Full-Time

Thermal Protection System Engineer

TPS

Deadline 6/3/27
Barrios

Barrios

No salary listed

No H1B Sponsorship

Houston, TX, USA

In Person

May require commuting to other installations; primarily on-site at Houston facility.

US Citizenship Required

Category
Aerospace Engineering (1)
Requirements
  • Bachelor's degree in aerospace, mechanical, or related engineering, plus ten (10) years of related experience. License and certification may be required.
  • Minimum of 5 years of engineering analysis experience related to thermal control systems.
  • Experience with thermal modeling tools such as Thermal Desktop, SINDA/FLUINT, FEMAP, Abaqus, or equivalent.
  • Demonstrated experience with spacecraft aerothermal environments, material characterization, and TPS design processes.
  • Understanding of spacecraft certification, qualification, or verification/validation processes.
  • Strong communication, documentation, and technical reasoning skills.
  • Must be a U.S. Citizen and successfully complete a U.S. government background investigation.
  • Applicant selected may be subject to government security investigation and must meet eligibility requirements for access to classified information.
  • Work may involve sitting for extended periods.
  • May require lifting and carrying up to 25 lb.
  • Must have sufficient mobility to enter areas of test facilities where necessary.
  • Generally, an office environment but can involve inside or outside work depending on task.
  • Regular attendance in accordance with established work schedule is critical.
  • Ability to work outside normal schedule and adjust schedule to meet peak periods and surge requirements when required.
  • Must be able to work in a team atmosphere.
  • Must put forward a professional behavior that enhances productivity and promotes teamwork and cooperation.
  • Grooming and dress must be appropriate for the position and must not impose a safety risk/hazard to the employee or others.
  • This position may require some commuting and traveling to other installations as needed.
Responsibilities
  • Support the design, analysis, and verification of ablative, reusable, and multi‑layer insulating TPS materials for spacecraft.
  • Develop thermal models and perform transient/steady‑state analyses to evaluate TPS performance across mission phases.
  • Conduct material trade studies, risk identification, and mitigation planning.
  • Support TPS subsystem requirements development, validation, and configuration management.
  • Interface with structural, aerothermal, manufacturing, and systems engineering teams to integrate TPS solutions into the vehicle design.
  • Review aerothermal environment predictions and translate loads into actionable TPS design criteria.
  • Participate in fabrication process development, qualification testing, and non‑destructive evaluation planning.
  • Conduct laboratory and high-temperature testing of TPS materials in support of design, development, test and evaluation.
  • Plan testing and analyze results from high enthalpy test facilities (arc jet, inductively coupled plasma (ICP) torch, etc.)
  • Support anomaly investigations and root‑cause analyses related to TPS performance.
  • Prepare technical documentation including analysis reports, presentations, verification artifacts, and data packages.
Desired Qualifications
  • Master's degree or PhD in a related engineering discipline.
  • Experience with re‑entry vehicles, launch vehicles, or commercial spaceflight programs.
  • Knowledge of ablative materials, reusable TPS systems, composites, high‑temperature ceramics, or insulation blankets.
  • Understanding of TPS physics under high enthalpy flow (ablation, multi-phase equilibria, radiative transport).
  • Experience with heat testing (arc-jet, plasma torch, furnace testing) and associated data reduction.
  • Familiarity with CAD tools, structural analysis, or multidisciplinary integration workflows.
  • Experience in leadership or technical oversight roles.

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