In this role you shape the structural and mechanical architecture of the Zephyr system, guiding design, validation, and certification. You work with cross‑functional teams to balance weight, strength, aeroelasticity, and manufacturability while ensuring safety and regulatory compliance. You will lead architectural trade studies and provide technical authority on structural integrity and verification. Your work supports a mission to deliver high‑altitude, long‑endurance platforms for global connectivity and sensing. This is an opportunity to influence certification strategies and drive robust, scalable aircraft architecture in a pioneering HAPS program.
Pay / Benefits
flexible working
bonus scheme
pension plan
Responsibilities
Define and maintain aircraft structural and mechanical system architecture, including primary/secondary structures and interfaces.
Lead design trades balancing weight, strength, stiffness, durability, aeroelasticity, thermal effects, and manufacturability.
Ensure integration with propulsion, avionics, and other systems.
Develop and apply top-level models to support architectural decisions and trade studies.
Lead multidisciplinary trade studies evaluating performance, mass, and operational constraints.
Provide structural authority, review designs, and guide application of analysis methods (e.g., FEA).
Define and lead structural certification strategies and interface with authorities.
Lead requirements decomposition, traceability, and participation in design reviews (SRR, PDR, CDR).
Oversee structural verification/validation, ground testing, and flight test support.
Act as key technical interface with engineers, customers, and stakeholders.
Provide technical oversight of structural suppliers and support issue resolution.
Identify and mitigate structural risks and ensure safe, compliant design margins.
Provide leadership and mentorship within the engineering team and promote best practices.
Key requirements
+10 years of experience in composite airframe structural analysis with leadership roles
Proven experience in primary structure certification against civil CS23/CS25 or equivalent
Proficiency with ANSYS and PATRAN/NASTRAN
Desirable: experience as EASA CVE/FAA DER or similar delegation
Desirable: flight test involvement
Desirable: RPAS design, integration, and testing
Bachelor’s or master’s degree in aerospace engineering or related field
Strong knowledge of static, fatigue, stability, aeroelasticity; lightweight aerospace structures
Experience with architectural trade-offs and engineering models at aircraft level
Familiarity with DOORS and JAMA; awareness of airworthiness regulations and certification frameworks
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