Stress Analysis Engineer - Level 2

Lockheed MartinFort Worth, TX
Onsite

About The Position

You will be the Stress Analysis Engineer - Level 2 for the F-35 Fuselage and MRB Stress Analysis Team which is responsible for delivering high‑fidelity structural assessments that enable safe, reliable aircraft operation. As the Stress Analysis Engineer - Level 2 you will be responsible for creating and evaluating structural models that support the F‑35 fuselage and MRB repair processes. Your responsibilities will include: Create high‑quality finite element model (FEM) meshes, post‑process FEM results, and generate stress packages to support crack correlation for the service‑life analysis team. Perform stress analysis on metallic materials, size detail parts, and assess the strength of primary and secondary aircraft structures. Support Production and Sustainment Material Review Board (MRB) repairs, ensuring discrepant parts or assemblies meet required strength standards. Conduct strength analysis to certify new and existing designs, size components, release drawings, and prepare analysis reports. Assist flight‑test instrumentation efforts by performing strength assessments using air‑vehicle FEM and spreadsheet stress analysis, providing data for service‑life evaluation of new brackets and flight‑test hardware.

Requirements

  • Bachelor's degree in an engineering technical discipline such as Mechanical, Aerospace, or Aeronautical Engineering
  • Experience with structural analysis of primary and secondary metallic airframe structure
  • MUST BE A U.S. CITIZEN
  • Ability to obtain a secret clearance

Nice To Haves

  • Experience with free-body diagrams
  • Classical hand calculations
  • Finite Element Modeling and Analysis including pre- and post-processing
  • Experience using Linux and Microsoft Operating Systems
  • Microsoft Office
  • Additional programing languages
  • Excellent written and verbal communication skills
  • Ability to collaborate in a team-based environment

Responsibilities

  • Create high‑quality finite element model (FEM) meshes
  • Post‑process FEM results
  • Generate stress packages to support crack correlation for the service‑life analysis team
  • Perform stress analysis on metallic materials
  • Size detail parts
  • Assess the strength of primary and secondary aircraft structures
  • Support Production and Sustainment Material Review Board (MRB) repairs, ensuring discrepant parts or assemblies meet required strength standards
  • Conduct strength analysis to certify new and existing designs
  • Size components
  • Release drawings
  • Prepare analysis reports
  • Assist flight‑test instrumentation efforts by performing strength assessments using air‑vehicle FEM and spreadsheet stress analysis
  • Provide data for service‑life evaluation of new brackets and flight‑test hardware

Benefits

  • Medical
  • Dental
  • Vision
  • Life Insurance
  • Short-Term Disability
  • Long-Term Disability
  • 401(k) match
  • Flexible Spending Accounts
  • EAP
  • Education Assistance
  • Parental Leave
  • Paid time off
  • Holidays
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