Orion Thermal Protection System (TPS) Engineer

Overview

Orion Thermal Protection System (TPS) Engineer

LOCATION : NASA Johnson Space Center
JOB STATUS : Full Time

CLEARANCE: Background check & U.S. Citizenship required

Are you inspired by human space exploration and passionate about pushing the boundaries of technology to benefit both space missions and life on Earth? Join our diverse and highly collaborative team as we tackle NASA's deep space exploration challenges. At ERC, NASA's largest engineering solutions provider, we partner with NASA centers across the United States to deliver cutting-edge engineering support for mission-critical programs.

We have an exciting opportunity for a Orion Thermal Protection System (TPS) Engineer to join the team. We are seeking a highly experienced aerospace engineer to provide subsystem management and technical leadership for the certification, testing, and build of the Orion Heatshield. This role acts as an agency-level expert in spacecraft thermal design, analysis, and testing. The position requires deep expertise in heat transfer, thermal protection systems, and spacecraft certification processes.

RESPONSIBILITES

• Lead subsystem management for the Orion Heatshield, including certification planning, testing, and build oversight.
• Oversee the development of thermal models, stress analyses, and test techniques to ensure successful heatshield
• certification.
• Evaluate proposed designs and specifications for Avcoat blocks, identifying deficiencies and recommending alternative
• approaches to meet technical and safety requirements.
• Direct thermal analysis and test efforts performed by NASA civil servants and contractors across multiple centers.
• Assess all heatshield related hardware designs and supporting data at critical design and hardware acceptance reviews.
• Coordinate material property testing to support thermal and mechanical model development, delivering ablative thermal
• material models to Lockheed Martin for thermal sizing.
• Define and manage test plans for arc jet and radiant heatshield test programs.
• Provide on-site technical expertise for block bonding and gap filling operations at Kennedy Space Center.
• Compile certification evidence, track verification completion, and develop certification of flight readiness statements.
• Provides status and update reports to the Organization Chief and to Directorate management.
• Provide technical authority and consultation on Entry, Descent and Landing (EDL) system design, testing, and analysis to
• programs across NASA.
• Develop strategies for advancing EDL technologies for current and future exploration spacecraft.
• Lead technical meetings, represent the organization at conferences, and build partnerships with industry, government
• agencies, and universities.
• Mentor junior engineers, interns, and academic researchers in EDL systems analysis and testing.
• Advise management on priorities, feasibility, and risks of EDL technology development projects.
• Propose and develop innovative concepts in collaboration with industry and government partners to advance state-of-the [1] art EDL technology.

REQUIRED EXPERIENCE/SKILLS

• Bachelor's degree in Mechanical or Aerospace Engineering from an accredited engineering school.
• Minimum of 5 years of engineering analysis experience related to thermal control systems.
• Experience working with complex, vehicle level models with multiple system interactions
• Excellent technical writing skills and the ability to use data to draw conclusions and - support the conclusions when
  challenged.

PREFERRED EXPERIENCE/ SKILLS

• Experience with developing and reviewing simulation models of spacecraft hardware and systems at varying levels of
  fidelity ranging from detailed, first-principal - models to more descriptive lumped-parameter models.
• Experience with flight hardware test plan development and execution.
• Experience with requirements definition and validation of space flight hardware.
• Knowledge of programming in one or more of the following: Python or MATLAB

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