Principal Aircraft Structures Design Engineer/Aerostructures Lead (R2977)
Shield AI
What you'll do:
- Lead the structural design architecture for the next-gen UAV, owning conceptual and preliminary structural configuration down to detailed design of primary and secondary load-bearing assemblies.
- Oversee the development of composite and metallic structures, optimizing for performance, weight, cost, manufacturability, and mission flexibility.
- Act as a technical mentor and design authority, coaching structural engineers and ensuring consistent design practices, review standards, and execution quality across teams.
- Collaborate with aero, GNC, propulsion, payload, and manufacturing teams to define interface and integration requirements for structures under real-world mission conditions.
- Integrate simulation-driven design workflows and validation methodologies, incorporating FEA, load path optimization, fatigue, and environmental constraints early in the design cycle.
- Provide hands-on support to prototype builds, manufacturing integration, and flight test activities, helping to resolve structural challenges in real time.
- Drive adoption of model-based development and digital engineering tools within the Siemens (NX, Teamcenter) environment.
- Partner with supply chain and manufacturing to ensure structural designs are ready for scalable production with clear specs, tolerances, and fabrication plans.
- Lead and support design reviews, failure investigations, corrective actions, and documentation efforts aligned with airworthiness and mission safety standards.
Required qualifications:
- Bachelor’s or Master’s degree in Aerospace Engineering, Mechanical Engineering, or a related field.
- 10+ years of experience in aircraft structural design, with at least 3 years in a technical leadership or mentorship capacity.
- Proven expertise in composite and metallic airframe structures, including bonding, bolted joints, sandwich panels, and repairability.
- In-depth understanding of structural analysis, including kinematics, dynamics, load paths, and stiffness/fatigue behavior.
- Proficiency in CAD (NX, CATIA, or SolidWorks) and familiarity with FEA tools (e.g., NASTRAN, ANSYS, or HyperWorks).
- Experience working within or alongside certification processes and airworthiness standards (FAA Part 23/25, MIL-HDBK, etc.).
- Demonstrated track record of delivering structurally sound, test-validated airframes from clean-sheet design through prototype or production.
Preferred qualifications:
- Experience with automated composite manufacturing (AFP, ATL), additive manufacturing, or advanced joining technologies.
- Hands-on experience with structural validation testing, including static, dynamic, fatigue, and thermal/environmental testing.
- Familiarity with aero-structural interaction, including aerodynamic performance, control surface loads, and thermal/aeroelastic effects.
- Exposure to digital engineering practices, model-based design workflows, or PLM integration (e.g., Siemens Teamcenter).
- Prior work on UAV, high-performance, or unconventional airframes in defense or advanced aerospace programs.