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Senior Staff Engineer, Structures and Vibration (6237)

Shield AI

Dallas · USD 170,000-260,000 / year · 12+ years experience · Onsite · Posted Oct 10, 2026

At a glance

Experience
12+ years experience
Workplace
Onsite
Location
Dallas
Salary
USD 170,000-260,000 / year

About the role

  • Shield AI is seeking a Senior Staff Engineer, Structures and Vibration to own V-BAT system loads and define structural requirements for subsystems, components, and suppliers.
  • The role involves leading composite structural analysis, vibration and shock environment assessments, and program-wide weight optimization reviews.
  • Candidates will serve as the bolted joint expert, mentor engineers in FEA and structural fundamentals, and present findings to engineering leadership and customers.

Responsibilities

  • Develop and maintain company structural standards, including design criteria, factors of safety and margin policy, analysis methods, material allowables, and joint design practices.
  • Own V-BAT system loads, and define structural requirements for subsystems, components, and suppliers.
  • Lead and perform static, stability, modal, dynamic, and fatigue analyses of V-BAT structures using hand calculations and FEA (Simcenter).
  • Lead composite structural analysis and define composite design requirements.
  • Serve as the bolted joint expert for the program.
  • Own vibration and shock environments. Assess existing profiles and use measured flight data to develop defensible test requirements.
  • Define and improve vibration test requirements and processes, from test planning through verification, validation, and model-to-test correlation.
  • Lead a program-wide weight optimization review of existing designs, and analyze new designs for weight efficiency and material selection.
  • Review structural analyses, test reports, and design review content, and present findings to engineering leadership and customers.
  • Mentor engineers in FEA and structural fundamentals, and build the team's structural analysis capability.

Requirements

  • B.S. in Mechanical Engineering, Aerospace Engineering, or a related discipline.
  • 12+ years of structural analysis experience on aircraft, UAS, or comparable complex system, including serving as a structural lead or technical authority.
  • Experience creating structural design criteria, analysis methods, or engineering standards.
  • Expert knowledge of structural mechanics and hand calculations, including strength, stability, fatigue, and structural dynamics.
  • Expertise with FEA tools, preferably Siemens Simcenter (Nastran or Femap), or equivalents such as ANSYS or Abaqus.
  • Significant experience analyzing composite aircraft structures and defining composite design requirements.
  • Expert-level knowledge of bolted joint analysis and design.
  • Hands-on experience with vibration and shock testing, including test planning, instrumentation, and data review, plus working knowledge of MIL-STD-810.
  • Proven track record of mentoring engineers.
  • Strong written and verbal communication skills.

Preferred qualifications

  • M.S. or Ph.D. in Mechanical or Aerospace Engineering.
  • Experience as the lead structural engineer on a Group 2–5 UAS, rotorcraft, or VTOL aircraft.
  • Experience deriving vibration environments from flight test data (PSD analysis, fatigue damage spectrum, test tailoring).
  • Experience with modal testing and FEA model correlation.
  • Experience leading structural weight reduction programs.
  • Experience developing composite allowables (e.g., CMH-17) and knowledge of composite manufacturing processes.
  • Familiarity with MIL-HDBK-516, RTCA DO-160, and aircraft structural certification.
  • Experience in startup or high-growth defense environments.

Benefits

  • Bonus
  • Benefits
  • Equity
  • temporary benefits package (applicable after 60 days of employment for temporary employees)

Skills

  • Simcenter
  • FEA
  • Nastran
  • Femap
  • ANSYS
  • Abaqus
  • MIL-STD-810
  • CMH-17
  • MIL-HDBK-516
  • RTCA DO-160

Shield AI

Senior Staff Engineer, Structures and Vibration (6237)

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