Support the design and certification of aircraft interior monuments, performing structural analysis, certification substantiation, and load development.
Compensation
The salary range for this role is 95,500 USD - 181,700 USD.
Responsibilities
Perform structural analyses of aircraft interior monuments and supporting interfaces
Develop and execute finite element models to evaluate strength, stiffness, stability, and durability
Generate and validate interface loads between monuments and aircraft primary structure
Perform static and dynamic analyses for various load conditions
Support qualification and certification test programs
Requirements
Bachelor's or Advanced Degree in STEM
Nice to have: FAA Part 25 familiarity
Nice to have: decompression and emergency landing knowledge
Nice to have: inertial load knowledge
Nice to have: composite and metallic aircraft structures
Aerospace Stress Engineer focused on the analysis, certification, and testing of composite and metallic primary structures.
Responsibilities
Stress analysis of composite primary structures
Conduct detailed stress analysis using both classical hand calculation methods (e.g., Bruhn, Peery, Roark, ESDU) and Finite Element Analysis (FEA) tools
Prepare and author certification stress reports; collaborate with FAA Designated Engineering Representatives (DERs)
Clearly communicate and justify analysis methods, assumptions, and results to both internal teams and external stakeholders
Requirements
Bachelor’s degree in aerospace or mechanical engineering
Define, analyze, and validate the loads environments that drive structural design for Project Ranger.
Compensation
Pay within range listed + Bonus + Benefits + Equity
Responsibilities
Develop air vehicle and component level loads analyses for primary and secondary structures.
Create and maintain loads models, free body diagrams, load paths, load cases, design envelopes, and critical load conditions that inform structural sizing, design decisions, and verification planning.
Partner with Aerodynamics, Flight Controls, Mass Properties, Propulsion, and Systems Engineering to define external loads, inertial loads, aerodynamic loads, actuator loads, interface loads, and vehicle operating conditions.
Deliver clear loads documentation, including design load reports, interface control loads, critical condition summaries, assumptions, margins, and recommendations for use by structures, test, and certification stakeholders.
Support ground and flight test planning, instrumentation definition, correlation activities, structural test execution, and post test data analysis to validate models and refine structural loads predictions.
Requirements
Bachelor’s or Master’s degree in Aerospace Engineering, Mechanical Engineering, or a related technical discipline
Nice to have: Master’s degree in Aerospace or Mechanical Engineering with emphasis in structural dynamics, aeroelasticity, aircraft loads, flight mechanics, or a related field
Senior Engineer, Structural Analysis (R6027)
f7d8749a-72d6-407c-bf98-292ea630c73a · Posted Oct 14, 2026
Shield AI is seeking a Sr. Structural Analyst to support the analysis and testing of advanced UAVs, focusing on the structural integrity of lightweight, high-performance aircraft.
Compensation
Pay within range listed + Bonus + Benefits + Equity
Responsibilities
Assist in building and refining finite element models (FEM) to evaluate the structural performance of UAV components.
Perform static, modal, fatigue, and vibration analyses to assess stress, deformation, and durability.
Conduct hand calculations to validate FEA results, ensuring accuracy and structural reliability.
Work with design engineers to optimize airframe structures, balancing weight, strength, and manufacturability.
Support the development of test plans for structural validation, including quasi-static, vibration, and shock testing.
Nice to have: Experience supporting uncrewed aircraft, fixed wing aircraft, rotorcraft, defense, space, or other aerospace vehicle development programs
Nice to have: Experience developing or correlating loads models using flight test, ground test, structural test, strain gauge, pressure, acceleration, or other instrumentation data
Nice to have: Familiarity with aeroelasticity, flutter, dynamic response, vibration, fatigue, durability, damage tolerance, or nonlinear structural analysis methods
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