Lockheed Martin
Loads and Dynamics Analyst (Level V)
Lockheed Martin, King Of Prussia, Pennsylvania, United States, 19406
Basic Qualifications
Experience in mechanical analysis, including finite element analysis (FEA), computational fluid dynamics (CFD), or classical hand calculations
Proficiency in application of FEA principles as well as rigid and flexible body models.
Knowledge of spacecraft or aircraft structural dynamic methods and testing.
Static, vibration, acoustic, modal, or shock analysis/test experience.
Must be a US Citizen, and have the ability to obtain a Secret clearance
Job Code / Title E1415: Mechanical Engineer Sr Stf
Location King of Prussia, PA
Job Description Lockheed Martin Space is seeking an
experienced Loads and Dynamics Analyst
to join our team in
King of Prussia, PA ! As a Senior Staff Loads & Dynamics Analyst, you will serve as a technical authority for loads and dynamics across reentry systems programs. You will have the ability to lead high‑impact, innovative structural‑dynamic analyses and represent the Loads and Dynamics team in meetings with customers, DOE partners, and program management. Operating with broad discretion, you will influence long‑range plans and development strategies, guide major program milestones, and ensure that our solutions set industry standards while protecting the organization’s reputation and business objectives.
Responsibilities
Lead end‑to‑end structural‑dynamic programs for reentry flight hardware, including the development of loads, shock, vibration and acoustic environments at both primary‑structure and component levels.
Create, validate, and maintain high‑fidelity models (in‑house and commercial tools such as Abaqus, NX/Nastran, ADAMS, Wave6) that capture mechanical loading, mechanism deployment, and separation‑event responses; generate super‑element and flexible‑body models to streamline the dynamic workflow.
Define, plan, and execute test campaigns (static, modal, separation dynamics, vibration, shock) – from requirement development and test‑plan authoring through test monitoring, data‑reduction, and post‑test reporting.
Integrate analysis and test data using signal‑processing and data‑analysis software (MATLAB, Python) to produce accurate comparisons, identify discrepancies, and refine models.
Produce technical documentation and deliverables (user guides, data packages, test reports) that support peer and customer reviews; present findings to engineering teams, customers, and program office personnel at design‑review and technical‑interchange meetings.
Interpret and flow down program requirements, develop work‑breakdown plans, and oversee budget and schedule tracking to minimize cost and cycle time while ensuring compliance with organizational objectives.
Serve as the primary technical liaison for advanced dynamic‑analysis projects, providing expert advice to internal stakeholders and external customers, and driving innovation across the program.
Desired skills
A Bachelor’s or Master's degree in mechanical or aerospace program
Experience using rigid body or flexible body analysis methods
Experience with coupled loads analysis and the supererelement method (ie: Craig-Bampton)
Experience with Abaqus, NX/Nastran, Matlab, ADAMS, Wave6, and Python
Experience leading a team of analysts and collaborating with other teams and disciplines
Mechanisms, antenna, electronic component, ground support, hoisting, and test support equipment, and composite materials analysis experience
Utilize software for signal processing and post test data analysis
Ability and desire to assume ownership of tasks and drive to closure quickly and efficiently
Creativity/innovation to tackle issues related to anomalous performance of any aspect of a mechanical system
Ability to work in a collaborative and highly integrated team environment
Active Secret Clearance
EEO Lockheed Martin is an equal opportunity employer. Qualified candidates will be considered without regard to legally protected characteristics. The application window will close in 90 days; applicants are encouraged to apply within 5 - 30 days of the requisition posting date in order to receive optimal consideration.
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Experience in mechanical analysis, including finite element analysis (FEA), computational fluid dynamics (CFD), or classical hand calculations
Proficiency in application of FEA principles as well as rigid and flexible body models.
Knowledge of spacecraft or aircraft structural dynamic methods and testing.
Static, vibration, acoustic, modal, or shock analysis/test experience.
Must be a US Citizen, and have the ability to obtain a Secret clearance
Job Code / Title E1415: Mechanical Engineer Sr Stf
Location King of Prussia, PA
Job Description Lockheed Martin Space is seeking an
experienced Loads and Dynamics Analyst
to join our team in
King of Prussia, PA ! As a Senior Staff Loads & Dynamics Analyst, you will serve as a technical authority for loads and dynamics across reentry systems programs. You will have the ability to lead high‑impact, innovative structural‑dynamic analyses and represent the Loads and Dynamics team in meetings with customers, DOE partners, and program management. Operating with broad discretion, you will influence long‑range plans and development strategies, guide major program milestones, and ensure that our solutions set industry standards while protecting the organization’s reputation and business objectives.
Responsibilities
Lead end‑to‑end structural‑dynamic programs for reentry flight hardware, including the development of loads, shock, vibration and acoustic environments at both primary‑structure and component levels.
Create, validate, and maintain high‑fidelity models (in‑house and commercial tools such as Abaqus, NX/Nastran, ADAMS, Wave6) that capture mechanical loading, mechanism deployment, and separation‑event responses; generate super‑element and flexible‑body models to streamline the dynamic workflow.
Define, plan, and execute test campaigns (static, modal, separation dynamics, vibration, shock) – from requirement development and test‑plan authoring through test monitoring, data‑reduction, and post‑test reporting.
Integrate analysis and test data using signal‑processing and data‑analysis software (MATLAB, Python) to produce accurate comparisons, identify discrepancies, and refine models.
Produce technical documentation and deliverables (user guides, data packages, test reports) that support peer and customer reviews; present findings to engineering teams, customers, and program office personnel at design‑review and technical‑interchange meetings.
Interpret and flow down program requirements, develop work‑breakdown plans, and oversee budget and schedule tracking to minimize cost and cycle time while ensuring compliance with organizational objectives.
Serve as the primary technical liaison for advanced dynamic‑analysis projects, providing expert advice to internal stakeholders and external customers, and driving innovation across the program.
Desired skills
A Bachelor’s or Master's degree in mechanical or aerospace program
Experience using rigid body or flexible body analysis methods
Experience with coupled loads analysis and the supererelement method (ie: Craig-Bampton)
Experience with Abaqus, NX/Nastran, Matlab, ADAMS, Wave6, and Python
Experience leading a team of analysts and collaborating with other teams and disciplines
Mechanisms, antenna, electronic component, ground support, hoisting, and test support equipment, and composite materials analysis experience
Utilize software for signal processing and post test data analysis
Ability and desire to assume ownership of tasks and drive to closure quickly and efficiently
Creativity/innovation to tackle issues related to anomalous performance of any aspect of a mechanical system
Ability to work in a collaborative and highly integrated team environment
Active Secret Clearance
EEO Lockheed Martin is an equal opportunity employer. Qualified candidates will be considered without regard to legally protected characteristics. The application window will close in 90 days; applicants are encouraged to apply within 5 - 30 days of the requisition posting date in order to receive optimal consideration.
#J-18808-Ljbffr