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    CV: Satellite System Engineer

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    Personal information
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    Candidate Profile
     Date Submitted:21-06-2009
     Last Modified:15-01-2010 (03:54)
    Job information
     Current job:Satellite System Engineer
     Employment Term:Permanent
     Relocation:Anywhere
     Date available:within 3months
     Industry:Satellite Manufacturers and Subcontractors
     KeywordsSatellite System Engineering project management Design development Assembly, Integration Verification and Test Mission design Earth Observation Navigation telecommunication Feasibility Study inter-personal relationship skills
    CV

     

     

    EDUCATION
     
    Degree in Aeronautical Engineering (Space System branch) at Politecnico di Milano
                97/100 on July 1990
     
    Degree in Philosophy (2nd degree; Logics-Economics branch) at Università La Sapienza di Roma            110/110 "cum laude" on July 2001
     
    PRESENT EMPLOYMENT
     
    Employer:                     THALESALENIA SPACE – Rome, Italy
    Recruitment date:          January 1991
     
    Present Position: Satellite AIV&T (Assembly, Integration, Verification & Test) Engineer (since 2004)
    Project:               GalileoSat (European Navigation Satellite System)
    Collocation:         Ottobrunn (München) as part of Astrium space segment system engineering team
    Customer(s):       ESA - European Space Agency;
    Tasks:                - Definition of AIV program at Satellite and subsystem level
    - Establishment of AIV requirements in terms of model philosophy, verification criteria, test planning and execution;
                              - Technical management of Satellite AIT (Assembly, Integration & Test) Sub-contractor;
    - Monitoring, control and technical support to Satellite AIT for the specification, procurement and utilisation of GSE;
    - Evaluation of suitability of test facilities.
    - Support to project management for the overall satellite schedule review/optimisation, the risks identification, the selection and implementation of mitigation actions.
    - Definition of all Mechanical Satellite Test requirements (test levels, test set-up, test facility, success criteria, etc.) as guideline for test procedure preparation and test execution;
    - Review of test procedures and test results.
    - Space Segment responsible for Satellite Structural Model during qualification test campaign (in ETS-ESTEC);
                                    
     
    Previous Position: Mission Design Engineer (2003)
    Project:               GioveB (Collocation in Ottobrunn as part of Galileo Industries satellite system engineering team) until delta-PDR (Preliminary Design Review)
    Customer:           ESA - European Space Agency;
    Tasks:                -     Establishment of mission profile, phases, timeline and operational sequences
    -          Supervision of Mission Analyses and relevant Launcher interface aspects.
     
    Previous Position: Deputy of Project Manager (2002 - 2003)
    Project:               Bus of RADARSAT-2C-Band SAR Satellite (Final development Phase C/D)
    Customers:         CSA (Canadian Space Agency); MDA (MacDonald Dettwiler) as Prime Contractor
    Tasks:                -    Coordination and supervision of Bus development, sub-contractor technical management and Bus requirement verification;
    -          Contribution, review and approval of Bus documentation (CDR data Package, Qualification Status Documents, Bus Verification Reports);
    -          Presentation and discussion of the verification status with customer during formal project review
     
    Previous Position: Satellite System Engineer In various feasibility studies for different satellite missions (1998 - 2001)
    Projects:             EGPM European Contribution to NASA Global Precipitation Mission - (ESA) Phase A
                              SMLASuperSpectral Mission for Land Applications – (ESA) Phase A
                              Actor Study of Alenia platform utilisation for ESA Earth Observation Missions Feasibility St.
                              L-SARSAT L-Band SAR Satellite:- (SAST - Shangai Academy of Space Technology) - Phase A-B
                              Clouds Cloud and Radiation monitoring satellite - EC (European Community)- Phase 0
                              SIRAL Radar Altimeter of CryoSat Remote Sensing Satellite (ESA) - Phase A
                              GalileoSat Navigation satellite Constellation (ESA) - Phase A
                              G.Marconi Data Relay Satellite for Mars (ASI-NASA) - Feasibility Study
    GOMAS GEO Observatory for Microwave Atmospheric Sounding - ASI (Italian Space Agency) - Feasibility Study
                              GIASIGEO Infrared Atmospheric Sounding Interferometer – EUMETSAT - Feasibility Study
    Tasks:                - Establishment of Satellite System requirements on the basis of Mission, Payload, Launcher System and Ground Segment requirements;
    -          Coordination, supervision and contribution to system engineering activities (definition of mission profile, satellite architecture, operational concept, platform & SubSystems design, system analyses, budgets and trade-offs);
    -          Definition of preliminary design, development and validation plan; ROM (Rough Order of Magnitude) costs.
     
     
    Previous Position: Mechanical Project Responsible (1997)
    Project:               SHF Receiving Antenna for SICRAL (GEO TLC satellite) in C/D Phase
    Customer:           Department of Defence of Italy
    Tasks:                -    Definition of mechanical design;
    -          Structural mathematical modelling and analyses;
    -          Preparation of Mechanical Test Plan, supervision of tests, check of test results.
     
    Previous Position: Satellite mechanical System Engineer in ESA projects
    Projects:             MCP TX (Mission Communication Package Transponder) of MSG (Meteosat Second Generation) satellite: Phase C/D; (1996)
                              ARTEMIS Data Relay Satellite in GEO: C/D Phase; (1994-1995)
    At ALENIA TURIN site:
                              CTV (Crew Transfer Vehicle) Phase0 – requirement assessment (1993)
                              U.V.C.S. (UltraViolet Coronograph Spectrometer), Core part of S.O.H.O. (Solar and Heliospheric Observatory) Telescope: C/D phase; (1992-1993)
    Aristoteles Satellite (Earth Observation): Pre-B study Phase; (1991)
    Tasks:                  -    Design and development of thermomechanical architecture and overall layout of space systems;
    -          System budgets and Environmental Analyses;
    -          Engineering support to Sub-contractor technical management: review of mechanical design, structural analyses, test plan and test reports
     
     
    PREVIOUS EMPLOYMENT
    Employer:       College: ‘Istituto Tecnico Industriale Malignani’Udine - Italy
    Position:          Teacher of ‘Automatic Systems’ and ‘Mechanics’
    Period:            November-December 1990
     
    PUBLICATIONS
     
     “Instruments and system for CLOUDS - a Cloud and Radiation monitoring satellite”
    Proceedings of the EOS/SPIE Symposium on Remote Sensing, Sept. 25‑29, 2000, Barcelona, Spain, SPIE v.4169, p.279-290.
     
     
     “CLOUDS - a Cloud, Aerosol, Radiation and Precipitation Explorer”
    Proceedings of the 3rd IAA Symposium on Small satellites for Earth Observation, April 2-6, 2001, Berlin, pp.8 .Also in: Acta Astronautica, 52, 739-746.
     
    Presentation at International Forum:
     
     “Drone Satellites for the Global Precipitation Mission: An Opportunity for a European / Italian Contribution” International Forum on a sustainable program of Small Satellite for Space Science and Applications; September 2000, Rome
     
    COURSE ATTENDANCE:
     
    ‘Economics’ – ThalesUniversity – Rome 2009
    ‘Passport to Project Management’ - ThalesUniversity – Turin 2008;
     ‘Successful Negotiation’ – Infinity - Rome 1999;
     ‘Satellite Communication Systems’ – CEI Europe - Barcelona 1998;
     ‘Nastran Dynamic Analysis’ – MacNeal Schwendler – Turin 1997;
     ‘Professional Capability and Organisational Behaviour’ – Finmeccanica - Rome 1994;
     ‘Space Systems Engineering’ – Alenia Internal Course - Turin 1991
     
     
    LANGUAGES
    Italian (Mother Language)
    English   (fluent)
    German (good)
    French (scholastic)
    Spanish (scholastic)
     


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