The role
Creation of mathematical structural models using the finite element method (FEM). Carrying out static and dynamic analyses of satellites and their subsystems. Condensation of finite element models using the Craig-Bampton method. Bolted joints verification according to ECSS-HB-32-23 and VDI-2230. Definition of test plans and procedures, perform test predictions and test-model correlations. Collaboration with mechanical design, thermal and system engineers. Contribution to technical exchanges with suppliers and customers. Development of internal tools for the evaluation and post-processing of the analysis and test results. Development and implementation of standards and procedures. Preparation of structural analysis and test documentation. Presentation of the results internally and to the customer.
What we expect
- Master’s degree in Aerospace, Mechanical engineering or similar qualification.
- At least 10 years of professional experience in the fields of static and dynamic analyses of spacecraft/launcher structures.
- Practical experience using Altair HyperWorks and MSC/Simcenter Nastran is an advantage.
- Basic proficiency with one or more programming languages such as Python and MATLAB.
- Good written and verbal communication skills.
- Organized, autonomous and attentive to detail.
- Team player capable of integrating into a multicultural team.
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careers.reorbit.space/jobs/8613954-senior-structural-analysis-engineer