Structures Architect — Conceptual Design

Headquartered in Silicon Valley, California, Archer is a leader in the next-gen aerospace sector building an end-to-end advanced air mobility platform that delivers air taxis, unmanned aircraft systems (“UAS”), aviation-related physical artificial intelligence (“AI”) solutions, and other technologies to customers worldwide across the commercial aerospace and defense sectors.

Our sights are set high and our problems are hard, and we believe that diversity in the workplace is what makes us smarter, drives better insights, and will ultimately lift us all to success. We are dedicated to cultivating an equitable and inclusive environment that embraces our differences, and supports and celebrates all of our team members.

THE ROLE As Structures Architect, you will develop the conceptual-level airframe architecture for a next-generation eVTOL: laying out and sizing the major structural components, evaluating alternative layouts and materials, assessing packaging and volume, and predicting weight for candidate configurations in close coordination with the vehicle, powertrain, and aero architects.

WHAT YOU'LL DODevelop conceptual-level airframe architecture and parametric structural models for the fuselage, wing, tail, and nacelle structure, including layout of the wing, fuselage, tailboom/empennage, rotor/proprotor pylon mounts, and landing gear attachment.

Size major structural components (spars, frames, longerons, skins, major fittings) using classical analytical methods, cross-sectional analysis tools such as “section properties”, and conceptual FEM.Predict and assess aeroelastic behavior at the conceptual level — including flutter and whirl-flutter margins and structural modal characteristics — using tools such as ASWING or similar beam-based aeroelastic codes.

Partner with the Vehicle Architect on loads and outer mold line (OML) definition; since structural sizing is ultimately driven by elastic, aeroelastic, and loads behavior, help identify the governing sizing cases (e.g., maneuver, gust, ground, fatigue) for each major structural element.

Evaluate and trade alternative structural layouts across candidate configurations for weight, manufacturability, and cost.

Lead material selection trades for major structural elements — composite vs. metallic vs. hybrid construction — weighing weight, cost, manufacturability, and schedule.

Assess packaging and volume allocation across the airframe (battery/fuel volume, powertrain bay, payload bay, avionics bays) in coordination with the powertrain and vehicle architects.

Generate structural weight estimates for candidate configurations and track weight margins through the concept phase.

WHAT YOU'LL NEED Aircraft structural design background at the conceptual or preliminary design level; rotorcraft, tiltrotor, or eVTOL experience strongly preferred.

Strong experience with aeroelastic analysis — including flutter and whirl-flutter prediction — and structural modal analysis.

Structural sizing methods (classical beam/panel analysis, weight-estimation relationships / CERs); experience with the section properties Python library or similar cross-sectional analysis tools a plus.

Experience with conceptual/preliminary structural and aeroelastic sizing tools such as ASWING, NeoCASS, Open Aero Struct , py Nastran, SUAVE, or similar.

Working knowledge of composite and metallic airframe construction and their trade-offs.

Strong Python programming experience for structural sizing and analysis automation.

Experience generating parametric geometry for aircraft structure — via commercial parametric CAD (e.g., CATIA, NX, Solid Works) or code-based parametric geometry tools (e.g., OpenVSP, Cad Query, custom scripting).Understanding of systems integration and packaging constraints in…