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The former chairman of the House aviation subcommittee and adviser to United Launch Alliance argues that all commercial spaceflight companies should support, rather than disrupt, the FAA's ongoing effort to streamline existing launch licensing processes. SpaceNews.com
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Wed, 13 Nov 2019 10:29:40 +0000
A NASA official warned that extended delays in finalizing a fiscal year 2020 budget for the agency could have implications for its ability to stay on schedule for returning humans to the moon in 2024. SpaceNews.com
Wed, 13 Nov 2019 00:14:41 +0000
Two astronauts are set to begin a series of spacewalks this week to repair an instrument outside the International Space Station that was never designed to be serviced in orbit. SpaceNews.com
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  • CV: Payload technical responsible as System and AIV Engineer

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    Personal information
     Name:<withheld>
     Age:<withheld>
     Country:<withheld>
     Location:<withheld>
    Contact information
     Email:<withheld>
     Phone:<withheld>
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    Candidate Profile
     Date Submitted:02-07-2014
     Last Modified:03-07-2014 (12:53)
    Job information
     Current job:Payload technical responsible as System and AIV Engineer
     Employment Term:Permanent
     Job location:Europe only
     Date available:within a month
     Industry:Satellite Manufacturers and Subcontractors
     KeywordsSpace System Engineer AIV manager Engineer ECSS Electrical design Test Engineer Labview Rational DOORS Test Campaigns Quality assurance RAMS Technical management Definition of requirements and specifications System and architectural design A
    CV

    EMPLOYMENT HISTORY:

    12/2010-present 

    Company/ Institution: Instituto Nacional de Técnica Aeroespacial (INTA)
    Department: Space Programs Department  
    Project: Mercury Imaging X-ray Spectrograph (MIXS), an X-ray Telescope and Collimator onboard of ESA Bepi Colombo mission. 
    Position: Payload technical responsible as System Engineer and  Assembly, integration and verification (AIV) manager Engineer

    Aims and tasks:    

    • Technical management of MIXS payload at INTA (Focal plane assembly, MIXS DPU and PSU and inter-unit harness)
    •    Definition of payload requirements and specifications.
    •    System and architectural design and analysis. 
    •    Manufacturing, assembly and integration of MIXS STM, EM, QM and FM at instrument level. 
    •    Full qualification of MIXS:  System qualification (STM, EM, QM) and acceptance (FM) test campaign management: environmental test campaign (vibration, thermal, thermal-vacuum, shock), EMC test campaign, functional test campaign. Analysis and report of acceptance test results.
    •    Treatment of quality assurance aspects.
    •    Integration campaign at S/C as design authority.
    •    Subcontractors and partner´s technical management.


    09/2010-12/2010 

    Company/ Institution: National Institute for Aerospace Technology (INTA)  
    Department: Space Programs Department  
    Project: OPTOS (Cubesat)
    Position: Mechanical System Engineer and AIV Engineer

    Aims and tasks: 

    • Mechanical and thermal analysis at system level. 
    • System design of mechanical and thermal vacuum test and electrical functional test during OPTOS QM test campaign. 

    06/2010-09/2010
     
    Company/ Institution: AERNNOVA
    Department: Structural design and mechanical analysis
    Project: SEOSAT/Ingenio
    Position: Structural design and mechanical analysis engineer

    Aims and tasks:    

    •   Structural design and mechanical analysis of the secondary mechanical structure of the SEOSAT satellite for PDR phase. 

    03/2010-06/2010 

    Company/ Institution: ALESTIS AEROSPACE
    Department: I+D+i  (R&D)
    Project: CENIT/TARGET
    Position: Research and development engineer

    Aims and tasks:   

    • R&D activities coordination for CENIT/TARGET project. 

    EDUCATIONAL QUALIFICATION:

    04/2012-07/2012 

    Academic Degree: Master in Satellite Technology
    Master course: System engineer - Space segment ( 5 credits)
    University: Universidad Politécnica de Madrid (UPM)
    Qualification: With Honors 

    10/2010-06/2011 

    Academic Degree: Master in Science and technology from Space  (60 ECTS credits )
    University: Universidad de Alcalá (UAH)
    Department: Space Research 
    Qualification: With Honors

    02/2009-12/2009 

    Academic Degree: Pegasus Award
    Subject: Master Thesis in new high performance thermoplastic for use as matrix in glass/carbon fiber reinforced composite laminates.
    University: TU Delft University (Netherlands), Faculty of Aerospace Engineering.
    Department: Design and Production of Composites Structures
     
    2001-2009
     
    Academic Degree: Ingeniero Superior Aeronáutico (Aerospace Engineer)
    Specialty: Aircrafts and spacecrafts (A2)
    Centre: Escuela Técnica Superior de ingenieros Aeronáuticos (ETSIA)
    University: Universidad Politécnica de Madrid (UPM)

    06/2008-10/2008 

    Fellowship:  JAE programme
    Organization: Consejo Superior de Investigaciones Científicas (CSIC)
    Purpose: Development of thermo/mechanical design of the PCM (Power Converter Module) integrated in BELA (BepiColombo Laser Altimeter) as part of the international scientific payload of BepiColombo mission (ESA-JAXA).
    Host institution: Instituto de Astrofísica de Andalucía (IAA) 
    Department:  Department of Solar System

    ANY OTHER SKILLS:

    Training courses:

    03/2013 

    Subject: Uncertainty in Measurements
    Place: Metrological Laboratory at INTA
    Purpose: Calculation of uncertainty in measurements. Monte Carlo Method vs GMU analysis. Uncertainty in technical specifications. Calibration of instruments. 
     
    10/2012 

    Subject: Advanced applications for FEM: modeling of mechanical joints and contact
    Place: Department of structural analysis at INTA
    Purpose: Modelling of bolted, riveted, welded and contact joints.

    02/2012 

    Subject: Electromagnetic Compatibility (EMC) testing.
    Place: Environmental tests laboratory at INTA
    Purpose: Conducted and radiated electromagnetic compatibility tests for spacecraft.  

    11/2011 

    Subject: Post-processing of FEM results
    Place: Department of structural analysis at INTA
    Purpose:
    •   Processing of Average/derive and derive/average, extrapolation and averaging Methods.  
    •   Failure Criteria.

    10/2011 

    Subject: Space mechanical environmental testing.
    Place: Environmental tests laboratory at INTA 
    Purpose:
    • Vibration test in electro mechanic system: Theoretical and practical parameters.
    • Mechanical tests for spacecraft.

    Languages Skills:

    Spanish: Native
    English: High Level 

    Computer skills and competences:

    Operated Systems: LINUX and WINDOWS
    Programming Languages: Fortran 95 , MatLab, Maple, 
    Computer Assisted Design: SolidEdge and Microstation, CATIA V5 R19 (Design, Analysis and Advanced Surfaces Modules)
    Mechanical Analysis: NASTRAN/PATRAN, ANSYS
    Thermal Analysis: ESATAN/ESARAD
    Computational fluid dynamics (CFD): ANSYS-CFX (Solver and post-processor)
    Mission simulation tool: STK
    Others: Package Open Office and Microsoft Office (Project, Word, Excel, PowerPoint), Latex and Lyx (text editor program), TecPlot (Visualizer), LabView (Interface to acquire external-device data).

    International Congress: 


    MERCURY IMAGING X-RAY SPECTROMETER (MIXS) IN BEPICOLOMBO MISSION: ENVIRONMENTAL TESTS
    62nd (IAC) International Astronautical Congress 2011 (Cape Town, Sudafrica, 2011) 

    Reference can be provided upon request


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