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Staff Loads Engineer (R4722)

Leads development and analysis of aerodynamic and structural loads for next-gen air vehicles, including maneuver, gust, and ground loads. Collaborates with aero, GNC, and structural teams; requires 8+ years experience and proficiency in NASTRAN, FEMAP, MATLAB.

137k – 205kDallas, TXSan Diego, CAHardware EngineeringOnsite8+ YOE

About the role

What you'll do

  • Own the development of aerodynamic and structural load envelopes for the full vehicle, from clean-sheet through flight test
  • Lead maneuver, gust, landing, and ground loads analyses, including both quasi-static and dynamic cases
  • Coordinate closely with GNC, aero, and structural teams to define load cases tied to mission profiles and flight control behaviors
  • Develop and validate loads models using tools like NASTRAN, FEMAP, MATLAB, or custom Python/Simulink scripts
  • Support the sizing and analysis of critical structural components through detailed load maps and V-n diagrams
  • Conduct aeroelastic stability assessments, including divergence and control reversal checks
  • Lead traceability of loads inputs/outputs across ICDs, FEA models, and design justification documents
  • Interface with test engineering to support strain gauge placement, instrumentation plans, and correlation of in-flight data
  • Author and present loads documentation for reviews, compliance, and technical buy-in
  • Support the long-term refinement of loads methodologies and automation across the aerostructures team

Required qualifications

  • Bachelor’s or Master’s degree in Aerospace Engineering, Mechanical Engineering, or related field
  • 8+ years experience performing loads and aeroelastic analysis for aircraft (manned or unmanned)
  • Proficiency with loads modeling tools such as FEMAP, NASTRAN, MATLAB, or other relevant simulation environments
  • Strong understanding of aircraft flight envelopes, control surface effects, and structural load paths
  • Demonstrated experience supporting both design and test phases with accurate load predictions
  • Excellent documentation, cross-functional collaboration, and communication skills

Preferred qualifications

  • Experience on UAV, eVTOL, or tactical military platforms
  • Familiarity with MIL-A-8860, FAR Part 23/25 loads regulations, or similar certification standards
  • Knowledge of aeroelastic stability, load alleviation, and adaptive control
  • Experience developing internal tools or automation for loads generation and reporting
  • Active or previous DoD clearance (not required)

Skills

NastranFemapMATLABPythonSimulinkAeroelastic AnalysisLoads AnalysisFEAGncV-N Diagrams

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