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Fri, 24 Apr 2015 07:12:00 +0100
Ariane Flight VA222 Arianespace has delivered another Ariane 5 to the launch zone at Europe's Spaceport in French Guiana, positioning this workhorse heavy-lift vehicle for tomorrow's flight with a pair of telecommunications satellites: THOR 7 and SICRAL 2. The Ariane 5 rolled out today from the Spaceport's Final Assembly Building to the ELA-3 launch zone, where it is scheduled for liftoff during a launch window that opens on April 24 at 4:38 p.m. local time in French Guiana. For this 78...
Thu, 23 Apr 2015 18:00:00 +0100
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Thu, 23 Apr 2015 07:58:00 +0100
Ariane Flight VA222 Ariane 5 has been authorized for its April 24 liftoff from the Spaceport in French Guiana, with the go-ahead for this upcoming mission - which will orbit the THOR 7 and SICRAL 2 telecommunications satellites - given following today's launch readiness review. This pre-launch step - performed prior to each Arianespace mission - checked the "go" status of the heavy-lift launcher, the flight's dual-passenger payload, the Spaceport's infrastructure and the network of trackin...
Thu, 23 Apr 2015 07:58:00 +0100
Vega Flight VV05 The latest in Europe's series of Sentinel Earth observation satellites landed at French Guiana today in preparation for its orbiting on an Arianespace Vega vehicle during June, while build-up of the lightweight launcher was initiated at the Spaceport this week. Sentinel-2A was delivered by a chartered Antonov An-124 cargo jetliner that touched down at Cayenne's Felix Eboue Airport, where the spacecraft's protective shipping container was unloaded along with support equipme...
Wed, 22 Apr 2015 12:00:00 +0100
Astronomers using the HARPS planet-hunting machine at ESO's La Silla Observatory in Chile have made the first-ever direct detection of the spectrum of visible light reflected off an exoplanet. These observations also revealed new properties of this famous object, the first exoplanet ever discovered around a normal star: 51 Pegasi b. The result promises an exciting future for this technique, particularly with the advent of next generation instruments, such as ESPRESSO, on the VLT, and future tele...
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    CV: PhD in Science, Technology and Measurements for Space

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    Personal information
     Name:<withheld>
     Age:<withheld>
     Country:<withheld>
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    Contact information
     Email:<withheld>
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    Candidate Profile
     Date Submitted:22-02-2012
     Last Modified:22-02-2012 (11:46)
    Job information
     Current job:PhD in Science, Technology and Measurements for Space
     Employment Term:Temp/Contract
     Job location:Anywhere
     Date available:within 3months
     Industry:Civil Agencies/International Organizations
     KeywordsStructural aerospace engineer, Light Gas Gun developer, stratospheric experiment mechanic developer
    CV

    28, Italian

     

    OBJECTIVE

    Challenging and formative job.

    Interested in aerospace research.

    Interested in temporary or part-time contracts.

    Willing to move and/or transfer abroad.

     

    EDUCATION and QUALIFICATIONS

     

    ·         PhD in Science, Technology and Measurements for Space (STMS), at the Centre of Studies and Activities for Space CISAS - "G.Colombo" research department of the University of Padova, Italy, 2009-2011

     

    o   The title of the doctoral thesis is " Measurement techniques for assessing and reducing the risk posed by Micrometeoroid and Orbital Debris to Space vehicles".

     

    Main research areas:

     

    §    Risk assessment methodology, impacts phenomenology and design methods.

    §    Experimental methods (i.e. acceleration techniques and diagnostic instrumentation).

    §    Engineering models (i.e. measurements of the effects of the M/OD and derivation of   damage equations).

     

    Supervisor: Prof. Alessandro Francesconi

     

    o   Other research areas:

     

    §   Visiting researcher at Cranfield University (UK),  June – September 2011

    -       Development of a single stage light gas gun.

     

    Supervisor: Prof. Rade Vignjevic

     

    §    ESA (European Space Agency) BEXUS Programme, December 2009 – May 2011

    -       SCRAT (Spherical Compact Rechargable Air Thruster) Experiment

    Development of the structural and pneumatic subsystem for a low-thrust cold  gas actuator.

    Supervisor: Mr. Olle Persson, Swedish Space Corporation project manager, ESRANGE Space Center

     

    o   Conferences and courses attended

     

    -       20th ESA Symposium on European Rocket&Balloon Programmes (05/2011)

    -       ARA 2010 (09/2010)

    -       11th Hypervelocity Impact Symposium 2010 (04/2010)

    -       5th European Conference on Space Debris (04/2009)

     

    -       Space Debris: Threat to orbiting S/C and mitigation concepts (05/2010)

    -       Image analysis for HVI (11/2010)

    -       Multifunctional Composites (03/2010)

    -       III National School INFN (04/2009)

     

    o   Seminars presented

     

    -       The SCRAT Experiment (Cranfield University, UK, 06/2011)

    -       Space Debris: An Increasing Risk (Cranfield University, UK, 07/2011)

     

     

    o   Papers

     

    -       BARILARO L., A. FRANCESCONI, PH.D, M. FARAUD, C. GIACOMUZZO, PH.D. AND R. DESTEFANIS (2010). IMPACT DAMAGE AND BALLISTIC LIMIT EQUATIONS FOR FLEXIBLE MULTILAYER METEOROID AND DEBRIS PROTECTION SHIELDS.

    [ARA2010 Best Student Paper Award] - ARA 2010 Congress. Thun (Switzerland), 12-17 September, 2010

     

    -       A. FRANCESCONI, PH.D, C. GIACOMUZZO, PH.D, BARILARO L., E. SEGATO, PHD (2010). NUMBER, SIZE AND SPEED DISTRIBUTION OF PARTICLES EJECTED FROM SPACECRAFT SURFACES DURING HYPERVELOCITY IMPACT.

                                                                  ARA 2010 Congress. Thun (Switzerland), 12-17 September, 2010

     

    -       A. FRANCESCONI, C. GIACOMUZZO, BARILARO L. (2010). A method to assess the average properties of spacecraft ejecta from hypervelocity impact.

    11th Hypervelocity Impact Symposium. Freiburg (Germany), 5-11 April, 2010

     

    -       ALESSANDRO FRANCESCONI, CINZIA GIACOMUZZO, DANIELE PAVARIN, LEONARDO BARILARO, FRANCESCO ANGRILLI (2009). Characterization of ejecta from hypervelocity impacts on spacecraft external surfaces.

    XX AIDAA Congress. Milano, June 29 - July 3, 2009

     

     

    ·         MSc. in Aerospace Engineering:                        University of Padua, Italy, April 2008, GPA  96/110

                                        “Design of a non pyrotechnic actuated valve for a hybrid rocket”

                                                           (in co-operation with CISAS and SELEX Galileo)

                                                                                                                   Supervisor: Prof. Daniele Pavarin

     Main courses:

    -         STRUCTURAL ANALYSIS LABORATORY

    o    Final report on “Structural optimization of an optical bench as a support for two telescopes” (with Ansys software)

    -         THERMAL CONTROL OF SPACE VEHICLES

    o    Final report on “Thermal control of a satellite”

    -      


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