Experience

Virgin Galactic

• United States
• Aviation and Aerospace Component Manufacturing
• 700 & Above Employee

• Specialist Stress Engineer

  • Mar 2022 - Present



The Spaceship Company

• United States
• Aviation and Aerospace Component Manufacturing
• 1 - 100 Employee

• Senior Stress Engineer

  • Oct 2020 - Present



Freelance

• Senior Stress Engineer

  • Jan 2017 - Oct 2020



Collins Aerospace

• United States
• Aviation and Aerospace Component Manufacturing
• 700 & Above Employee

• Senior Stress Engineer

  • Apr 2017 - May 2020

  Interior structure static stress and stability analysis for Large Commercial Aircraft. Use of conventional "hand calculations" and advanced Patran/Nastran FEM techniques such as transient nonlinear analyses. Interior structure static stress and stability analysis for Large Commercial Aircraft. Use of conventional "hand calculations" and advanced Patran/Nastran FEM techniques such as transient nonlinear analyses.



B/E Aerospace

• Aviation and Aerospace Component Manufacturing
• 700 & Above Employee

• Senior Stress Engineer

  • Nov 2012 - Apr 2017

  Large Commercial Aircraft reconfiguration structure static stress and stability analysis. Use of conventional "hand calculations" and Patran/Nastran FEMs.

• Senior Stress Engineer

  • Nov 2012 - Apr 2017

  Large Commercial Aircraft interior structure static stress and stability analysis. Use of conventional "hand calculations" and Patran/Nastran FEMs.



Boeing

• United States
• Aviation & Aerospace
• 700 & Above Employee

• Stress Engineer

  • Nov 2010 - Nov 2012

  Large Commercial Aircraft primary composite structure static, stability and damage tolerance analysis. Use of conventional "hand calculations" and Patran/Nastran and Abaqus FEMs. Large Commercial Aircraft primary composite structure static, stability and damage tolerance analysis. Use of conventional "hand calculations" and Patran/Nastran and Abaqus FEMs.



B/E Aerospace

• Aviation and Aerospace Component Manufacturing
• 700 & Above Employee

• Stress Engineer

  • Jan 2008 - Aug 2008

  A300 Passenger to Freighter conversion. FEM and loads analysis.

• Stress Engineer

  • Jun 2006 - Jan 2008

  SUKHOI Superjet cargo doors structure FEM development, stress analysis (static and stability) and certification reports.



Boeing

• United States
• Aviation & Aerospace
• 700 & Above Employee

• Stress Engineer

  • Nov 2004 - Jun 2006

  Boeing 737-900ER Wing box, leading and trailing edges and main landing gear attachments stress analysis (static, fatigue and stability) and reports. Boeing 737-900ER Wing box, leading and trailing edges and main landing gear attachments stress analysis (static, fatigue and stability) and reports.



Airbus

• France
• Aviation and Aerospace Component Manufacturing
• 700 & Above Employee

• Lead Stress Engineer

  • Jul 2002 - Nov 2004

  Management and leading of Cadtech’s work team for Airbus Spain’s A380 Composite Wing Ribs project. (Preliminary sizing and studies, detailed composite wing-ribs FE Models generation and sizing and stress justification reports and FEMs validation).Through CT Ingenieros.

• Stress Engineer

  • Nov 2001 - Jul 2002

  A380 Section 19 preliminary sizing (frames, fittings, beams).Through CT Ingenieros.

• Lead Stress Engineer

  • Jun 2000 - Nov 2001

  T.A.N.G.O. Project - Wing Work Package II:Management and leading of the project assigned to Cadtech by the European Commission; Sizing and design of Composite Wing-box test dummy boxes.Through CT Ingenieros.



Spanish Red Cross

• Non-profit Organizations
• 400 - 500 Employee

• Emergency Technician and Lifeguard

  • Jan 1993 - Jan 2001

  Paramedic, ambulance driver, and radio operator in emergency coordination centers. Paramedic, ambulance driver, and radio operator in emergency coordination centers.



EADS Defence & Security

• Defense and Space Manufacturing
• 1 - 100 Employee

• Stress Engineer

  • Feb 2000 - Nov 2000

  Eurofighter wing secondary structure stress justification and certification reports. Through CT Ingenieros. Eurofighter wing secondary structure stress justification and certification reports. Through CT Ingenieros.



THE CT ENGINEERING GROUP

• Spain
• IT Services and IT Consulting
• 700 & Above Employee

• Stress Engineer

  • Sep 1999 - Feb 2000

  Dornier 728 Jet ProjectVertical Tail Plane:- Preliminary sizing and design.- VTP FE Model generation. Documentation and validation.- Sizing of specific elements (rib, shear-ties…).- Development of training courses for Cadtech’s Stress Team.

• Design Engineer

  • Feb 1999 - Sep 1999

  Dornier 728 Jet Project.- Vertical Tail Plane: Preliminary design and modeling of VTP to fuselage fittings. CATIA v4.2.0.Airbus A340-600 Project.- Horizontal Tail Plane Trailing Edge: Documents generation, manufacturing and assembly drawings...- Elevator: Preliminary studies and 3D models, drawings and documentation generation. Manufacturing and assembly drawings.