Stress Engineer

ICON Aircraft

$90K — $120K *
Aerospace & Defense
Less than 5 years of experience
Job Overview by Ladders

Qualifications

  • B.S. in Mechanical/Aerospace Engineering
  • 3+ years of stress analysis on aircraft or similar weight-critical structures
  • 2+ years using high-level CAD systems (preferably Creo)
  • Strong structural intuition for light aircraft
  • Detail-oriented with a focus on weight sensitivity
  • Practical knowledge of Design for Manufacturing

Responsibilities

  • Perform stress analysis on composite and metallic structures using hand calculations and FEA
  • Support production and field efforts by assessing damage and defining repairs
  • Verify preliminary designs produced by engineers
  • Suggest design modifications to meet functional and weight criteria
  • Write comprehensive stress reports and support compliance testing
  • Extract geometric data from CAD models

Benefits

  • Collaborative work environment
  • Opportunities for professional growth
  • Involvement in innovative aerospace projects
  • Access to advanced engineering tools and practices
  • Potential for mentorship from experienced engineers
Full Job Description
Title: Stress Analyst

Mission of Role: To perform stress analysis on primary composite and metallic structures using hand calculations and FEA.

Location: Vacaville, CA

Reports to: VP, Engineering

Primary Areas of Responsibilities:
  • Perform stress analysis on primary composite structures and metallic components using hand calculations and Finite Element Analysis (FEMAP, Nastran, linear and non-linear FEM creation and validation)
  • Support production and field support efforts. Assess damage and issues, define and substantiate repairs
  • Verify preliminary analyses of design engineers
  • Suggest design changes to meet functional, strength, and weight requirements
  • Write stress reports, structural test plans and test results. Support compliance testing
  • Extract geometry from Creo (Pro/E) CAD models

Required Experience & Education:
  • B.S. in Mechanical/Aerospace Engineering
  • 3+ years of directly applicable aircraft or similar weight critical structures, performing hand calculation stress analysis (per approved stress methods: Bruhn, Niu, etc.) and FE analysis (FEMAP/Nastran, Linear/Non-Linear analysis) on composite and metallic structures (primary and secondary)
  • 2+ years using any high-level CAD system but Creo (Pro/E) is preferred
  • Strong structural intuition for light aircraft
  • Extremely detail oriented and weight sensitive
  • Practical - good Design for Manufacturing awareness
  • Strong communication skills and highly collaborative

Ideal Experience:
  • Experience with composite material qualification or testing
  • Composite part design, layup mold design and/or bonding fixture design
  • Experience with metrology, interpretation and /or operation
  • Evaluation of technical options against schedule and budgetary constraints
  • Aerospace product and industry experience/knowledge. Aerospace tooling experience, aerospace design experience
  • Strong computer skills

Other Traits:
  • Highly intelligent - Analytical and problem solver
  • Team player
  • Good judgement
  • Extreme attention to detail
  • Self-motivated, positive thinker
  • Mature and sensitive to multiple decision-making styles
  • Ability to grasp issues in a dynamic environment and organize activities to quickly achieve desired outcomes

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