Skip to main content

Hermeus

Structures Design Engineer

Los Angeles, CA$91.8k–$187.5kfull-timemidAdded 1 month ago

About this role

Hermeus, a defense aviation company, seeks a Structures Design Engineer to develop primary and secondary aircraft structures for hypersonic vehicles. You'll lead structural design from concept through flight testing while collaborating with cross-functional teams to deliver high-speed aerospace systems.

What you'll do

  • Design and analyze primary and secondary aircraft structures for hypersonic vehicles
  • Lead hardware development from trade studies through detailed design and manufacturing
  • Collaborate with propulsion, aerothermal, manufacturing, and test teams
  • Support manufacturing integration and coordinate flight test activities
  • Conduct structural analysis and validation throughout development lifecycle
  • Balance rapid iteration with engineering rigor and design discipline

What they're looking for

  • Structural design and analysis
  • Hypersonic or high-speed aircraft experience
  • Finite element analysis (FEA)
  • Materials and composites knowledge
  • Cross-functional collaboration
  • Problem-solving in ambiguous environments
  • Manufacturing design considerations
  • Technical documentation and communication
Apply with Autofill

Opens the application — the Jobs AI extension fills it for you. Set up autofill

Opens the official application on the employer’s site. No login required.

Hermeus

Hermeus is a defense aviation company building hypersonic and high-speed aircraft systems. The company is hiring engineers across thermal management, welding, tooling, and testing disciplines to support rapid prototyping and manufacturing of advanced aerospace defense capabilities.

View all jobs at Hermeus

Likely interview questions

  • Walk us through your experience with structural analysis and FEA tools—which packages have you used most, and how have you validated your models against physical test data?
  • Describe a time you had to make a design trade-off between structural performance, manufacturability, and schedule pressure. How did you approach it?