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Cowboy Space

Designs orbital power, compute, and launches

Structural Analyst

Materials & StructuresConfirmed live in the last 24 hours
Full-timeIn-person

About the Job

Requirements

  • A bachelor's degree in Mechanical Engineering, Aerospace Engineering, or a related field.
  • At least 5 years of experience performing structural analysis for flight vehicles, propulsion systems, or other high-performance hardware.
  • Strong fundamentals in solid mechanics, structural analysis, stability, and materials behavior, including plasticity, fatigue, and fracture, with demonstrated experience determining static strength, stability, and fatigue analysis; knowledge of damage-tolerance and crack-growth methods.
  • Proficiency with commercial finite element analysis tools for linear and nonlinear structural problems.
  • Ability to substantiate results with classical hand calculations and explain and defend method selection, not only tool output.
  • Proficiency with Python or MATLAB for analysis automation, post-processing, and tool development.
  • Must be a U.S. citizen or national, U.S. permanent resident (current Green Card holder), or lawfully admitted into the U.S. as a refugee or granted asylum.

Responsibilities

  • Own the full lifecycle of structural prediction and data for the team, from load definition and first-order sizing through correlated, test-anchored models used to clear hardware for flight.
  • Derive and maintain structural load sets, including quasi-static and dynamic load cases, pressure and thermal loads, and coupled loads across ground handling, ascent, and on-orbit environments.
  • Perform static strength and stability analysis, including yield and ultimate margins, buckling, joint and fastener analysis, bearing and bolt-group checks, and local detail stress.
  • Perform fatigue and durability analysis, including spectrum development, cumulative damage, and life prediction for reusable and cycled hardware.
  • Perform fracture and damage-tolerance analysis with crack growth where applicable, including initial flaw assumptions, critical flaw sizes, and inspection intervals; provide guidance to the broader team on best design practices to avoid needing these analyses.
  • Develop tools, scripts, templates, and checklists for performing, documenting, and verifying structural analyses so results are consistent, reviewable, and repeatable across engineers.
  • Select and apply material allowables accounting for temperature, environment, process, and material form, and maintain the allowables used for analysis.
  • Define test objectives and pass/fail criteria; support proof, static, modal, vibration, and life testing with predictions; and perform data analysis and model correlation.
  • Reduce structural test data and correlate analytical predictions against measurements.
  • Support anomaly investigation and root-cause analysis, including failure reconstruction, post-test and post-flight inspection, and disposition of nonconformances.

Desired Qualifications

  • At least 10 years of experience performing structural analysis for flight vehicles, propulsion systems, or other high-performance hardware.
  • Direct experience with launch vehicle, spacecraft, or rocket engine structures.
  • Experience with formal fracture-control programs and standards such as NASA-STD-5019, and crack-growth tools such as NASGRO or AFGROW.
  • Familiarity with NASA-STD-5001 and NASA-STD-5002 structural design and verification requirements, and with factor-of-safety and model uncertainty factor policy.
  • Experience with structural dynamics, including modal survey and correlation, random vibration, shock, and coupled loads analysis.
  • Experience with composite and bonded structure analysis, including failure criteria and damage tolerance for laminates and COPVs.
  • Experience analyzing pressure vessels, tanks, or pressurized structures to ASME BPVC or AIAA S-080/S-081.
  • Strong working knowledge of relevant industry standards and material allowables sources, including MMPDS/MIL-HDBK-5, ASME BPVC, AIAA, and NASA structural standards.
  • Experience with nonlinear finite element analysis, including contact, large deflection, and material nonlinearity, and with thermal-structural or fluid-structure coupled analysis.
  • Experience developing analysis automation, scripted workflows such as ANSYS APDL or Mechanical scripting, or internal analysis tooling used by a team.
  • Experience supporting structural qualification campaigns, proof and burst testing, or vehicle static and modal testing.
  • Experience setting or owning analysis standards and review processes for a group of engineers.

About the Company

Cowboy Space

Designs orbital power, compute, and launches

Cowboy Space Corporation designs and builds orbital infrastructure to supply continuous energy and compute in orbit. It vertically integrates rocket and hardware design with space-based solar power, in-orbit computing, and launch services in one ecosystem. Its 'blank-sheet' approach makes the upper stage and compute payload a single unit, so each stage becomes a one-megawatt orbital data center on arrival, and it is expanding to space-to-Earth and space-to-space power for AI workloads. By owning end-to-end systems and avoiding launch bottlenecks, it aims to offer a scalable, persistent orbital alternative to ground-based data centers for AI and data fusion.

Company size
51-200
Company stage
Series B
Total funding
$335M
Headquarters
San Carlos, CA
Founded
2024

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