Saratech is seeking a Senior Stress Engineer to support our client. The Stress Engineer II will support both vehicle design/build and flight test operations directly, via hands on assessment and analytical substantiation of vehicles in a fast-paced, multi-disciplinary environment.
You will be involved in both build and vehicle operations phases of programs. Stress Engineers interface and collaborate with other disciplines, including but not limited to: Structures Design, Maintenance & Operations teams, Manufacturing, Propulsion, Flight Test and more to provide design substantiation, test support, and operations support. Maintain focus on timeliness and execution of tasks and deliverables every day.
- Perform structural analysis using classical methods and finite element analysis to provide analytical definition and/or ensure structural integrity of components, assemblies, and systems
- Develop and/or utilize finite element models (global and discrete)
- Review, update, and create engineering analytical definition of components, assemblies, and systems (analysis documentation)
- Prepare clear and concise reports that collect, analyze, and summarize information
- Play an integral role in the workflow release process for structural design
- Support review of manufacturing plans and procedures to ensure compliance with design and load requirements
- Support the creation of structural component and system test plans which will be used to verify manufacturing and testing
- Develop standardized analysis criteria and templates
- Work independently for moderate periods under guidance of senior engineers and produce work that meets industry and company standards, tolerances, weight and cost targets
- Coordinate with various engineering stakeholders during the design, production, integration, test, delivery, and operation of air/space vehicles
- Adhere to set directions and guidelines from team leader to support collaboration across teams to complete project
- Mentor more junior team members
| Location | Las Cruces, NM |
| Job Type | Full-time |
| Salary | $135,000–$140,000 Per Year |
Required Skills and Experience:
- 8 years of experience and a Bachelor's degree in a relevant Engineering discipline; or 3 years and a master's degree; or a PhD without experience; or equivalent work experience
- Minimum of 3 years prior experience in structural analysis of aerospace primary structure
- Solid understanding of material properties and behavior, statistics/free body diagrams, and structural load paths
Preferred Skills:
- Familiarity with classical aerospace sizing methods (Bruhn, Niu, Roark, etc.)
- Knowledge of composite aircraft structural analysis and familiarity with industry standards for the manufacture, repair, and assembly components
- Previous experience with Finite Element Modeling and Analysis
- Previous experience with FEMAP, HyperX, TMP Slim/Vision, NASTRAN
- Familiarity with CAD software to design aircraft/spacecraft structures and components
- Knowledge of and/or experience with Fatigue and Damage Tolerance
- Familiarity with MRB tasks associated with dispositioning non-conformant metallic and composite components resulting from manufacturing, assembly, or field operations
- Experience with manufacturing-based Enterprise Resource Planning (ERP) systems, such as Oracle
- Experience with Product Lifecycle Management tools (PLM software), requirements management tools, and configuration management
- Experience with the design of flight vehicles or vehicle systems to a set of requirements or standards such as CFR 14, Part 400, Part 23 and 25, military or NASA is highly desired
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