Senior Thermal Structures Engineer

Inversion

$137K — $193K *
Vista, CA 92084In-Person
Aerospace & Defense
5 - 7 years of experience
Job Overview by Ladders

Qualifications

  • Bachelor's in Mechanical or Aerospace Engineering or equivalent experience.
  • 5+ years in mechanical or structural design of aerospace hardware.
  • Experience with structural analysis methods, including hand analysis and finite element analysis (Nastran, Abaqus, Ansys).
  • Proven understanding of thermal-structural analysis and its effects.
  • Strong fundamentals in strength of materials and structural mechanics.
  • Proficient in 3D CAD for part and assembly design, including GD&T.
  • Ability to work effectively in fast-paced environments.

Responsibilities

  • Own detailed mechanical design of heat shield components and assemblies.
  • Conduct structural and thermal-structural analysis from hand calculations to finite element analysis.
  • Design for environments influenced by thermally induced strains.
  • Collaborate with materials and manufacturing engineers on component design for high-temperature composites.
  • Define and support structural and thermal testing for design verification.
  • Develop part and assembly models, ensuring comprehensive documentation.

Benefits

  • Exposure to cutting-edge technology in aerospace engineering.
  • Opportunity to work on high-impact projects for maneuverable reentry vehicles.
  • Collaboration with experts in materials and manufacturing engineering.
  • Hands-on experience with rapid prototyping and iteration.
  • Work in a vibrant office located in Playa Vista, CA.
Full Job Description
What You'll Do:

A heat shield is where the harsh reentry thermal environment meets structural reality - materials want to expand, attachments must not let them fail, and parts must be manufacturable at scale. As the Senior Thermal Structures Engineer, you will own the detailed design of heat shield and hot structure hardware from concept through flight, with responsibility for both the design and analysis of a key subsystem for a maneuverable reentry vehicle. In this role, you will:
  • Own the detailed mechanical design of heat shield components and assemblies, including TPS panels, hot substructure, attachments, and interfaces to the vehicle
  • Perform structural and thermal-structural analysis of your designs, from hand calculations through detailed finite element analysis
  • Design for environments where thermally induced strains are a primary driver, managing CTE mismatch, thermal gradients, and constrained expansion across joints and interfaces
  • Work with materials and manufacturing engineers to design components that can actually be fabricated, machined, and inspected in high-temperature composite material systems
  • Define and support structural and thermal-structural testing to verify your designs, from element-level tests through qualification
  • Develop your own part and assembly models, drawings, and GD&T, carrying designs from concept through released engineering

Required Qualifications:
  • Bachelor's degree in Mechanical Engineering, Aerospace Engineering, or equivalent experience in a related field
  • Typically, 5+ years of experience in the mechanical or structural design of aerospace hardware
  • Experience performing structural analysis of your own designs, including both classical hand analysis and finite element analysis (e.g., Nastran, Abaqus, Ansys)
  • Experience with thermal-structural analysis, including thermally induced stress and deflection
  • Strong fundamentals in strength of materials, structural mechanics, and the design of fastened and bonded joints
  • Proficiency with 3D CAD sufficient to own detailed part and assembly design end-to-end, including drawings and GD&T
  • Proven ability to work effectively in a fast-paced environment, including prototyping and rapid iteration of new products
  • This position is on-site at Inversion HQ in Playa Vista, CA.
  • Must have the ability to obtain and maintain a U.S. government Secret/Top Secret security clearance.

Desired Qualifications:
  • Experience designing high-temperature structures where thermally induced strains are a major design driver (hypersonic airframes , turbine engine hot sections, exhaust structures)
  • Experience designing high-density TPS components from reinforced carbon/carbon, carbon phenolic, or ceramic matrix composites
  • Experience designing hot-structure attachment schemes, such as expansion or slip joints, standoffs, flexures, and compliant interfaces
  • Experience analyzing anisotropic and composite materials, including appropriate failure criteria
  • Familiarity with the manufacturing constraints of composite or ablative materials, including machining, densification shrinkage, and inspection
  • Experience designing or supporting thermal-structural test campaigns, including strain and deflection measurement at elevated temperature
  • Prior experience working in startups and/or small independent teams

Our office headquarters is located in Playa Vista, CA. This position requires in-office presence.

The California annual base salary for this role is currently $137,000-$193,000. Pay Grades are determined by role, level, location, and alignment with market data. Individual pay will be determined on a case-by-case basis and may vary based on the following considerations: interviews and an assessment of several factors that are unique to each candidate, job-related skills, relevant education and experience, certifications, abilities of the candidate and internal equity.

ITAR Compliance:

To conform to U.S. Government space technology export regulations, including the International Traffic in Arms Regulations (ITAR) you must be a U.S. citizen, lawful permanent resident of the U.S., protected individual as defined by 8 U.S.C. 1324b(a)(3), or eligible to obtain the required authorizations from the U.S. Department of State. Learn more about the ITAR here.

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