Design and develop structural components for next-generation autonomous UAVs from concept through production, working cross-functionally with aerodynamics, propulsion, and manufacturing teams. Requires 7+ years aircraft structural design experience and proficiency in CAD and aerospace structures.
130k – 200k
On-site7+ YOEHardware Engineering
About the role
Responsibilities
Design and develop structural components and assemblies for next-generation UAV platform, supporting both primary and secondary aircraft structures
Execute all stages of the design lifecycle including conceptual development, initial CAD modeling, detailed design, and drawing release
Perform hand calculations for stress or strain with limited basic FEA analysis
Collaborate with aerodynamics, propulsion, avionics, payload, and manufacturing teams to support system integration across airframe interfaces
Support structural validation efforts including coupon testing, subcomponent testing, and system-level verification
Generate high-quality design documentation, drawings, interface definitions, and analysis reports in compliance with aerospace standards
Partner with manufacturing and flight test teams to resolve build issues and support hardware through test and deployment
Participate in design reviews and technical discussions
Requirements
Bachelor's or Master's degree in Mechanical Engineering, Aerospace Engineering, or related discipline
7+ years of experience in aircraft structural design or closely related aerospace structures
Experience designing and releasing structural components in development or production environments
Working knowledge of composite and metallic structures, including fasteners, bonded joints, and load paths
Proficiency in CAD tools (NX, CATIA, SolidWorks, or similar)
Understanding of GD&T, tolerance stackups, and DFMA principles
Strong written and verbal technical communication skills
Demonstrated ability to operate in fast-paced, high-ownership engineering environments
Nice-to-Haves
M.S. degree in Aerospace or Mechanical Engineering
Experience supporting UAV, DoD, or aerospace vehicle programs
Familiarity with aerospace standards (MIL-STD, ASME Y14.5, FAA)
Experience supporting hardware through test, failure analysis, and design iteration
Exposure to composite design and manufacturing methods
Experience using FEA tools (ANSYS, Abaqus, NASTRAN, or similar) for linear structural analysis
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