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Structures Engineer
2021-07-13 16:14:04| Space-careers.com Jobs RSS
Aurora is an established supplier of skilled manpower to ESA and in particular at ESTEC and ESAC. Aurora has the opportunity to expand our support to ESA in the domain of SMT Structures, Materials, Mechanisms and Thermal Engineering. We are looking for a Structures Engineer to support the Structures Section in the Directorate of Technology, Engineering and Quality TEC. Happiness of our employees has proven key to obtaining excellent results and a client who also regards us highly for excellent service. Overview Structures Static, BucklingStability, ThermoElastic Analysis. Support the generation and setup of structural mathematical models using the finite element method for structural analysis problems for Agency 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. Perform stability analysis leading to the determination of buckling loads and deformations. Where necessary the post buckling behaviour shall be addressed, adequate nonlinear approaches used, and where relevant specific solution sequences shall be developed. Evaluate critically the results, and issue relevant documentation covering all analysis steps. Support the generation and setup of mathematical models for structural thermoelastic stability problems for Agency funded projects, taking into account specific requirements attached to this type of analysis. Perform the interpolation of the temperature maps as resulting from thermal analysis for their employment in finite element structural analysis. Perform thermoelastic analysis leading to the determination of loads and deformations, evaluate the outcome in terms of margins of safety and stability budgets, evaluate critically the results and issue relevant documentation covering all analysis steps. Where necessary nonlinear approaches shall be considered and specific solution sequences shall be developed. Evaluate critically the results and the loads and issue relevant documentation. Design and Configuration Support spacecraft and launcher configuration studies for Agency projects. This includes operating CAD tools and participation in Concurrent Design Facility CDF sessions at ESTEC. Perform mass, inertia and balance calculations and relevant budget assessments. Issue relevant documentation covering all configuration definition aspects, and where necessary shall support the configuration definition by preliminary structural analyses using FEM models. Ensure CAD interfaces and configuration data transfer with Agency contractors via international standards. Ensure the interface between the CAD systems and the relevant FEM tools to enable further evaluation of the structural behaviour. Contribute to the further development of the Structures and Configuration tools deployed in the Agency, including in the CDF. Support progress meetings and reviews in support to Agency projects. Support the updating and maintenance of CAD and FE models databases. Support and contribute to the establishment and maintenance of relevant Structures Engineering Standards and Handbooks. Dynamic Test Data Analysis And Test 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. Take into account the specific objectives of such analyses and where necessary nonlinear analyses shall be performed and specific solution sequences shall be developed. Issue relevant documentation covering all analysis steps. Where applicable produce advanced reduced dynamic mathematical models. Specific qualification requirements 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. Proactive attitude to solving problems. Good organisational skills. A very good working knowledge of spoken and written English is essential. Legal and Security Requirements All applicants must be legally allowed to work in The Netherlands Applicants are required to provide a copy of their passport and degree certificate. Aurora will validate the Degree with the issuing University and provide evidence to ESA. Prior to issuing a letter of employment the applicant shall provide to Aurora a recent official document declaring that they are of good conduct from the country where currently resident. Location The work will be performed at the European Space Technology and Research Centre ESTEC at Noordwijk, The Netherlands. Contract The selected candidate will receive good remuneration in line with ESA Job Class. Will be registered for both social security and tax in the Netherlands. The standard working hours are 40 per week. There are 12 public holidays and an additional 30 annual days holiday. Training to improve efficiency and provide strength for future career are of course included. Aurora assist with relocation both with support and financially. Aurora contributes to a company pension scheme. To be considered for this Position Prior to 17 August 2021, please apply via our Job Application form quoting TECSMT744 RTCTECMSS00744 as reference. Aurora will agree conditional employment terms and conditions with candidates before presenting them by 19 August 2021, 13.00 hours.
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structures engineer
engineer structures
Structures Engineer
2021-07-09 17:13:38| Space-careers.com Jobs RSS
Structures Engineer Deadline for submission to the Client 18082021 Client and Location The European Space Agency is ATGs biggest client. They are an international organization with 22 member states with sites in the Netherlands, Germany, Spain, France, Italy, UK and Belgium. ESA is Europes gateway to Space! Job Description We are looking for a Structures Engineer on behalf of the European Space Agency ESA for their location in Noordwijk, The Netherlands, to join their Structures Section. Please note, the successful candidate will be employed by ATG Europe and not by ESA. The successful candidate will be tasked with, but not limited to Tasks and Responsibilities Support the generation and setup of structural mathematical models using the finite element method for structural analysis problems for Agency 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 Perform stability analysis leading to the determination of buckling loads and deformations. Where necessary the post buckling behaviour shall be addressed, adequate nonlinear approaches used, and where relevant specific solution sequences shall be developed Evaluate critically the results, and issue relevant documentation covering all analysis steps Support the generation and setup of mathematical models for structural thermoelastic stability problems for Agency funded projects, taking into account specific requirements attached to this type of analysis Perform the interpolation of the temperature maps as resulting from thermal analysis for their employment in finite element structural analysis Perform thermoelastic analysis leading to the determination of loads and deformations, evaluate the outcome in terms of margins of safety and stability budgets, evaluate critically the results and issue relevant documentation covering all analysis steps. Where necessary nonlinear approaches shall be considered and specific solution sequences shall be developed Evaluate critically the results and the loads and issue relevant documentation Support spacecraft and launcher configuration studies for Agency projects. This includes operating CAD tools and participation in Concurrent Design Facility CDF sessions at ESTEC Issue relevant documentation covering all configuration definition aspects, and where necessary shall support the configuration definition by preliminary structural analyses using FEM models Ensure CAD interfaces and configuration data transfer with Agency contractors via international standards Ensure the interface between the CAD systems and the relevant FEM tools to enable further evaluation of the structural behaviour Contribute to the further development of the Structures and Configuration tools deployed in the Agency, including in the CDF 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 Take into account the specific objectives of such analyses and where necessary nonlinear analyses shall be performed and specific solution sequences shall be developed Issue relevant documentation covering all analysis steps. Where applicable produce advanced reduced dynamic mathematical models. Requirements Masters degree or equivalent in mechanical or aeronautical engineering Minimum 4 years of relevant experience within the field of spacecraft and launcher structures design, analysis, verification and testing Experience with Structures Static, BucklingStability, ThermoElastic Analysis Experience with spacecraft configuration would be an asset Experience with CATIA would be an asset Experience with dynamic analysis and test correlation would be an asset 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. Fluency in English is mandatory knowledge of another European language is an advantage. What do we offer? ATG offers excellent working conditions and provide you with all the other necessary means to further your career. We believe that training and education, combined with regular assessments and a personal development plan, will create the best environment for growth. If needed, we also assist you with settling in your new home or finding the right school for your children. ATG will help in any way it can, including a relocation budget that is applicable for ATG staff as well as employees working at one of our clients. About ATG Europe Today, ATG is recognized as a leading provider of specialized engineering, scientific and technical services to the European Space industry. Our headquarters is located in Noordwijk, the Netherlands and we have subsidiaries in Germany, Ireland and the UK. Besides these countries, ATG also operates in Spain, Italy, France and Belgium. ATG People is the key player in delivering highly educated personnel for RD environments throughout Europe. We are continually recruiting experienced Engineers for exciting, fulltime positions based at our customers sites. As an ATG Engineer, you will be working on very diverse missions and assignments. This opens up unique opportunities to be engaged in innovative projects and challenging you to perform to high standards and utilizing the full extent of your professional knowledge. Interested? Submit your CV and personal details through our website at www.jointhebrightestminds.com.
Tags: structures
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structures engineer
engineer structures
Structures Engineer
2021-07-08 17:13:38| Space-careers.com Jobs RSS
Position Reference 973 On behalf of ESA, we are currently looking for a Structures Engineer to work in its Site ESTEC in the city of Noordwijk, The Netherlands. Tasks and Activities The scope of work will include Structures Static, BucklingStability, ThermoElastic Analysis Support the generation and setup of mathematical models for structural thermoelastic stability problems for Agency funded projects, taking into account specific requirements attached to this type of analysis. Perform the interpolation of the temperature maps as resulting from thermal analysis for their employment in finite element structural analysis. Perform thermoelastic analysis leading to the determination of loads and deformations, evaluate the outcome in terms of margins of safety and stability budgets, evaluate critically the results and issue relevant documentation covering all analysis steps. Where necessary nonlinear approaches shall be considered and specific solution sequences shall be developed. Design and Configuration Support spacecraft and launcher configuration studies for Agency projects. This includes operating CAD tools and participation in Concurrent Design Facility CDF sessions at ESTEC. Perform mass, inertia and balance calculations and relevant budget assessments. Issue relevant documentation covering all configuration definition aspects, and where necessary shall support the configuration definition by preliminary structural analyses using FEM models. Ensure CAD interfaces and configuration data transfer with Agency contractors via international standards. Ensure the interface between the CAD systems and the relevant FEM tools to enable further evaluation of the structural behaviour. Contribute to the further development of the Structures and Configuration tools deployed in the Agency, including in the CDF. Support progress meetings and reviews in support to Agency projects. Support the updating and maintenance of CAD and FE models databases. Support and contribute to the establishment and maintenance of relevant Structures Engineering Standards and Handbooks. Evaluate critically the results and the loads and issue relevant documentation. 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. Produce advanced reduced models of spacecraft and launchers. Set up relevant documents and maintain all models and tools required to perform launcher spacecraft coupled loads analysis. 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. Take into account the specific objectives of such analyses and where necessary nonlinear analyses shall be performed and specific solution sequences shall be developed. Issue relevant documentation covering all analysis steps. Where applicable produce advanced reduced dynamic mathematical models. Skills and Experience The following skills and experience are mandatory MSc. in Aeronautical or Mechanical 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 deadline. Fluency in English, both written and spoken. How to Apply Looking to take your career to the next level? Interested applicants should submit their CV and Cover Letter to RHEAs Recruitment team at careersrheagroup.com no later than 17082021. Preference will be given to candidates eligible for an EU or national personal security clearance at the level of CONFIDENTIAL or above.
Tags: structures
engineer
structures engineer
engineer structures
Structures engineer
2021-07-08 17:13:38| Space-careers.com Jobs RSS
Telespazio Belgium is an international company which specializes in the space industry for over 30 years. The European Space Agency is our biggest client and we provide highly qualified employees to many sites of ESA mainly in the Netherlands, Germany, Spain, France, and the UK. Your career is very important to us, therefore, we provide a permanent contract with great benefits, good salary, relocation package and genuine support to our employees. On behalf of the European Space Agency, we are looking for a highly skilled Structures Engineer to work in ESTEC, in the Netherlands. SPECIFIC TASKS the generation and setup of structural mathematical models using the finite element method for structural analysis problems for Agency 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. Perform stability analysis leading to the determination of buckling loads and deformations. Where necessary the post buckling behaviour shall be addressed, adequate nonlinear approaches used, and where relevant specific solution sequences shall be developed. Evaluate critically the results, and issue relevant documentation covering all analysis steps Support the generation and setup of mathematical models for structural thermoelastic stability problems for Agency funded projects, taking into account specific requirements attached to this type of analysis. Perform the interpolation of the temperature maps as resulting from thermal analysis for their employment in finite element structural analysis. Perform thermoelastic analysis leading to the determination of loads and deformations, evaluate the outcome in terms of margins of safety and stability budgets, evaluate critically the results and issue relevant documentation covering all analysis steps. Where necessary nonlinear approaches shall be considered and specific solution sequences shall be developed. Evaluate critically the results and the loads and issue relevant documentation. Support spacecraft and launcher configuration studies for Agency projects. This includes operating CAD tools and participation in Concurrent Design Facility CDF sessions at ESTEC. Perform mass, inertia and balance calculations and relevant budget assessments. Issue relevant documentation covering all configuration definition aspects, and where necessary shall support the configuration definition by preliminary structural analyses using FEM models. Ensure CAD interfaces and configuration data transfer with Agency contractors via international standards. Ensure the interface between the CAD systems and the relevant FEM tools to enable further evaluation of the structural behaviour. Contribute to the further development of the Structures and Configuration tools deployed in the Agency, including in the CDF. Support progress meetings and reviews in support to Agency projects. Support the updating and maintenance of CAD and FE models databases. Support and contribute to the establishment and maintenance of relevant Structures Engineering Standards and Handbooks. 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. Take into account the specific objectives of such analyses and where necessary nonlinear analyses shall be performed and specific solution sequences shall be developed. Issue relevant documentation covering all analysis steps. Where applicable produce advanced reduced dynamic mathematical models. REQUIREMENTS Masters degree in Aeronautical or Mechanical Engineering. At least 4 years of relevant experience. DEADLINE 18082021 Please note that interviews canwill be held via skype, webex or other digital platforms. The TUD will be agreed taking into account how the coronavirus situation develops.
Tags: structures
engineer
structures engineer
engineer structures
Space Structures Engineer
2020-08-06 09:10:42| Space-careers.com Jobs RSS
Aurora is an established supplier of skilled manpower to ESA and in particular at ESTEC and ESAC. Aurora has the opportunity to expand our support to ESA in the domain of STM Structures, Materials, Mechanisms and Thermal Engineering. Happiness of our employees has proven key to obtaining excellent results and a client who also regards us highly for excellent service. Overview General tasks related to the role are Support spacecraft and launcher configuration studies for Agency projects. This includes operating CAD tools and participation in Concurrent Design Facility CDF sessions at ESTEC. Support and contribute to the establishment and maintenance of relevant Structures Engineering Standards and Handbooks. Support the generation and setup of structural mathematical models using the finite element method for structural analysis problems for Agency 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. Perform stability analysis leading to the determination of buckling loads and deformations. Where necessary the post buckling behaviour shall be addressed, adequate nonlinear approaches used, and where relevant specific solution sequences shall be developed. Evaluate critically the results, and issue relevant documentation covering all analysis steps. Support the generation and setup of mathematical models for structural thermoelastic stability problems for Agency funded projects, taking into account specific requirements attached to this type of analysis. Perform the interpolation of the temperature maps as resulting from thermal analysis for their employment in finite element structural analysis. Perform thermoelastic analysis leading to the determination of loads and deformations, evaluate the outcome in terms of margins of safety and stability budgets, evaluate critically the results and issue relevant documentation covering all analysis steps. Where necessary nonlinear approaches shall be considered and specific solution sequences shall be developed. Evaluate critically the results and the loads and issue relevant documentation. 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. Take into account the specific objectives of such analyses and where necessary nonlinear analyses shall be performed and specific solution sequences shall be developed. Issue relevant documentation covering all analysis steps. Where applicable produce advanced reduced dynamic mathematical models. Specific qualification requirements University degree MSc. in Aerospace or Mechanical engineering. 5 to 10 years experience in the space industry on the mechanical design, development and verification of space segment hardware. 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. Fluent in the English language spoken and written. Knowledge of another European language is an asset. Legal and Security Requirements All applicants must be legally allowed to work in The Netherlands Applicants are required to provide a copy of their passport and degree certificate. Aurora will validate the Degree with the issuing University and provide evidence to ESA. Prior to issuing a letter of employment the applicant shall provide to Aurora a recent official document declaring that they are of good conduct from the country where currently resident. Location The work will be performed at the European Space Technology and Research Centre ESTEC at Noordwijk, The Netherlands. Contract The selected candidate will receive good remuneration in line with ESA Job Class. Will be registered for both social security and tax in the Netherlands. The standard working hours are 40 per week. There are 12 public holidays and an additional 30 annual days holiday. Training to improve efficiency and provide strength for future career are of course included. Aurora assist with relocation both with support and financially. Aurora contributes to a company pension scheme. To be considered for this Position Prior to 10 September 2020, please apply via our Job Application form quoting TECSTM631 as the reference. Aurora will agree conditional employment terms and conditions with candidates before presenting them by 14 September 2020, 13.00 hours.
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