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We are seeking a part-time Senior Thermal Protection Systems (TPS) Engineer to provide technical leadership and strategic insight in support of current and next-generation spacecraft programs to join the JETSII Contract. This role is ideal for a subject matter expert with a strong background in TPS design, analysis, and testing, and a proven track record of contributing to mission-critical aerospace systems. As a senior technical contributor, you will help shape the direction of TPS technology development, collaborate with multidisciplinary teams, and provide expert guidance during high-stakes decision-making for NASA programs. The scope of this position spans materials innovation, high-temperature testing, thermal modeling, and system-level integration.
Job Responsibility:
Lead the development and qualification of advanced TPS materials and coatings
Oversee and interpret high-enthalpy testing campaigns (arc jet, ICP torch, etc.) to validate TPS performance
Develop and maintain the TPS technology roadmap
Serve as a technical focal point for TPS-related mission operations, including real-time anomaly resolution and risk assessment
Mentor junior engineers and contribute to the strategic planning of TPS R&D initiatives
Collaborate across disciplines to ensure TPS integration aligns with vehicle-level thermal, structural, and aerodynamic requirements
Requirements:
Typically requires a minimum of a bachelor’s degree in Engineering
may be expected to have a related master’s or higher degree
normally possess 15+ years of related experience
15+ years of relevant experience in aerospace engineering, with a focus on thermal protection systems
Extensive experience in TPS design, analysis, and testing, with a deep understanding of material behavior in high-enthalpy environments
Demonstrated excellence in technical communication, including the ability to defend complex analyses and recommendations to senior stakeholders
Proven experience in TPS integration and flight certification, including system-level verification and validation processes
Proof of U.S. Citizenship or US Permanent Residency may be a requirement
Must be able to complete a U.S. government background investigation
Nice to have:
Bachelor's degree in Mechanical, Aerospace, or a related engineering discipline from an accredited institution
Advanced knowledge of aerothermal environments, including high-temperature gas dynamics and radiative heat transfer
Familiarity with CFD tools and interpretation of flowfield data for TPS boundary conditions
Familiarity with thermal response modeling using tools such as CHAR, FIAT, or PATO
Familiarity with 3D modeling and CAD tools for TPS design and integration
Hands-on experience with ablative and reusable TPS materials, as well as hot structure technologies
Proven ability to lead or manage complex spacecraft systems or subsystems
Comfortable serving as the technical authority during mission operations, including rapid decision-making under pressure
What we offer:
Excellent personal and professional career growth
9/80 work schedule (every other Friday off), when applicable