.MissionAs part of a small, passionate, and accomplished team, you will be responsible for the Design of the launch vehicles structures.Responsibilities Design of launch vehicle structural elements and configurations jointly with other engineering disciplines.Design of primary metallic structures (different size range of machined components, sheet metal parts, welded structures, metallic pressure vessels and tanks, etc.).Design of primary composite structures (sandwich, monolithic, filament winding elements, hand lay-up, RTM parts, etc.).Design of secondary structures as brackets or supports for rigid pipes, valves, avionics equipment, antennas, mechanism, electrical harness, etc.Generation of Engineering documentation such as 3D models, Drawings, BOMs, MCI and weight reports, technical reports and Eng. Change Notes for the complete definition of Detailed Parts, Assemblies and Installation.Liaise with others Engineering departments (Stress Analysis, M&P, Testing, Propulsion, Avionics, etc.) and provide information to Manufacturing area under request.Responsible to accomplish with Product Specifications, Sub-System requirements and Interface definition during the development of the product design along the entire lifecycle and across all phases, from Prototype, Testing and Series production.Participate in the periodic design reviews dealing with SCH/Manufacturing for the achievement of requirements, specifications, feasibility, lead time and costs.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".Necessary RequirementsAerospace or Mechanical Engineering Bachelor's degree.Minimum 5 years of technical experience in Aerospace Industry as Structural Design Engineer or an equivalent combination of education and experience.More than 5 years of experience in parametric modelling software.Experience in Drawing dimensioning, Tolerance Stack Analysis and Methods (ASME Y14.5, ISO 1101).Competence in the design of Aerospace primary structure (metallic and composites parts) and secondary structure.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.Familiar with reading and applying Aerospace normative, papers and documentation.High Proficiency with CAD (Siemens NX) and PDM tools (Teamcenter).Desired RequirementsExperience in Rockets Structural Design is a plus.Experience concerning the typical design requirements of structures exposed to extreme conditions, (cryogenic, high temperatures, vibration environment, etc ).Experience in insulation materials, procedures and methods.Familiar with the main manufacturing technologies and capabilities (machining, sheet metal forming, welding, composite hand lay-up, RTM, filament winding, etc
