Raffaele Basile

Technical Authority A5 stage for Vega and Vega-C at AVIO
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Location
Colleferro, Latium, Italy, IT
Languages
  • Italiano Native or bilingual proficiency
  • Inglese -
  • Tedesco -

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Credentials

  • KC & TOLERANCING PROCESS
    Airbus Group Learning Centre, Augsburg
    Jan, 2014
    - Sep, 2024
  • PLMlight Release 1
    Premium AEROTEC
    Jan, 2012
    - Sep, 2024
  • PDMLink SSCI Definition Phase (E)
    ELS (EADS Group HR Operations Learning Services), Augsburg
    Jan, 2011
    - Sep, 2024
  • Structure Concession Supplier Engineering
    Airbus Quality Training Deutschland, Augsburg
    Jan, 2011
    - Sep, 2024
  • VPM A350 - Design In Context (E)
    ELS (EADS Group HR Operations Learning Services), Augsburg
    Jan, 2011
    - Sep, 2024
  • PRIMES A400M End to End Process
    Ikarus Solutions and Capable Technologies Hamburg
    Jan, 2009
    - Sep, 2024
  • CATIA V5 All Methods
    Ikarus Solutions and Capable Technologies Hamburg
    Jan, 2008
    - Sep, 2024
  • CATIA V5 Validation
    Ikarus Solutions and Capable Technologies Hamburg
    Jan, 2008
    - Sep, 2024

Experience

    • Italy
    • Aviation and Aerospace Component Manufacturing
    • 500 - 600 Employee
    • Technical Authority A5 stage for Vega and Vega-C
      • Jul 2018 - Present

      June 2021 - now Technical Authority A5 stage for Vega and Vega-C July 2018 - May 2021 Development and definition of design interfaces for the A5 stage of VEGA and VEGA-C launcher. Requirements analysis and implementation of interface specifications for light structures, dedicated to the transport and ejection of paying loads. Development and optimization of satellite accommodation and related equipment for the various missions of the launchers. 3D models realization, interface and manufacturing drawings creation, bills of materials and design documents creation. Show less

    • Germany
    • Aviation & Aerospace
    • 100 - 200 Employee
    • Aerospace Design Engineer
      • Feb 2016 - Jul 2018

      Development and evaluation of design concepts for highly loaded welded and riveted space structures. Design optimization regarding mass, cost and manufacturability. 3D models and manufacturing drawings creation, bills of materials and design documents creation. Development and evaluation of design concepts for highly loaded welded and riveted space structures. Design optimization regarding mass, cost and manufacturability. 3D models and manufacturing drawings creation, bills of materials and design documents creation.

    • Primary Structural Design Engineer
      • May 2011 - Jan 2016

      • Feb 2014 - Jan 2016 Concession's Technical Answer for Primary Structure of A350 -900/-1000 S13/14 and S16/18 Focal Point Design for (G1c) Wedge Test Concessions, bonding Test for Stringer and Skin Panel Special Technical repair Designer in CATIA V5 - DMU Specialist MAP and Manufacturing supporting Focal Point Concession Steering Member of the Industrialization Department of A350 • Sep 2012 - Feb 2014 (1 year and 6 months) Focal Point for CFRP Cargo Door Surrounding of A350-1000 S16/18 Cargo Door Surrounding development from Maturity A to Maturity B Focal Point for Supplier interface Design proposals and investigations in CATIA V5 - DMU Specialist Design Principles 3D/2D design and check Member of Door Surrounding Department of A350 • May 2011 - Sep 2012 (1 year and 5 months) DQN and Concession's Technical Answer for Primary Structure of A400M CFLS Special Technical repair Designer in CATIA V5 - DMU Specialist 3D/2D design and check DQN incorporation Member of A400M Central Fuselage Lower Shell Department Show less

    • Structural Design Engineer
      • Nov 2008 - Apr 2011

      • Jul 2010 - Apr 2011 (10 months) DQN Team Leader/Deputy and Supplier work management DQN Analysis & Solution, MAP support, secondary structure design for A400M (IFA Factory Airbus - Bremen - Germany) Design and development of 3D/2D single part for milled and sheet metal parts used for electrical, mechanical, pneumatic, insulation, air conditioning, equipment and hydraulic systems. • Mar 2010 - Jun 2010 (4 months) Design Check for 3D/2D environment installation and manufacturing of secondary structure for A400M (IFA Factory Airbus - Bremen - Germany) • Aug 2009 - Feb 2010 (7 months) DQN Analysis & Solution, MAP support, secondary structure design for A400M (IFA Factory Airbus - Bremen - Germany) Design and development of 3D/2D single part for milled and sheet metal parts used for electrical, mechanical, pneumatic, insulation, air conditioning, equipment and hydraulic systems. • Jun 2009 - Jul 2009 (2 months) DQN Analysis & Solution, MAP support, secondary structure design for A400M (FAL Factory Airbus - Seville - Spain) Design and development of 3D/2D single part for milled and sheet metal parts used for electrical, mechanical, pneumatic, insulation, air conditioning, equipment and hydraulic systems • Apr 2009 - May 2009 (2 months) DQN Analysis & Solution, MAP support, secondary structure design for A400M (IFA Factory Airbus - Bremen - Germany) Design and development of 3D/2D single part for milled and sheet metal parts used for electrical, mechanical, pneumatic, insulation, air conditioning, equipment and hydraulic systems. • Nov 2008 - Mar 2009 (5 months) Installation drawing Design, secondary structure for A400M 2D installation drawing of sheet metal parts for electrical systems. Show less

    • Aerospace and Mechanical Engineer (Design, Research and Development)
      • Apr 2007 - Oct 2008

      Development and Design of the P1XX fuselage barrel for a test structure in collaboration with Piaggio Aero Industries S.p.A Involved in design and development of a wing model for a wind tunnel test in IWT (Icing Wind Tunnel) at CIRA (Italian Research Centre Aerospace) Design and implementation of porosity adjustment system for the test chamber of the PT1 wind tunnel at CIRA Development and Design of the P1XX fuselage barrel for a test structure in collaboration with Piaggio Aero Industries S.p.A Involved in design and development of a wing model for a wind tunnel test in IWT (Icing Wind Tunnel) at CIRA (Italian Research Centre Aerospace) Design and implementation of porosity adjustment system for the test chamber of the PT1 wind tunnel at CIRA

Education

  • Università degli Studi di Napoli 'Federico II'
    Aerospace Engineering Master Degree, Ingegneria aerospaziale, aeronautica e astronautica
    2000 - 2007

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