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CV: Payload technical responsible as System and AIV Engineer
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Date Submitted: Last Modified: Current job: Employment Term: Job location: Date available: Industry: Keywords
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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