Structural Analyst III

Overview

Application close date:
Applications will be accepted on an ongoing basis until the requisition is closed.

At Blue Origin, we envision millions of people living and working in space for the benefit of Earth. We're working to develop reusable, safe, and low-cost space vehicles and systems within a culture of safety, collaboration, and inclusion. Join our team of problem solvers as we add new chapters to the history of spaceflight!

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.

As part of a hardworking team of engineers, designers and specialists you will perform analysis of structural subsystems for New Glenn's first stage stage using classic hand calculations as well as Finite Element Model (FEM) simulations to support design, manufacturing and operations. A thorough understanding of structural analysis and load path is required as we strive for a weight optimized design.

As we transition from the initial design, release and qualification testing of the flight hardware to the production and operational phase you will be responsible for supporting production issues, ongoing testing and mission operations.

We are looking for someone to apply their technical expertise, leadership skills, and commitment to quality to positively impact safe human spaceflight. Passion for our mission and vision is required!

Special Mentions
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• Relocation may be provided
• Travel expected up to 15% of the time
• Interviews will include a technical assessment

• Detailed hand calc and FEM analysis of primary and secondary aerospace structures for production support and sustainment initiatives
• Drive hardware discrepancies to resolution including dispositioning of manufacturing nonconformances
• Documentation of stress analysis to support release of engineering drawings / documents
• Deep understanding of repair methods and analytical practices for both metallic and composite structure
• Ability to perform technical assessment of damage or out of tolerance conditions and provide guidance on repair or use
• Providing technical guidance on design concepts (risk vs. cost vs. performance)
• Maintain and report on technical status
• Participate in subsystem test planning, execution, data reduction and analysis.
• Prepare technical content and present to internal and external customers
• Supporting cross organizational teams with input for production activities and configuration development
• Analysis checks for designers and junior structural analysts in stress/stability/fracture analysis and best practices
• Improving enterprise analysis capabilities such as creating process automation tools for model creation, strength checks, and analysis report generation

• Minimum of a B.S. degree or higher in aerospace engineering, mechanical engineering, or related field.
• 6+ years of experience within the fields of aircraft, spacecraft, or launch vehicle structures
• Experience with analyzing / dispositioning non-conformances
• Complete hand calculations including free-body diagrams for internal and reaction load derivation
• Bolted joint calculations (bolt preload, joint stiffness, shear-tension interaction, insert pull-out, etc.)
• Knowledge of engineering materials and their applications to achieve optimal structures
• Strong experience with classical and aerospace analysis methods (Bruhn, Niu, Roark, Blodgett, Mark's Shigley, etc.)
• Demonstrated knowledge of vehicle load path and stress analysis of metallic and/or composite structures (pressure vessels, skin-stringer, fittings, sandwich panels, etc.)
• Demonstrated expertise with at least two of the following analysis codes:
  Ansys, Nastran, Optistruct, LS Dyna, Hypermesh, Hypersizer, NASGRO, Abaqus
• Demonstrated experience using scripting languages (VBA, Matlab, Python, FORTRAN, etc.)
• Understanding of FEM modeling techniques (boundary conditions, bolted connections, contact, verification methods, etc.)
• Mesh…