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Wed, 21 Feb 2018 04:29:31 +0000
In spite of all the safeguards, companies must continually monitor traffic on their global networks to detect attempted or successful penetration and take steps to mitigate the impact of security breaches. SpaceNews.com
Tue, 20 Feb 2018 22:02:12 +0000
Bigelow Aerospace has established a space operations subsidiary whose first task will be to study the market for the company's commercial space stations as it grapples with competition from China and NASA. SpaceNews.com
Tue, 20 Feb 2018 19:50:53 +0000
President Trump's 2019 NASA budget would pull the plug on astronomer's No. 1 priority for the next decade. NASA's former astrophysics chief says Congress should keep WFIRST funded. SpaceNews.com
Tue, 20 Feb 2018 08:57:05 +0000
Vector, one of a growing number of companies developing small launch vehicles, plans to carry out its first orbital launch this summer from Alaska. SpaceNews.com
Mon, 19 Feb 2018 22:29:05 +0000
When members of the National Space Council meet this week, they are expected to discuss, among other issues, regulatory reforms intended to promote growth of the commercial spaceflight industry. SpaceNews.com
Mon, 19 Feb 2018 15:06:38 +0000
What exactly will replace SBIRS remains to be seen. Air Force Secretary Heather Wilson suggested the new system will be “simpler” and more survivable to enemy attacks. SpaceNews.com
Mon, 19 Feb 2018 13:44:31 +0000
Air Force leaders say changes in procurement spending are necessary for the military to ensure air and space supremacy. SpaceNews.com
Mon, 19 Feb 2018 10:38:47 +0000
The head of the organization that manages the national laboratory portion of the International Space Station will leave next month as it deals with an uncertain long-term future for the station. SpaceNews.com
Sun, 18 Feb 2018 15:32:36 +0000
Telesat, with one demonstration satellite for its planned broadband satellite constellation in orbit, expects to announce plans for manufacturing the full system in the coming months as it seeks partners to help fund its development. SpaceNews.com
Fri, 16 Feb 2018 21:45:19 +0000
NASA has certified the current version of the SpaceX Falcon 9 to launch some categories of science missions, a milestone needed for the upcoming, but delayed, launch of an astronomy spacecraft. SpaceNews.com
Fri, 16 Feb 2018 19:38:53 +0000
Eutelsat Chief Executive Officer Rodolphe Belmer is taking a contrary view on short-term capacity leases and the explosive growth of video streaming — two disruptive video trends causing angst among satellite operators with substantial television broadcast business. SpaceNews.com
Fri, 16 Feb 2018 15:20:41 +0000
The U.S. Air Force and Aerojet Rocketdyne are working to revise an agreement to support development of the company's AR1 rocket engine, as questions continue about the engine's long-term future. SpaceNews.com
Thu, 15 Feb 2018 23:05:27 +0000
The president of the Canadian Space Agency said he is taking a "wait and see" approach to NASA's plans to end funding of the International Space Station in the mid-2020s, citing the lack of detail. SpaceNews.com
Thu, 15 Feb 2018 22:38:59 +0000
NASA’s topline budget will be flat for the foreseeable future — which means an effective decrease in real dollar funding for the agency. As a result, President Trump may see his moon plans come crashing down to Earth. SpaceNews.com
Thu, 15 Feb 2018 20:09:54 +0000
Satellite hardware and network builder Gilat of Israel, seeking to interest cellular operators in expanding their reach by satellite, is pressing forward with a strategy of building the entire network for them in exchange for multi-year commitments to pay for the service. SpaceNews.com
Thu, 15 Feb 2018 18:33:42 +0000
The Air Force creating a budget line for small launch is a “very good thing for the industry,” said Steve Nixon, vice president of strategic development at Stratolaunch. SpaceNews.com
Thu, 15 Feb 2018 17:31:01 +0000
Fleet operator ViaSat’s newest satellite could lose around 15 percent of its intended throughput due to an antenna problem discovered after launch. SpaceNews.com
Thu, 15 Feb 2018 09:34:06 +0000
A United Nations committee reached agreement last week on nine guidelines intended to reduce the risk of collisions in space and other harmful space activities. SpaceNews.com
Wed, 14 Feb 2018 19:25:22 +0000
Federal Communications Commission Chairman Ajit Pai wants his agency approve SpaceX’s 15-month-old application to serve the U.S. with its proposed megaconstellation. SpaceNews.com
Wed, 14 Feb 2018 18:17:22 +0000
U.S. intelligence report: “Russia and China aim to have nondestructive and destructive counter-space weapons available for use during a potential future conflict.” SpaceNews.com
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  • CV: Founder and Thermal Engineer

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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:13-02-2018
     Last Modified:13-02-2018 (05:20)
    Job information
     Current job:Founder and Thermal Engineer
     Employment Term:Temp/Contract
     Job location:Anywhere
     Date available:immediately
     Industry:Civil Agencies/International Organizations, Satellite Manufacturers and Subcontractors, Satellite Operators, , , Launch Systems, Business Services
     KeywordsHas been in the field of spacecraft for the past nine years. He has performed his duties as a Senior Thermal Engineer who holds his own in sub-field of thermal analysis, thermal tests. These areas are of his special expertise which is use
    CV

    Thermal Engineer

     

    Thermal, heat transfer

    Spacecraft and satellite subsystems’ 3D modelling

    ESATAN-TMS thermal modelling suite

     

    Thermal engineering / Space industry

     

    Operating system: Windows, Linux

    Office applications: MS-Office, Lotus

    CAD and thermal software: ESATAN-TMS, CORATHERM/CIGAL (now known as e-Therm)

     

     

    FOUNDER / ALPHID LTD / SPACE / UNITED KINGDOM                           07-2013 to Present

        Skills required: Thermal analysis, Requirements analysis, Satellite subsystem, Modelling

        Nature of project: Calculating ExoMars STR Radiator view factors to space

        Objectives:

    The STR Radiator should have a minimum direct view factor to space of 80%

        Achievements:

    Built the detailed geometry model of STR Radiator

    Computed STR Radiator view factors to space

        Technical background:

    Windows 10 / ESATAN-TMS 2017, MS Word, MS Excel

     

    Skills required: Thermal analysis, Requirements analysis, Satellite subsystem, Modelling

        Nature of project: Thermal analyses of PROBA-3 spacecraft Laser Control Electronics Unit (LCEU)

        Objectives:

    Validating the current thermal design of LCEU and make appropriate changes in the thermal design, as necessary to meet the requirements

        Achievements:

    Built the detailed model of LCEU

    Defined and ran the worst cold and hot cases

    Identified the minimum and maximum temperatures of LCEU components over time for all the cases

    Compared the minimum and maximum temperatures with the limit temperature range of LCEU components

    Optimised the thermal design of LCEU to meet the requirements

        Technical background:

    Windows 10 / ESATAN-TMS 2017, MS Word, MS Excel

     

    Skills required: Thermal analysis, Requirements analysis, Satellite subsystem, Modelling

        Nature of project: Thermal analyses of PROBA-3 spacecraft Corner Cube Retroreflector (CCRR)

        Objectives:

    Validating the current thermal design of CCRR and make appropriate changes in the thermal design, as necessary to meet the requirements

        Achievements:

    Built the detailed model of CCRR

    Defined and ran the worst cold and hot cases

    Identified the minimum and maximum temperatures over time for all the cases

    Compared the minimum and maximum temperatures with the limit temperature range of CCRR

    Optimised the thermal design of CCRR to meet the requirements

        Technical background:

    Windows 10 / ESATAN-TMS 2017, MS Word, MS Excel

     

    Skills required: Thermal analysis, Requirements analysis, Satellite subsystem, Modelling

         Nature of project: Thermal analyses of a scanning LIDAR sensor

    Objectives:

    Assessing survival heater budget for the non-operational cold scenario

    Achievements:

    Built the detailed model of the camera

    Defined and ran the worst cold and hot cases

    Assessed how large of a power heater is needed to maintain the critical components above their non-operational temperature limits

    Recorded the time for which the critical units stabilise above their operational temperature limits for the operational cold case under the transient state condition

    Assessed the need for radiators for the worst hot cases

    Technical background:

    Windows 10 / ESATAN-TMS 2017, MS Word, MS Excel

     

    Skills required: Thermal analysis, Requirements analysis, Satellite subsystem, Modelling

         Nature of project: Correlations of reduced models of mid and side antenna panels of SCA instrument on MetOp-SG

    Objectives:

    Optimising reduced models of mid and side antenna panels of SCA instrument on MetOp-SG

    Achievements:

    Updated detailed and reduced models

    Compared detailed model temperature results with the reduced models

    Calculated temperatures under steady state conditions

    Modified reduced models to meet the requirements

    Technical background:

    Windows 7 / ESATAN-TMS r7, MS Word, MS Excel

     

    Skills required: Thermal analysis, Requirements analysis, Satellite subsystem, modelling

         Nature of project: Predictions of PROBA-3 spacecraft DARA instrument extreme temperatures

    Objectives:

    Calculating PROBA-3 spacecraft DARA instrument extreme temperatures in hot and cold nominal cases

    Achievements:

    Elaborated detailed model

    Modelled conductors

    Calculated temperatures under steady and transient state conditions

    Technical background:

    Windows 7 / ESATAN-TMS r7, MS Word, MS Excel

     

    Skills required: Thermal analysis, Requirements analysis, Satellite subsystem, Modelling

         Nature of project: Elaboration of reduced and detailed models of mid and side antenna panels of SCA instrument on MetOp-SG

    Objectives:

    Creating reduced and detailed models of mid and side antenna panels of SCA instrument on MetOp-SG

    Achievements:

    Implemented detailed and reduced models for the PDR

    Modelled conductors

    Calculated temperatures under steady and transient state conditions

    Technical background:

    Windows 7 / ESATAN-TMS r7, MS Word, MS Excel

     

    Skills required: Thermal analysis, Requirements analysis, Satellite subsystem, Modelling

         Nature of project: Predictions of conductive and radiative heat fluxes within the harness radiator of EUCLID spacecraft in the nominal case

    Objectives:

    Calculating conductive and radiative heat fluxes within the harness radiator of EUCLID spacecraft in the nominal case

    Achievements:

    Elaborated detailed and reduced model for the PDR

    Modelled conductors

    Calculated conductive and radiative heat fluxes under steady state conditions

    Technical background:

    Windows 7 / ESATAN-TMS r7, MS Word, MS Excel

     

    Skills required: Thermal analysis, Requirements analysis, Satellite subsystem, Modelling

         Nature of project: Creation of reduced model of Aperture Cover (ACV) on Meteosat Third Generation (MTG)

    Objectives:

    ng reduced model of Aperture Cover (ACV) on Meteosat Third Generation (MTG)

    Achievements:

    Implemented reduced model

    Correlated reduced model

    Calculated temperatures under steady state conditions

    Technical background:

    Windows 7 / ESATAN-TMS r6, MS Word, MS Excel

     

    Skills required: Thermal analysis, Requirements analysis, Satellite subsystem, Modelling

         Nature of project: Creation of reduced model of Corner Cube Mechanism (CCM) of Infra-Red Sounder (IRS) on Meteosat Third Generation (MTG)

    Objectives:

    ng reduced model of Corner Cube Mechanism (CCM) of Infra-Red Sounder (IRS) on Meteosat Third Generation

    Achievements:

    Implemented reduced model

    Correlated reduced model

    Calculated temperatures under both steady state and transient conditions

    Technical background:

    Windows 7 / ESATAN-TMS r5, MS Word, MS Excel

     

    Skills required: Thermal analysis, Requirements analysis, Satellite subsystem, Spacecraft, Modelling

         Nature of project: Predictions of PROBA Next spacecraft extreme temperatures

    Objectives:

    Calculating PROBA Next spacecraft extreme temperatures

    Achievements:

    Elaborated radiative model

    Modelled conductors

    Calculated temperatures under transient conditions

    Technical background:

    Windows 7 / ESATAN-TMS r4, MS Word, MS Excel

     

    Skills required: Thermal analysis, Requirements analysis, Satellite subsystem, Modelling

         Nature of project: Creation of detailed model of Corner Cube Mechanism (CCM) of Infra-Red Sounder (IRS) on Meteosat Third Generation (MTG)

    Objectives:

    Elaborating detailed model of Corner Cube Mechanism (CCM) of Infra-Red Sounder (IRS) on Meteosat Third Generation (MTG)

    Achievements:

    Implemented detailed model

    Modelled conductors

    Calculated temperatures under both steady state and transient conditions

    Technical background:

    Windows 7 / ESATAN-TMS r5, MS Word, MS Excel

     

    SENIOR THERMAL ENGINEER / ITP ENgines UK / SPACE / LEICESTER, UK               09-2010 to 07-2013

         Skills required: Thermal analysis, Spacecraft, Modelling, Testing, Support, Training, Presenting

    Achievements:

    Provided spacecraft thermal engineering technical services

    Investigated issues in customer models

    Answered user enquiries regarding our thermal analysis products (ESATAN-TMS, ThermNV, CADbench and ThermXL)

    Offered advice on the use of our products

    Provided input to the user requirements

    Tested pre-release software

    Delivered training material

    Technical background:

    Windows 7, Linux / FORTRAN 77 / ESATAN-TMS Thermal Modelling Suite (ESATAN-TMS, ThermNV, CADbench and ThermXL), MS Office

     

         Skills required: Thermal analysis, Requirements analysis, Spacecraft, Modelling

         Nature of project: Predictions of Solar Orbiter spacecraft SWA-EAS instrument temperatures

    Objectives:

    Calculating the SWA-EAS instrument temperatures in sun orbit to validate its thermal design

    Achievements:

    Elaborated radiative model

    Modelled the Solar Orbiter spacecraft external thermal environment in which the SWA-EAS instrument will be inserted

    Merged the Solar Orbiter spacecraft with the SWA-EAS instrument

    Calculated temperatures

    Calculated SWA-EAS instrument temperatures for hot and cold cases

    Posted processing of temperature results

    Technical background:

    Windows XP / ESATAN-TMS, MS Word, MS Excel

     

         Skills required: Thermal analysis, Requirements analysis, Spacecraft, Modelling

         Nature of project: Predictions of TROPOMI instrument (TSS) temperatures

    Objectives:

    Calculating the TROPOMI instrument temperatures in Summer Solstice and Winter Solstice orbits to identify the worst temperature gradients of TSS, and minimize them; the aim was to maintain the temperature of TSS at 293K all over the orbit

    Achievements:

    Elaborated radiative model

    Merged the TROPOMI spacecraft (internal model, external model and baffle telescope) with the TROPOMI instrument (TSS)

    Modified geometry of internal and external tent in order that they fit with the TROPOMI instrument

    Modified conductors

    Reduced conductor between TSS and warm TBU to reduce the temperature gradients of TSS

    Implemented heaters

    Implemented four PID heaters on the TSS baseplate to maintain the target temperature of TSS at 293K.

    Calculated temperatures

    Calculated TROPOMI satellite instrument temperatures for hot and cold cases

    Posted processing of temperature results.

    Technical background:

    Windows XP / ESATAN-TMS, MS Word, MS Excel

     

    SPACECRAFT THERMAL ENGINEER / altran / SPACE / CANNES, FRANCE              04-2008 to 08-2010

         Skills required: Thermal analysis, Requirements analysis, Spacecraft, Modelling

         Nature of project: Predictions of YAMAL satellite solar array panels extreme temperatures

    Objectives:

    Calculating the YAMAL satellite solar array panels extreme temperatures in T/O and G/O orbit to confirm their design

    Achievements:

    Elaborated radiative model

    Implemented 4000C2 and 4000C3 satellites models

    Recovered the motor and HRMs from APSTAR7 and W71 satellites models

    Modelled of satellite (SM and CM), the solar array panels, hinges, synchronization devices, and the yokes

    Implemented conductors

    Calculated temperatures

    Calculated solar array panels temperatures for hot and cold cases

    Posted processing of temperature results

    Technical background:

    Windows XP / ESATAN-TMS, MS Word, MS Excel

     

         Skills required: Thermal analysis, Requirements analysis, Spacecraft, Modelling

         Nature of project: Predictions of AMOS4 satellite SMA mechanism tests’ temperatures

    Objectives:

    Calculating SMA (Shape Memory Alloy) mechanism temperatures on the thermal tests’ boundaries, according to two configurations:

    Case 1: The I/F temperature of the root hinge is fixed at -20°C; the I/F temperature of the satellite is fixed at -20°C; the I/F temperature of the yoke bracket is fixed at 40°C; the I/F temperature of the coupon GS is fixed at 60°C; and the SMA heaters are OFF.

    Case 2: The I/F temperature of the root hinge is fixed at 30°C; the I/F temperature of the satellite is fixed at 30°C; the I/F temperature of the yoke bracket is fixed at -20°C; the I/F temperature of the coupon GS is fixed at -20°C; and the SMA heaters are OFF. The Solar arrays are not modelled. SMA mechanism is modelled in stowed configuration. Then, the results of temperatures will be compared to the measured temperatures during the balance thermal tests.

    Achievements:

    Elaborated model

    Recovered SMA model

    Modelled the satellite I/F and the solar array coupon

    Created calculations cases

    Parameterised of calculations cases associated to two tests’ configurations (case 1 and case 2)

    Calculated temperatures

    Calculated SMA temperatures for two configurations

    Posted processing of temperature results

    Technical background:

    Windows XP / ESATAN-TMS, MS Word, MS Excel

     

         Skills required: Thermal analysis, Spacecraft, Testing

         Nature of project: W3B satellite thermal tests

    Objectives:

    Steering cycling and balance thermal tests

    Ensuring efficient conduct of tests

    Not exceeding the equipment’s qualification temperatures

    Reaching the equipment’s objectives’ temperatures before giving the green light to the electronic engineers to start the equipment’s performing tests during the cycling thermal tests

    Achievements:

    Controlled equipment’s temperatures

    Configured setting heater lines

    Configured setting heater lines for the E1 and E2 cases in the balance tests

    Configured setting heater lines for the cold and hot levels in the cycling tests

    Steered transition phases from hot level to cold level, and vice versa

    Conducted end-to-end tests

    Checked to ensure the heater lines are operational

    Conducted consumption tests

    Measured the real heater lines’ consumption to compare it with the theoretical heater lines’ consumption to make sure that the real heater lines’ consumption is coherent

    Technical background:

        Windows XP, Linux / Dynaworks, TMS, IHM, MS Excel

     

         Skills required: Thermal analysis, Requirements analysis, Spacecraft, Modelling

         Nature of project: Predictions of SatcomBw2 satellite flight’s final temperatures

    Objectives:

    Optimising OSR areas

    Calculating satellite flight final temperatures

    Achievements:

    Elaborated

    Used legacy satellite model from CDR as input

    Integrated model modifications carried out during the correlations in the flight final predictions model (modification of the structure nodal breakdown on the PSSE1)

    Updated dissipation power and heater lines’ thresholds

    Updated of REPEATER and SM equipment’s dissipation power of satellite

    Updated of harness dissipation

    Updated heater lines’ thresholds

    Parameterised and achieved calculation cases

    Calculated satellite temperatures for the four cases (Equinox BOL 0% Drive, Equinox BOL 100% Drive, Summer Solstice EOL 100% Drive, and Winter Solstice EOL 100% Drive)

    Posted processing and analysing results

    Modified OSR area

    Reduced the OMUX OSR area to allow this equipment to maintain the equal or superior temperature of design in cold case (Equinox BOL 0% Drive) in case of breakdown of one of heater lines

    Calculated satellite temperatures for the four cases after modification of OSR area

    Technical background:

        Windows XP, Linux / CIGAL, CORATHERM, MS Word, MS Excel

     

         Skills required: Thermal analysis, Requirements analysis, Spacecraft, Modelling

         Nature of project: Correlations of the SatcomBw2 satellite

    Objectives:

    Validating the existing model

    Optimising the satellite mathematical model to better fit the reality

    Modifying the satellite design

    Making the model more accurate to decrease the uncertainties for the flight predictions

    Achievements:

    Compared the measured temperatures during the balance tests to the calculated temperatures

    Created an Excel file that allows highlighting of the important temperature differences of equipment

    Analysed the more important temperature differences to identify their causes and reduce them

    Step 0 

    The battery and test facilities nodes are fixed at the real temperature of the thermal tests.

    The .

    Updated dissipations strongly related to the test consumption and configuration (PCU, SADM) in the model

    Updated

    Step 1

    Updated

    Calculated temperatures

    Calculated correlated model temperatures for the three E1, E2, and E3 balance cases

    Converged correlated model’s calculated temperatures to the measured temperatures

    Technical background:

        Windows XP, Linux / CIGAL, CORATHERM, MS Word, MS Excel

     

         Skills required: Thermal analysis, Spacecraft, Testing

         Nature of project: SatcomBw2 satellite thermal tests

    Objectives:

    Steering cycling and balance thermal tests

    Ensuring efficient conduct of tests

    Not exceeding the

    Reaching the equipment’s objectives temperatures before giving the green light to the electronic engineers to start the equipment’s performing tests during the cycling thermal tests.

    Achievements:

    Controlled equipment’s temperatures

    Configured setting heater lines

    Configured setting heater lines for the E1, E2, and E3 cases in the balance tests

    Configured setting heater lines for the cold and hot levels in the cycling tests

    Steered transition phases from hot level to cold level and vice versa

    Conducted end-to-end tests

    Checked that the heater lines are operational

    Conducted consumption tests

    Measured the real heater lines’ consumption to compare it with the theoretical heater lines’ consumption to ensure that the real heater lines’ consumption is coherent

    Technical background:

        Windows XP, Linux / Dynaworks, TMS, IHM, MS Excel

     

         Skills required: Thermal analysis, Requirements analysis, Spacecraft, Modelling

         Nature of project: Predictions of SatcomBw2 satellite tests’ temperatures

    Objectives:

    Calculating satellite temperatures on the thermal tests’ boundaries, according to three configurations: E1 (REPEATER OFF), E2 (REPEATER ON 100% drive), and E3 (REPEATER ON 0% drive); then, the results of temperatures will be compared to the measured temperatures during the balance thermal tests

    Achievements:

    Elaborated model

    Used legacy satellite model from CDR as input

    Withdrew satellite external equipment (antennas)

    Modelled of test facilities (70m3 vacuum chamber, IR grid, cryopanel)

    Configured setting heater lines and equipment

    Implemented heater lines’ dissipation power, equipment and harness for the E1, E2, and E3 case in the model

    Created calculations cases

    Parameterisation of calculations cases associated to three satellite tests’ configurations (E1, E2 and E3)

    Calculated temperatures

    Calculated satellite temperatures for three configurations

    Posted processing of temperature results

    Technical background:

        Windows XP, Linux / CIGAL, CORATHERM, MS Word, MS Excel

       

         Skills required: Requirements analysis, Spacecraft, Modelling

         Nature of project: Nodal breakdown of NILSAT satellite south and north CM

    Objectives:

    Performing nodal breakdown of NILSAT satellite south and north CM

    Generating the «. rad » and «. geopl » output files of south and north CM for the satellite thermal analysis

    Achievements:

    Performed nodal breakdown

    Performed the nodal breakdown from a south and north CM by considering heat pipes networks, temperature gradient areas, and reinforcements

    Elaborated the south and north CM geometry that will be used later for the thermal analyses:

    Integrated nodal breakdown in the software tool

    Performed «. rad » and «. geopl » output files of south and north CM

    Technical background:

        Windows XP / PTA2, MS Excel

     

         Skills required: Requirements analysis, Spacecraft, Modelling

         Nature of project: Modelling of W3B satellite

    Objectives:

    Modelling of the W3B satellite external thermal environment to enable inserting the satellite antennas into its environment and perform the antennas’ thermal analysis

    Achievements:

    Modelled satellite

    Recovered satellite dimensions from « SEEMAGE » file (CAD file)

    Modelled satellite and external equipment (IRES, GLOBAL HORN, GS)

    Performed nodal breakdown of satellite East, West, and Earth faces

    Numbered nodes and assignment of materials

    Technical background:

        Windows XP / CIGAL, MS Word, MS Excel

     

    THERMAL ENGINEER INTERN / Thales Alenia Space / SPACE / TOULOUSE, france              01-2007 to 07-2007

         Skills required: Thermal analysis, Requirements analysis, Spacecraft, Testing

         Nature of project: Testing of two software tools dedicated to thermal calculation; an existing circuit electronic board model was imported into the software tools to perform the tests

    Objectives:

    Assessing two circuit electronic board thermal calculation software tools: FLO/PCB and BETASOFT (now known as HyperLynx Thermal)

    Replacing the existing thermal calculation AUTOTHERM software tool

    Achievements:

    Assessed existing software tool: AUTOTHERM

    Learned and used AUTOTHERM software tool

    Tested software tool from IDEAS TMG software

    Highlighted AUTOTHERM software tool limits

    Analysed thermal engineers’ expectations:

    Discussed with thermal engineers

    Wrote and finalised requirements

    Assessed FLO/PCB and BETASOFT software tools:

    Assessed all criteria defined on the requirements for each software tool

    Imported an existing model circuit electronic board into the reference tool, IDEAS TMG

    Performed the circuit electronic board temperatures calculations with IDEAS TMG

    Modelled the same circuit electronic board with FLO/PCB and BETASOFT tool

    Performed the circuit electronic board temperatures’ calculations with FLO/PCB and BETASOFT

    Compared the temperature results obtained with FLO/PCB and BETASOFT with the reference tool, IDEAS TMG.

    Highlighted software performance for each one in the table form, which the ability to integrate with the others conception software tools

    Presented results at the thermal calculation team

    Technical background:

        Windows XP, Unix / AUTOTHERM, IDEAS TMG, FLO/PCB, BETASOFT, Lotus

     

    APPRENTICE FOOTBALLER / TOULOUSE FOOTBALL CLUB / FOOTBALL / TOULOUSE, FRANCE        08-1999 to 06-2001

    Learned the soccer profession

     

    PRE-APPRENTICE FOOTBALLER / CASTELMAUROUX / FOOTBALL / CASTELMAUROUX, FRANCE          08-1997 to 06-1998

    Improved my level of game and prepare me at the formation of professional soccer player

    Earned title of “Champion of France”, category of fourteen years old

     

    Master’s degree in Mechanics and Energy                   09-2007

    Polytech’Marseille Graduate School of Engineering (IUSTI), Marseille, France

     

    Two-year university degree in Physical Sciences                  06-2004

    Université Paul Sabatier (Toulouse III), Toulouse, France

     

    French                  Native

    English                 Fluent

     

     


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    Please also note that we are located in France. Our normal office hours are 09:00 to 18:00 Monday to Friday. France timezone is GMT+1.

     

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    We are very serious about our job seekers privacy so only legitimate recruiters and employers are eligible for a recruiter account. All subscriptions requests will be manually approved and recruiter accounts constantly monitored. Users who enter inaccurate or incomplete information will not gain access to post jobs or search resumes. Sharing of login details with a third party will result in the suspension of the recruiter's account with no subscription refund.
    Recruitment agencies are only eligible for a Gold package and recruitment agencies recruiting for companies already using Space Careers will not be accepted.

    To ensure you are approved, please include the following on your application:
    * The website address of your Company. Under construction websites will be rejected.
    * Email - Must end in @yourcompany.com. Applications using free email accounts such as Hotmail, Yahoo or Gmail will be rejected.

    Individual exceptions can be made on a case by case basis by emailing sales@space-careers.com. Accounts found not to be in compliance will be deleted.

     
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