AWARDS

PATRICK HARVEY MECHANICAL ENGINEER

P H O N E : 5 0 2 -5 23 -8 9 3 2

E M A I L : pa tr ick .g .ha rve y @ gma i l .co m

WE B : www.l inke d i n . co m/ in/ha rve ypa t r ic k/

AD D R E S S : 7 4 Ba rne s Ct , Ap t 7 0 8 , S ta nfo rd , CA, 9 4 3 0 5

Colorado Engineering Council Certificate of Merit - awarded to the top 3 graduating class (~300). Candidates

must excel academically, show strong leadership, community involvement and strong moral character.

Tau Beta Pi Engineering Honors Society, CSU Chapter: President, (May 2014-May2015)

American Institute of Aeronautics and Astronautics (AIAA): Activities Chair, (May 2013-May2014)

EDUCATION

EXPERIENCE

PROJECTS

LEADERSHIP

Stanford University, Palo Alto, CA

MS in Aeronautical and Astronautical Engineering

Colorado State University, Fort Collins, CO

BS in Mechanical Engineering with Honors, Cum Laude BS in Engineering Science with Honors, Cum Laude

Fundamentals of Engineering Exam

Anticipated: June 2017

GPA: 3.99

Graduated: May 2015

GPA: 3.92

Date Passed: 01/15/2015

May 2013-Aug 2013

Technical Analyst Aviation Security, ANSER

Dept. of Homeland Security

Falls Church, VA

Assessed the impact of growing comercial drone capabilities over and impact on

domestic security, submitted white paper highlighting expected development dates

and proposed solutions to minimize risks.

Combined engineering technical analysis with human behavioral studies to predict

future threats to domestic aviation to inform DHS policy decisions.

June 2016-Sept 2016

Propulsion Intern Advanced Concepts

The Boeing Company

Long Beach, CA

PATENT PENDING: Developed an advanced propulsion integration concept, patent

being pursued by Boeing.

Developed and automated engine modeling tool in T-MATS , gave detailed air flow

data at all operating points, modeled dynamic performance for a full flight cycle.

Performed fuel burn analysis on advanced propulsion concepts, results used for

basis of future studies and to inform research collaboration with engine companies.

May 2014-Aug 2015

Mechanical Intern Aerospace and Defense

Group

Keysight Technologies

Loveland, CO

Collaborated with multidisciplinary team to design test systems for aerospace

applications; specifically improved thermal management and simplified integration.

Oversaw changes in supply chain and integration for mechanical components to scale

up production from 3 units a month to over 20 while still meeting deadlines.

Communicated with technicians to resolve production issues on the floor by making

design or procedural changes in order to reduce delays.

January-June 2016: Rocket Combustion Chamber Temperature Measurement, Stanford Created an experimental spectrometry method to use sodium D-line reversal to determine temperature

in hybrid rocket combustion chambers, successfully validated method with hot fires.

Collected data and collaborated on a paper submitted for publication at the Joint Propulsion Conference.

January-June 2016: Experimental Nytrox Rocket Design Project, Stanford Developed prototype hybrid motor using nytrox combining the self-pressurizing capabilities of nitrous

and the performance of oxygen. Specifically in charge of all plumbing, avionics and recovery systems.

Successfully test fired rocket and achieved a thrust of approximately 650 lbf.

Launch delayed to early 2017 due to sensor failure. Will be first ever flight of a nytox motor.

June 2014-May 2015: High Heat Flux Thermal Management, CSU/Lawrence Livermore National Lab Increased heat pipe cooling capacity through advanced miniaturized manufacturing techniques.

Designed and conducted experiments to investigate internal fluid flow and heat transfer of heat pipe.

Verified developed theoretical model with results and used it to inform future design iterations.