Lead design, analysis, and system trade studies to determine optimal architecture for satellite structures and launch vehicle adapters.
Execute design and evaluation of assigned projects using sound engineering principles and program requirements.
Develop structural configurations, testing requirements, materials, processes, and tools.
Create and maintain mechanical/structure design documentation: analysis reports, interface control drawings, test procedures, and manufacturing drawings.
Prepare and present design and readiness reviews to management and peers.
Troubleshoot anomalies, perform root-cause analysis, and implement resolutions.
Collaborate with manufacturing to ensure efficient transfer of design information.
Champion new technologies and methods to improve design and production.
Communicate effectively with multidisciplinary teams to support integration and testing.
Requirements
Master’s degree in mechanical engineering or related technical field.
A minimum of 15 years of hands-on experience in mechanical design, integration, and testing of spacecraft and launch vehicle structures.
Expertise in stress and static load testing for satellite or launch vehicle structures.
Familiarity with design for manufacturability and on-orbit environments.
Experience with Autodesk Inventor (preferred) or other CAD tools such as CATIA, SolidWorks, CREO.
Benefits
Equal Opportunity Employer
Employment governed on the basis of merit and qualifications