Structural engineer

Alb*** ***** (XX años)
Space Structural Optimization Engineer en CITD
Carlos III University of Madrid - UC3M
Madrid,
Madrid
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Experiencia
Space Structural Optimization Engineer
CITD
sep 2017 - Actualmente
Space structure analysis and additive manufacturing in Airbus Space projects.

•	Structural analysis of JUICE spacecraft (primary and secondary structure) in CDR and MRR phases.
•	Structural topology optimization of parts for additive manufacturing.
•	Structural analysis of H3 launch vehicle Payload Adapter Fitting (PAF) for HTV-X spacecraft.
•	Design and analysis of MGSE and test set-ups.
•	Static and dynamic analysis.
•	Performing testing phase of Jason-CS/Sentinel-6 spacecraft.
•	Creation and validation of FEM models.
•	Documentation: structural analysis report.
Space Structural Engineer
ATOS
dic 2016 - sep 2017
Space structure analysis in Airbus Space projects.

•	Structural analysis of JUICE spacecraft in PDR phase.
•	Structural analyses of Jason-CS/Sentinel-6 spacecraft in CDR phase.
•	Static and dynamic analysis.
•	Creation and validation of FEM models.
•	Fatigue analysis of cleats.
•	Documentation: structural analysis report.
F&DT Stress Engineer
ATOS
abr 2016 - dic 2016
Fatigue and damage tolerance analyses.

•	F&DT analyses of A350-900 XWB S19 (MSN5 and MSN74).
•	Analyses of spectra, fatigue lives and crack propagations.
•	Metallic frames and joints analyses (inner caps, support holes, mouse holes and skin joint).
•	Knowledge of ISAMI (F&DT modules).
•	Documentation: certification reports and ACDs.
Stress Engineer
ATOS
nov 2012 - mar 2016
Airbus A380 structures analysis.

•	Modifications and concessions of Airbus A380 (section 19, 19.1 and HTP).
•	Parametric evaluation of rear corner splices (Section 19).
•	Studies of the Section 19 upper corner skin area residual strength, as result of the appearance of some cracks.
•	Creation and modification of FEM models.
•	Justification of section 19.1 parts which have been affected by curing cycle deviation.
•	Pull-through justification of the frame-skin joint of Section 19.
•	Frame riveting justification of Section 19 for aircraft A380-800, adding global thermal loads.
•	Study for the replacement of BMI to Epoxy in Section 19.1.
•	Justification of section 19 for Russian Certification (loop loads)
•	Correlation of GFEM and test results.
•	Development of tools for data processing by VBA/Excel.
•	Airbus tools knowledge.
•	Documentation.
Formación
Degree in Mechanical Engineering
Carlos III University of Madrid - UC3M
sep 2008 - jul 2013

          
        
Idiomas
Spanish - Native language
English - Upper intermediate level
French - Upper intermediate level