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Anthony CARON

Courcouronnes

En résumé

An enthusiastic, dynamic and driven personality with several years experience within the Aerospace industry and an Engineering Degree in Fluids Mechanic and energetic. Having the ability to lead engineering projects and being familiar with the European Space Environment and operation. Fascinated by Space sector, always improving my profile with new skills in this field

Mes compétences :
Électromécanique
Modélisation multiphysiques
Simulink
Lean management
Mécanique des fluides
Thermique
Moteur électrique
Gestion de configuration
Gestion de projet
Visual Basic
MATLAB
Mécatronique
Comsol Multiphysics

Entreprises

  • Snecma - Project Engineer for the development of fluid control mechanisms of Ariane 6 main cryogenic stage

    Courcouronnes 2014 - maintenant

  • Snecma - Design engineer of fluid control mechanisms for cryogenic rocket propulsion in R&T programs

    Courcouronnes 2013 - 2014 In the frame of a Research and Technologies program, I have achieved activities in order to mature technologies linked to Pogo Suppressor Device for the next generation of rocket cryogenic propulsion system :

    - Project management
    * Elaboration of the technical proposal
    * Elaboration of the development logic (activities, planning, ressources, risks)
    * Progress report
    * Technical synthesis
    - Elaboration of technical specification in compliancy with upper systems requirements and ESA/CNES design rules
    - Functional design and modelisation
    - Management of mechanical design activities and reliability activities (elaboration of the statement of work, management of the choosen technical suppliers)
    - Technical synthesis and holding of the succesful Feasibility Concept Review

  • Snecma - Design engineer of cryogenic rocket engine valves for R&T programs

    Courcouronnes 2011 - 2014 I participated to Research and Technologies activities about hardware in the loop cryogenic rocket engine control simulation for the next generation of engines. In that frame, I was particularly in charge of activities linked to cryogenic valves.

    From the beginning to the Preliminary Design Review :
    - Project management
    * Elaboration of the technical proposal
    * Elaboration of the development logic (activities, planning, ressources, risks)
    * Progress report
    * Technical synthesis
    - Elaboration of valves technical specifications in compliancy with upper systems requirements and ESA/SNEC design rules
    - Functional design and modelisation of the valves
    - Management of the subcontractors performing the functionnal design of the control electronics
    - Management of mechanical design and reliability activities (elaboration of the statement of work, management of the choosen technical subcontractors)
    - Technological innovation (patent, integrated in the technological roadmap elaboration)
    - Participation to the different succesfull reviews

    From the Preliminary Design Review up to now :
    - Elaboration of the technical proposal up to completion in line with the development logic

  • Snecma - Design engineer of cryogenic rocket engine valves for Ariane 5 ME Upper stage

    Courcouronnes 2010 - 2014 I was in charge of the technical management of subcontractors developing monostable and bistable valves using solenoid actuator for the Vinci cryogenic rocket engine. I have particularly ensured the following activities since the Feasibility Concept Review to the Critical Design Review :
    - Elaboration of the Technical Specifications in compliance with upper systems requirements and ESA/CNES Design rules
    - Technical management of suppliers
    * Technical choices validation (actuator parts, tightness parts, mechanical parts, hydraulic parts...)
    * Modelisation cross check,
    * Test plans validation and test results analysis
    * Configuration management
    - Synthesis and report to the customer
    - Participation to the different succesfull reviews

  • Snecma - Thermal and fluids mechanic calculation engineer

    Courcouronnes 2010 - 2010 Improvement of aerothermic calculation methodology on cryogenic rocket engine thrust chamber :
    - Modelisation and mapping of Hm7-b engine (Engine of Ariane 5 upper stage) thrust chamber (2D axi and 3D model)
    - Realization of a sensibility studies on different parameters and comparison to tests results (viscosity law, turbulent models, size of the mapping...)

Formations

  • Université De Droit, Économie Et Gestion UFR (Rouen)

    Rouen 2014 - maintenant Licence 1

  • ENSIAME

    Valenciennes 2007 - 2010 Engineer's degree, Mechanic and energetic

    English (TOEIC 840)

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