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Structures Engineer

2018-03-14 12:25:21| Space-careers.com Jobs RSS

The candidate we are looking for will be able to fulfil the following duties Design and Configuration Ensure the interface between the CAD systems and the relevant FEM tools to enable further evaluation of the structural behaviour. Support spacecraft and launcher configuration studies for ESA Agency projects. This includes operating CAD tools and participation in Concurrent Design Facility CDF sessions at ESTEC. Ensure CAD interfaces and configuration data transfer with ESA contractors via international standards. Structures Static, BucklingStability, ThermoElastic Analysis Support the generation and setup of structural mathematical models using the finite element method for structural analysis problems for ESA funded projects, taking into account the specific objectives of such analysis, covering all structural materials applied in spacecraft and launchers. Where necessary nonlinear approaches and specific solution sequences shall be applieddeveloped e.g. Nastran SOL 600, Mecano, Abaqus. Perform the analysis, evaluate critically the results and issue relevant documentation covering all analysis steps. Support the generation and setup of mathematical models for structural elastic stability problems for Agency funded projects, taking into account specific requirements attached to this type of analysis. Structural Dynamics Analysis and Vibration Test Data Evaluation Structural Dynamics Support the generation and setup of structural dynamic mathematical models for spacecraft and launchers of Agency funded projects using the finite element method. Heshe shall take into account the specific objectives of such analysis and where necessary nonlinear approaches shall be considered and specific solution sequences e.g. Nastran DMAPS shall be developed. Perform the analysis modal, frequency and transient responses, random responses, preliminary inhouse launcher spacecraft coupled analysis, evaluate critically the results and issue relevant documentation covering all analysis steps. Dynamic Test Data Analysis and Correlation Support the preparation and execution of mechanical tests modal survey, sine, random, acoustics, microvibration, shock, etc for spacecraft launchers of Agency projects by performing andor reviewing analytical predictions and procedures. Perform modal identification of the test data, evaluate critically the results and make usage of these results for updating structural finite element models. Perform assessments of shock response data. The candidate should have A Masters degree or equivalent in mechanical or aeronautical engineering. Relevant experience within the field of spacecraft and launcher structures design, analysis, verification and testing. Good knowledge in space system engineering, and space engineering standards ECSS. Knowledge and experience of structures numerical analysis tools such as Nastran, Patran, Abaqus, ESACRACK etc Good interpersonal and communication skills. Ability to work effectively, autonomously and cooperatively in a diverse and international team environment, defining and implementing solutions in line with team and individual objectives, as well as project deadlines. Preference will be given to candidates eligible for an EU or national personal security clearance at the level of CONFIDENTIAL or above

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