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Tag: components
Volkswagen Group Components previews mobile charging robot
2020-12-29 10:55:41| Green Car Congress
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US telcos ordered to 'rip and replace' Huawei components
2020-12-11 05:27:15| BBC News | Business | UK Edition
The order is the latest US move against Chinese communications firm Huawei on security grounds
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Electromagnetics Components EMC Engineer
2020-12-09 15:13:02| 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 EDP Electromagnetics Components Data Power Systems Engineering. Happiness of our employees has proven key to obtaining excellent results and a client who also regards us highly for excellent service. Overview Provide expertise in the field of Support to ESA projects for EMC harness as well as for magnetic cleanliness. Build up expertise and create network in the field of EMC. Definition and assessment of EMC requirements at both System and Equipment level. Definition and assessment of EMC test and verification procedures of spacecraft equipment and systems. Electromagnetic and circuital analyses. Assessment of EMC test results, EMC nonconformances and Request for Waivers. Troubleshooting activities for spacecraft equipment and system exhibiting electromagnetic interference. Active participation to Spacecraft or payloads Preliminary Design Reviews PDR, Critical Design Reviews CDR and Flight Acceptance Reviews FAR. Specific qualification requirements The candidateshall have experience of system engineering including PhD or MSc in Electrical Engineering, Physics or related specialization. Background and experience in EMC as well as Lab testing for EMC. Expertise in EMC analysis and practical experience in EMC testing, expertise in harness engineering is an asset. Expertise in using Matlab for data processing and evaluation. Ability to work in a team as well as independently, good communication skills. Acquaintance with both Industrial EMC practices and the Agency review processes. Assessment of EMC test data, specifications and request for Waivers. EMC Test and analysis expertise. Proactive attitude to solving problems. Good organisational skills. A very good working knowledge of spoken and written English isessential. 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 withESA 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 12 January 2021, please apply via ourJob Application form quoting TECEDP669 RTCTECEPE00669as reference. Aurora will agree conditional employment terms and conditions with candidates before presenting them by 18January 2021, 13.00 hours.
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Volkswagen Group Components delivering essential components for Volkswagens ID.4 electric SUV
2020-11-29 11:55:37| Green Car Congress
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Propulsion components design and analysis engineer
2020-11-12 17:12:17| Space-careers.com Jobs RSS
Description Design and Analysis of launch vehicle Propulsion elements and configurations in concert with Structures subsystem. Specific focus on Propellant lines design analysis. Responsibilities Participate in subsystem design and architecture of pressurefed liquid rocket engine, including component sizing, loads determination, and detailed designanalysis. Perform thermal mechanical load analysis for propellant lines including cryogenics and fuel lines as well as high pressure gas lines. Create and manage test and development plans for engines and propulsion components. Perform analysis and interpretation from Propulsion test and flight data. Design of primary metallic structures different size range of machined components, sheet metal parts for propellant lines cryogenics, fuel and gas fitting. Design of secondary structures as brackets or supports for rigid pipes, valves, mechanism, propulsion components electrical harness, etc. Generation of Engineering documentation such as 3D models, Drawings, BOMs, and Eng. Change Notes for the complete definition of Detailed Parts, Assemblies, and Installation. Maintain and improve program standard approaches to design, safety factors, material allowables, drafting standards, etc. Liaise with others Engineering departments Structures design and stress, MP, Quality, etc. and provide information to the Manufacturing area under request. Responsible to accomplish with specifications and requirements during the development of the assigned tasks or product design along the entire lifecycle and across all phases from Prototype, Testing and Series production. Participate in the periodic design reviews dealing with SCHManufacturing for the achievement of requirements, specifications, feasibility, lead time and prices. Continuous research to optimize design solutions. Identify and recommend opportunities to reduce costs and improve efficiency. Complete the assigned tasks on time, on quality, on cost. Required competences Aerospace or Mechanical Engineering Bachelors degree or demonstrable relevant experience in lieu thereof. Minimum 5 years of technical experience in Aerospace Industry as Propulsion design analysis engineer or Structural Design Engineer or an equivalent combination of education and experience. Demonstrated experience in design analysis of Launcher Propulsion or Aircraft Propulsion. Knowledge in selection and application of design criteria and rules, Aerospace standards, materials, strengths, and other mechanical properties, according to the loading conditions, working environment, etc. High degree of CAD competence and PDM tools. Valued competences Familiar with the main manufacturing technologies and capabilities Knowledge of the most common corrosion prevention rules and surface protection. Knowledge of the most common cryogenic LOX cleaning procedures. Knowledge of Cryogenic LOX manipulation. Proven in the development of products from the original concept design according to Aerospace normative and rules, through to the delivery of detailed technical design packaging into final production. Design focused to assembly line concerns, tooling, and jigs. Familiar with Aerospace standard parts and typical light materials, metallic and nonmetallic. Preferred software Siemens NX and Teamcenter. An occasional need to travel with the role will be required. Selfmotivated and able to work under pressure to meet deadlines, dealing with situations that are constrained by time and managing different tasks at once. Able to work autonomously with little supervision. Fluent written and oral communication Spanish and English. Experience 5 years experience minimum in design of Launcher Propulsion or Aircraft Propulsion. 5 years experience in parametric modelling software. Experience in Rockets Aircraft Structural Design is a plus.
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