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| Year of birth |  | 1978 |
Permanent/Home Location/Address |
| City or Town | | Redondo Beach |
| Country | | USA |
Current Location/Address |
| Country | | USA |
Languages |
| Primary Language | | Fluency |
| English | | Read, write and speak fluently |
Nationalities |
| Main Nationality | | USA |
| Other Nationality | | URUGUAY |
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Experience Classification |
| Job Function | | Years Experience |
| Aeronautical Engineer | | 9 |
| Aerospace Engineer | | 9 |
| Stress Engineer | | 9 |
| Design Engineer | | 9 |
| Mechanical Engineer | | 9 |
| Industry | | Years Experience |
| Aerospace and Aviation | | 9 |
Qualifications |
| Highest Qualifications | | Masters |
| Qualification | Subject | Establishment/Country | Year |
| Masters or Higher | Aerospace Engineering | Stanford University/USA | 2002 |
| Degree | Mechanical and Aero Engineering | University of California, Davis/USA | 2001 |
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Computer Skills and Software Used |
| PATRAN, NASTRAN, Ansys Workbench, FEMAP 10.1, ProMechanica Wildfire 2.0, FORTRAN, Perl, SLIM, Vision, Mathcad, SolidWorks, Catia V5, Unigraphics NX 4.0, and Standard Microsoft Office/Windows Software. |
Work Locations |
| Are you willing to move or relocate? | |
Yes - I will travel domestically
Yes - I will relocate domestically
Yes - I will travel internationally
Yes - I will relocate internationally | |
Availability |
| Start Immediately? | | Available Now |
Ideal Next Job |
| International position working primary structure on commercial, military, or space vehicle. Open to all work locations, open to all offers. |
Required Salary & Conditions |
| Open to all offers. |
Employment History |
| Total Years of Work Experience: | | 9 |
| Commenced Full Time Work: | | 2001 |
| Name | | Northrop Grumman Space Technologies |
| Job Title: | | Engineer |
| Duration | | From : 2009 To: |
Summary |
Extensive experience using PATRAN/NASTRAN, Ansys Workbench, FEMAP 10.1, ProMechanica Wildfire 2.0, Catia V5, Unigraphics NX 4.0, UNIX, and Excel.
Strong knowledge of structural analysis principles, classical stress analysis, classical laminate analysis methods, fatigue and fracture analysis, layout sizing, load path assessment, and weight control.
Experience creating large, detailed, FEMs of composite and metallic structure for linear/non-linear analysis, frequency response, and stability.
Experience providing quick turn around dispositions in support of assembly line tags and non-conformances.
Extensive experience creating detailed analysis documentation for customer review. |
Work Experience |
Space Exploration Technologies, Hawthorne CA, 6/2009 - Present
Engineer, Falcon 9 Rocket
Responsible for design and integration of 1st Stage recovery system, including: design layout, structural analysis, fabrication and supplier selection, assembly, and testing of all components.
Extensive interaction with parachute supplier to ensure their on-time product delivery and execution per contract.
Northrop Grumman Corporation (via Pacific Crossings LLC), El Segundo CA, 2008 – 6/2009
Structural Analyst, F-35 Program Center Fuselage IPT
Static and DaDT layout and sizing of primary structure, including Center Fuselage main Fuel Floors.
Extensive FE modeling of “contact” behavior of Lift Fan Mounts for detailed Fail-Safe DaDT analysis.
Lockheed Martin Corporation (via Multax Systems Inc), Palmdale CA, 2006 – 2007
Structural Analyst, F-35 Program Outboard Wing and Control Surfaces IPT
Principal engineer for primary load path structure (Wingfold Rib) of Outboard Wing Section of CV variant, performing static and DaDT sizing.
Principal engineer for various pieces of primary metallic structure of Outboard Wing box as well as bushings, bearings, hinges, linkages, and composite control surface seals.
Performed structural analysis and layout on numerous control surfaces of the Control Surfaces and Edges IPT, analyzing composite skins, honeycomb core, bond-lines, and interfaces.
Northrop Grumman Corporation, El Segundo CA, 2002 – 2006
Structural Analyst, F-35 Program Center Fuselage IPT
Principal engineer for composite Chine Longerons for Conventional (Air Force), Short Take-Off (Marines), and Carrier Variant (Navy) aircraft, overseeing and mentoring less experienced engineers. Responsible for joint/load path concepts, layout sizing, detailed analysis, weight control, and detailed analysis documentation.
Responsible for initial layout of all fore/aft structure in Aft Duct IPT for A-1 CTOL variant. |
Last Updated on 03-Apr-10
-- End of CV/Resume --
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