Loads and Dynamics Senior Engineer

Lockheed Martin•Huntsville, AL

16h•Onsite

About The Position

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. As an NGI Senior Loads & Dynamics engineer you will:

Requirements

Bachelor's degree in Engineering or relevant technical field; or combination of relevant education/experience
Knowledge and/or experience with static and structural dynamics analysis of spacecraft, aircraft, or missiles
Demonstrated experience with ADAMS Multibody dynamics software, NX Simulation, NASTRAN, LS-Dyna, Wave6, or equivalent
Experience in programming and use of MATLAB (or equivalent) for analysis and data manipulation
Active Secret security clearance; US citizenship is required

Nice To Haves

Master’s degree in Mechanical Engineering/Structural Mechanics program or equivalent from an accredited college/university or equivalent experience with minimum 5 years dynamics experience
Understanding of missile and/or spacecraft structures, statics, strength of materials, structural dynamics principles, and methods
Experience evaluating designs using rigid body or flexible body analysis methods and tools
Experience with modern substructure modeling, assembly, and component mode synthesis methods such as Craig-Bampton sub structuring
Proficiency in Finite Element Modeling, modal analysis techniques, and model correlation/verification
Proficiency with structural analysis of composite structures, metallic structures, and mechanisms
Experience in Coupled Loads Analysis (CLA) on spacecraft/launch vehicles
Experience in the planning and execution of static, vibration, acoustic, modal, and shock tests for aerospace flight hardware
Demonstrated ability to collaborate effectively with adjacent disciplines (e.g. systems engineering, aerodynamics, stress analysis, design, test) in a highly integrated team environment
Ability and desire to assume ownership of tasks and drive to closure quickly and efficiently

Responsibilities

Perform structural dynamic analyses for spacecraft flight hardware
Produce and maintain models generated from both in-house and commercially available software codes that simulate mechanical loading conditions, dynamic environments (shock and vibration), and mechanism motions
Perform loads development (primary/secondary structure and component level), shock and vibration environments determination, component and system level testing, and data evaluation
Document analysis results in formal reports and presentations that are clear, adequately detailed, and timely
Define and integrate requirements into the system baseline
Prepare test plans/requirements for: static, separation dynamics, vibration, modal, and shock tests. Analyze and document the results in post-test reports
Present analysis and test results at program reviews such as Design Reviews, Technical Interchange Meetings, Engineering Review Boards, and Test Readiness Reviews