Senior Mechanical Engineer (Stress Analysis Level 3)

Standard Job Description 
 Space is a critical domain, connecting our technologies, our security and our humanity. While others view space as a destination, we see it as a realm of possibilities, where we can do more — we can innovate, invest, inspire and integrate our capabilities to transform the future. At Lockheed Martin Space, we aim to harness the full potential of space to cultivate innovation, reduce costs, and push the boundaries of what technology can achieve. We’re creating future-ready solutions, focusing on resiliency and urgency through our 21st Century Security® vision. We’re erasing boundaries and forming partnerships across industries and around the world. We’re advancing spacecraft and the workforce to fuel the next generation. And we’re reimagining how space can connect us, ensuring security and prosperity. Join us in shaping a new era in space and find a career that's built for you. Come join our team as our next Orion Stress Analyst! Your duties will include the providing on-site stress analysis and structural test support of flight hardware as part of the Orion Production Engineering team. Tasks will include providing timely stress analyses to guide the development of design changes, assist with verification and validation of evolving mission requirements, disposition of flight hardware discrepancies, leading acceptance tests of composite and metallic structures, and coordinating with the Engineering team to develop problem resolutions in support of ATLO. Other duties may include: Perform stress and fracture analyses in support of Engineering release Coordinate with Loads & Dynamics on component and structures environments Support structural qualification testing Coordinate with Systems Engineering on verification tasks Generate performance metrics and status reports for Program Management Researches, plans, designs and develops mechanical products and systems such as instruments, controls, robots, engines, machines and mechanical, thermal hydraulic or heat transfer systems for production, transmission, measurement, and use of energy. Applies research to the planning, design, development, and testing of mechanical and/or electromechanical systems, instruments, controls, engines, and/or machines. Basic Qualifications 
 Bachelor’s degree from an accredited college or university in a related field, or equivalent combination of education and experience Experience with FEMAP finite element model pre/post processor Advanced knowledge of and experience with NASTRAN finite element solver Proven experience leading and mentoring junior engineers with spacecraft structural analysis methods Knowledge of structural characteristics and mechanical joints with ability to determine detailed load paths through complex systems Ability to apply new and advanced analytical techniques necessary to perform structural analysis US Citizenship required for this role Desired Skills 
 A Master's degree is strongly preferred for this position Hardware experience, including design, analysis, assembly, Integration and Test Knowledge of human rated structural verification requirements of spacecraft structures Experience with NASA’s Fracture Control system Experience performing crack growth analysis with NASGRO Experience in manufacturing environment and dispositioning of discrepant hardware Experience with static structural testing Experience performing fatigue analysis Experience analyzing composite material systems Experience with TMP Slim/Vision Knowledgeable of, and possesses experience with, NASA’s Artemis Program Experience using EPDM Windchill Demonstrated ability to manage multiple assignments and customers, simultaneously and independently Excellent verbal/written communication, presentation and interpersonal skills with technical and non-technical audiences US Citizenship required with the ability to obtain or maintain a Secret security clearance Proficient in AI prompting as it applies to this