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  • CV: Founder and Thermal Engineer

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    Personal information
     Name:<withheld>
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    Candidate Profile
     Date Submitted:13-02-2018
     Last Modified:29-12-2018 (07:38)
    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
     KeywordsHe has been in the field of spacecraft for the past ten years. He has performed his duties as a senior thermal engineer, where he excels in the sub-field of thermal analysis and thermal tests. These areas are his special
    CV

    CAREER OBJECTIVE

    Founder / Thermal Engineer

     

    SKILLS & EXPERTISE

    Thermal, heat transfer

    Spacecraft and satellite subsystems’ 3D modelling

    ESATAN-TMS thermal modelling suite

     

    INTERVENTIONS

    Thermal engineering / Space industry

     

    TECHNICAL DOMAINS

    Operating system: Windows, Linux

    Office applications: MS-Office, Lotus

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

     

    WORK EXPERIENCE

    FOUNDER / ALPHID LTD / SPACE / HARWELL, UK                                      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 Luna-Resource Lander LEIA (LIDAR for Extra-terrestrial Imaging Applications)

    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:

    - Elaborating 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:

    - Elaborating 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 AERO / 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 equipment’s and heater lines’ operational configuration are updated in the model.

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

    - Updated equipment’s dissipations in the model

    Step 1

    - Updated conductive coupling between Helium tank and PIA

    - Updated structure nodal breakdown on the PSSE1

    - Updated North SM and South CM conductivity value

    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 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, 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 (TFC) / FOOTBALL / TOULOUSE, FRANCE                                08-1999 to 06-2001

    - Learned the soccer profession

                                                                

    PRE-APPRENTICE FOOTBALLER / REGIONAL FOOTBALL CENTER (CRF) / 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

     

    EDUCATION

    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

     

    LANGUAGES

    French                  Native

    English                 Fluent

     

    PUBLICATIONS

    REMOVAL OF THERMAL ENERGY FROM SPACECRAFT ELECTRONICS / EMPS WORKSHOP / YVERDON-LES-BAINS, SWITZERLAND                  26-04-2018

    Description: Requirements analysis, Spacecraft, Modelling Spacecraft electronics are critical satellite subsystems that ensure the success of the space mission. Therefore, it is fundamental to build thermal models of spacecraft electronics to implement and test the thermal design of the spacecraft electronics at an early stage before operating them in space.

    Link to publication: http://emps.port.ac.uk/documents/EMPS-9%20documents/download/S2-3.pdf

     

    THERMAL MODELLING PROCESS / EUROPEAN SPACE THERMAL ANALYSIS WORKSHOP / NOORDWIJK, NETHERLANDS                 20-11-2012

    Description: To emphasis the strength and flexibility of ESATAN-TMS a demonstration of the complete thermal modelling process shall be given. The latest version of ESATAN-TMS shall be used, with particular emphasis on the new features in the release.

    Link to publication: https://exchange.esa.int/download/thermal-workshop/workshop2012/parts/TMSCAD.pdf

     

    CERTIFICATION

    CERTIFICATE OF RECOGNITION / ALLIED ACADEMIES / ROME, ITALY           2018 to Present

     

    COURSE

    THERMICA TRAINING / AIRBUS DEFENSE AND SPACE / TOULOUSE, FRANCE          09-2017

    ADVANCED PRESENTATION SKILLS / NLP / EVESHAM, UK                                                 2011

     

    HONOR & AWARD

    GROUP HEAD AWARD / ITP AERO / LEICESTER, UK                        11-2011

    As part of the Company's ongoing nomination process I would like to give you a Group Head Award for all your recent work on the thermal modelling of TROPOMI instrument and meeting the needs and requirements of Dutch Space (now known under the name of Airbus Defence and Space Netherlands B.V.).

    For the last four weeks you have been working in Leiden, Holland, providing thermal support in modelling a Tropospheric Ozone Monitoring Instrument using ESATAN-TMS. The work has progressed very well and the feedback received from Dutch Space has been really good resulting in more work for us.


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