaborate cross functionally with design, development, and test groups
  • Develop test plans for experimental test campaigns to validate simulation results
  • Lead the review of post‑flight data and compare the data to pre‑flight estimates
  • Contribute to the development of proposals and new products that enhance the organization’s technical capabilities and support strategic growth objectives
Required Qualifications
  • Demonstrated ability to deliver on tight schedules using scrappy and creative solutions
  • Excellent written and verbal communication skills with an aptitude for interdisciplinary technical communication
  • Strong understanding of engineering fundamentals in chemistry, physics, structures, materials science, and thermodynamics
  • Experience of the entire program lifecycle of a spacecraft, from initial concept to mission success
  • Undergraduate degree in a relevant technical field with 2+ years of experience performing vehicle‑level CFD, preferably applied to launch vehicles and/or reentry systems
  • Direct experience with thermal analysis and heat transfer simulations
  • Experience with thermal protection system sizing & analysis using standard tools like FIAT, CHAR, CBAero, TPSSizer, MINIVER, and/or LAURA
  • Familiarity with Python and industry‑standard CFD tools like FUN3D, Star‑CCM+, ANSYS Fluent, or other equivalent applicable tools
Preferred Qualifications
  • Exposure to aerothermal wind tunnel and flight testing and instrumentation
  • Familiarity with typical spacecraft thermal control technologies (e.g. heat pipes, pumped fluid systems, thermal blankets, optical coatings, etc.)
  • Program management leadership experience
  • Experience performing detailed thermal analysis in programs such as ANSYS static and transient thermal (or equivalent).
  • Understanding of TPS manufacturing and integration principles, especially as they related to design for manufacturability/assembly
  • Ability to contribute to engineering proposals, driving the conceptualization, trade studies, and technical writing for advanced TPS designs and materials.
  • Familiarity with space and defense standards such as but not limited to SMS-S-016, MIL-STD-810, NASA-GSFC-7000 series or other industry equivalent standards for design, analysis, and testing of defense articles or launch vehicles
  • Active U.S. Security Clearance (Secret or higher), or the ability to obtain one based on eligibility. This includes meeting background check and other requirements, as required for…
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