✨ About The Role
- This position involves developing and validating internal loads finite element models for lunar transportation systems.
- The role requires performing static, dynamic, buckling, and modal analysis of space vehicle primary structures.
- The candidate will need to accurately model boundary conditions and external loads for all flight events throughout the mission.
- Responsibilities include compiling and presenting organized internal loads data sets with clear documentation.
- The position requires regular collaboration and communication with NASA and National Team Partners as part of the Human Landing System program.
âš¡ Requirements
- The ideal candidate will have a minimum of 10 years of experience in finite element analysis (FEA) within aerospace applications.
- A strong foundation in static and dynamic structural engineering fundamentals is essential for success in this role.
- The candidate should possess a deep understanding of aerospace FEA modeling techniques and be able to solve complex structural problems.
- Excellent communication skills are necessary to collaborate effectively with various engineering teams.
- A commitment to quality and safety in human spaceflight is crucial, along with a passion for the mission of enabling human presence in space.