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Engineer Design

Location:
United States
Posted:
April 01, 2012

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Resume:

KEITH F. PETERSEN

**** ***** ******** **** *****

Tucson, Arizona 85718-5452

Cell: 1-520-***-****

Email: ********@*******.***

_____________________________________________________________________________________

AREAS OF Airframe Structural Design Molded Plastic Parts Pro/ENGINEER Rel. 12-WF 4.0

KNOWLEDGE Conceptual Design Sheet Metal (20,000+ hours)

Systems Design Analysis Unigraphics/SIEMENS Ver.9-NX6

Avionics Systems Composites (13,000+ hours)

E-M Packaging / Wiring Military Standards SolidWorks 2009

Heavy Castings / Forgings Geometric Tolerances AutoCAD

Hydraulic Systems ASME Y14.5M -1994 3-D Solid Modeling

NASA Standards MIL-STD-100 Advanced Surfacing

Pro/Engineer Pro/SHEETMETAL Pro/PIPING Pro/FEATURE

Modules Utilized Pro/ASSEMBLY Pro/INTERLINK Pro/SURFACE

Pro/MECHANICA Pro/WINDCHILL Pro/CABLE

PDM/Link Pro/Windchill Aero/PDM

Moving mechanical mechanisms - Reverse engineering of existing products

Weldments of both tubing and plate - Styling of cosmetic or irregular surfaces

Plastic molded parts and rapid prototypes - Job shop fabrication drawings

Proficient with Windows OS, MS Office (Excel, Word, Outlook, PowerPoint, etc.)

CAREER DEVELOPMENT

02/10 – 11/11 Senior Mechanical Engineer – Aerojet Corporation, Sacramento, CA

I was assigned to a small group of engineers to design and analysis propulsion sub-

system equipment to be used for a new super-sonic cruise missile design. This includes

E/M packaging, metallic primary airframe structures, incorporating composite materials,

working with complex machined components and managing large assemblies through PDM

. Also, working with evaluating various equipment configurations, cost and weight reduction,

interfacing with vendors, creating presentations and conduct design reviews. All is being

performed on a SIEMENS NX6 CAD/CAE system.

08/08 - 02/10 Senior Design Engineer – General Dynamics Corporation, Westminster, MD

Assigned to the Environmental Controls department for the new Expeditionary Fighting

Vehicle (EFV). My responsibilities included designing and developing a quick disconnect,

replaceable auxiliary cooling system. The project included mounting pumps includes,

valves, sensors and tubing on a module pallet. All work was being performed on a

Pro/ENGINEER CAD/CAE system.

02/08 - 08/08 Senior Design Engineer – Paragon Space Development Corporation, Tucson, AZ

Responsibilities included designing and routing various tubing and ducting components

for the new generation Orion spacecraft. The systems involved environmental controls

and thermal dissipation. Also participated in feasibility studies, proposal development &

mentoring junior engineers. All work was being performed on a Solidworks

CAD/CAE system.

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KEITH F. PETERSEN

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06/07 - 02/08 Design Engineer – Jacobs Engineering, Clear Lake, TX

Assigned to a small group of engineers to design and analysis the new Portable Life

Support System (PLSS). This system will be used to traverse Lunar and Martian surfaces.

Conceptual design includes feasibility studies and rapid prototypes for the thermal control

system of the new spacesuit development. This include machined stainless steel

housings, E/M packaging, electronic valves and routing cables. All work included

interfacing with NASA and maintaining specification requirements. All work was being

performed on a Pro/ENGINEER CAD/CAE system.

04/05 - 06/07 Aircraft Design Engineer – Honeywell Corporation, Tucson, AZ

Functions included the design and modification of aircraft cabin pressure control systems

Also, assigned to the KEI project to work on the thrust vector control EMAC systems.

Components comprise of pressure relief valves, E/M packaging for electronic controllers,

sensors, cables and printed circuit boards. Also sheet metal housings and aluminum

machined structures. All work was being performed on a Pro/ENGINEER CAD/CAE system.

11/02 -10/04 Structural & Payload Design Engineer – Northrop Grumman, San Diego, CA

Responsibilities included designing and routing hydraulic systems for the advanced

Global Hawk unmanned reconnaissance aircraft. Work entailed building installation

assemblies, choosing various hardware, making calculations & interfacing with primary

primary structure. Components include pumps, coolers, sensors and standoffs. All

work was being performed on a Pro/ENGINEER CAD/CAE system.

02/02 -11/02 Structural Engineer – United Defense, York, PA

Assigned to design and develop structural weldments for a new armament re-supply

module. Work involves using sheet metal, extrusions and plate steel. Also responsible

for reducing part count and simplifying manufacturability. All work was being performed

on a Unigraphics 2 CAD/CAE system & Pro/ENGINEER CAD/CAE system.

10/00 - 02/02 Mechanical Engineer – Novellus Systems Incorporated, Wilsonville, OR

Worked in a cross-functional team environment on Semi-Conductor capital equipment

design. Proposing solutions to difficult technical issues associated with specific projects.

This includes machine design & instrument controls. Particularly large frame assemblies

& robotic mechanisms. All work was performed on a Pro/ENGINEER CAD/CAE system.

01/99 – 09/00 Aerospace Engineer – Lockheed/Martin, Goodyear, AZ

Primary responsibilities included designing electronic chassis & wave-guides for

advanced radar systems. This work included incorporating printed circuit boards,

routing cables & machined chassis and sheet metal brackets. All work was being

performed on a Pro/ENGINEER CAD/CAE system.

5/96 - 12/98 Aircraft Engineer - Raytheon Corporation, Waco, TX

Designed environmental systems & structural modifications for executive aircraft

interiors. This entailed designing special housings & ducts, incorporating complex

surfaces. Also, developed early detection systems for a Boeing 747 - SP aircraft. All

work was performed on a Pro/ENGINEER CAD/CAE system.

EDUCATION Bachelor of Science, Mechanical Engineering

University of Wisconsin - Milwaukee, Wisconsin

CLEARANCE Active



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