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Stratolaunch

CFD Engineer

Mojave, CAmidAdded 1 month ago

About this role

Stratolaunch is seeking a Level II or Senior CFD Engineer to support the design of hypersonic vehicles operating at Mach 5+. You'll perform advanced aerodynamic and aerothermal analyses, develop CFD databases, and contribute to design trade studies and flight test support for reusable air-launched testbeds.

What you'll do

  • Conduct advanced CFD analyses of hypersonic vehicles, focusing on interference effects and high-speed flow interactions
  • Develop, manage, and validate large CFD databases for various vehicle configurations
  • Integrate analytical, numerical, wind tunnel, and flight test data into aerodynamic and aerothermal models
  • Perform design trade studies and detailed analyses supporting conceptual and detailed design phases
  • Support flight test operations and correlate predictions with flight data
  • Develop analytical tools for hypersonic vehicle design and analysis

What they're looking for

  • CFD analysis and solver expertise (subsonic to hypersonic regimes)
  • Aerodynamic and aerothermal modeling
  • High-speed flow physics and Mach 5+ environments
  • Multi-body and propulsion-airframe interaction analysis
  • Database management and validation
  • Wind tunnel and flight test data correlation
  • Design trade study methodologies
  • Programming or scripting for tool development
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Stratolaunch

Stratolaunch develops reusable air-launched hypersonic vehicles and testbeds, including the Talon-A platform, designed to operate at Mach 5+ speeds. The company is hiring engineers across aerodynamics, structures, payloads, environmental testing, and avionics systems to support hypersonic vehicle design, integration, testing, and flight operations.

View all jobs at Stratolaunch

Likely interview questions

  • Walk us through your experience with CFD analyses in the hypersonic regime—what solvers have you used and what physical phenomena were most challenging?
  • How have you handled multi-body interference effects or propulsion-airframe interactions in previous projects?