Sr Structural Design Engineer - Glenn

This role supports the development and operations of New Glenn, a single-configuration, heavy‑lift orbital launch vehicle capable of routinely carrying people and payloads to low‑Earth orbit, geostationary transfer orbit, cislunar, and beyond. Its first stage is fully reusable, and the vehicle was designed from the beginning to be human‑capable.

• Lead a design team through frequent hardware design cycles and advise them on technical design, analysis, qualification, testing, manufacturing, and integration activities.
• Foster open communication and present to all levels of leadership within the organization.
• Drive solutions forward and advise the team on problem resolution.
• Take ownership of the full lifecycle of hardware from requirements definition through concept development, design, analysis, testing, qualification, and integration onto a launch vehicle.
• Design, analyze, develop, and test primary and secondary metallic and composite structures.
• Perform research, develop concepts, and run trade studies.
• Build 3‑D models, detail part drawings, assemblies, installations, and interface control documents.
• Build test plans, specifications, and other documentation for the development of flight hardware.
• Provide technical guidance and on‑site support for manufacturing, production, and integration activities.
• Support configuration development and trade studies.
• Take ownership of test planning, execution, data reduction, analysis, and authoring of test reports.
• Work with multi‑functional teams that are responsible for selecting materials, manufacturing processes, and suppliers to produce world‑class aerospace hardware.
• Develop component specifications and manage suppliers.
• Plan, coordinate, conduct tests, and review test data.
• Participate in the development and purchase of new equipment and tooling.
• Maintain and report on activity schedule, budget and technical status.
• Coach, mentor and technically assist other engineers.
• Find opportunities for improvements and operational cost savings.
• Work with spacecraft customers in a technical capacity.
• Own spacecraft structural integration cycles.
• Drive hardware discrepancies to resolution.
• Prepare technical content and present to internal and external customers.
• Complete hand calculation and FEM analyses to report margins of safety for primary and secondary aerospace structures.
• Perform access studies, loss of clearance analyses, vehicle clocking studies, and develop solutions to mission unique requirements.
• Collaborate with internal and external teams throughout design, manufacturing, and mission integration.

• Minimum of a B.S. degree in engineering and 10+ years of experience with aircraft, spacecraft, or launch vehicle structures.
• Experience on recently developed aircraft or launch vehicles in one or more of the following areas: vehicle load‑path distribution, first‑order strength assessment and sizing; skin‑stringer and sandwich panel design; material selection, compatibility and manufacturing techniques.
• Experience working in a multi‑functional organization to develop designs and produce world‑class engineered products.
• Strong understanding of composite and metallic design fundamentals.
• Experience in bolted joint design and analysis.
• Experience with Geometric Dimensioning and Tolerance analysis (ASME Y14.5).
• Familiarity with ASME Y14.100 and Y14.41.
• Structural design experience using CAD (Creo/Windchill preferred), hand calculations, and FEA (ANSYS preferred) tools.
• Ability to take ownership of the hardware lifecycle from requirements definition through concept development, design, analysis, testing, qualification, and integration onto a launch vehicle.
• Strong written and verbal communication skills.

• Dynamic separation systems and interface design.
• Experience with rapid development techniques for hardware.
• Experience with fabrication using automated fiber placement (AFP) and tape laying (ATL).
• Experience or expertise with fabrication of large‑scale out‑of‑autoclave composite structures.
• Demonstrated experience developing manufacturing processes for transition to production.
• Knowledge of systems engineering practices, fabrication…