Dr. Michael W. Martin
**** *. ****** **, *********, Texas 77539 979-***-**** *************@*****.***
SUMMARY OF QUALIFICATIONS
Eleven years of experience in the Aerospace industry in the design, testing, and operation of spacecraft.
One year of experience as a flow control valve design engineer in the Petroleum industry.
One year of experience as a Project Lead managing personnel.
EDUCATION Texas A&M University, College Station, TX
PhD – Mechanical Engineering 2014
Dissertation: “Prediction of Damage to Structure Resulting from Recirculation of Particles from a
Magnetoplasma Spacecraft Engine”
Engineering Management Certificate from Mays Business school 2011
University of New Orleans, New Orleans, LA 2002
Master of Science – Mechanical Engineering
Thesis: “Design and Construction of a Two-Dimensional Experimental Hybrid Rocket Test Bed to
Determine Regression Rate using Optical Techniques”
Bachelor of Science – Mechanical Engineering 1998
PROFESSIONAL EXPERIENCE
02/2014 – 01/2015
Schlumberger, Rosharon, TX
Mechanical Engineer
Project Lead for mechanical seal testing in high temperature and pressure environments.
Design Engineer for an ODIN flow control valve using Creo Elements® / Pro 5.0 CAD software with
GD&T.
Successfully managed project and one employee to produce seal friction estimation software.
Modeled structural loads using ANSYS simulation software.
Work resulted in a patent application for my invention of a new mechanical seal.
01/2013 – 10/2013
Qualified Technical Services, Houston, TX
Flight Controller (ADCO) for the International Space Station
Received extensive training in NASA flight systems and Russian prop ulsion.
Command-certified and performed flight controller duties in complex simulations with NASA and
contractors.
Assisted in the creation of training materials and computer interfaces for ADCO personnel.
08/2010– 01/2013
Texas A&M University, Department of Mechanical Engineering
PhD student
Modeled electrodynamic fluid flow through a rocket engine using COMSOL Multiphysics FEA.
01/2007 – 08/2010
Lockheed Martin Space Systems, New Orleans, LA
Senior Design Engineer Security Clearance: Public Trust (2009)
Designed propulsion sub-assembly and other flight components for the Orion Service Module (SM)
using GD&T with Pro/Engineer® CAD software, Wildfire, and Windchill. Produced GD&T drawings
and modeled fluid, thermal, and chemical systems in the Service Module.
Acted as project interface for Propulsion, Radiators, Camera, Instrumentation, and Mechanisms with
NASA, Lockheed Martin, and numerous sub -contractors.
2/2
05/2006 – 08/2006
NASA Goddard Space Flight Center, Greenbelt, MD
NASA/AAAS Intern
Designed and built a precision cleaning apparatus for titanium tubing used on the Solar Dynamics
Observatory (SDO) spacecraft. Saved NASA thousands of dollars in cleaning expenses.
Successfully made parts and assembled them in a Level 10 clean room and worked with the NASA
Propulsion group in the preparation and installation of piping, ducts, and flow valve systems for SDO.
01/2003 – 05/2003
Los Alamos National Laboratory, Los Alamos, NM
Research Engineer Intern
Designed, analyzed, and built piping and valves for hydraulic cooling system on the test apparatus.
Tested over 1,000 diode assemblies with capacitors, and repaired bad soldered joints.
Constructed support structures for various lab equipment.
02/1999 – 08/2002
Lockheed Martin Space Operations, NASA SSC, MS
Test Operations Engineer
Assisted in propulsion hot-fire testing of hybrid, hypergolic, and cryogenic rocket engines for NASA,
Boeing, TRW, and Lockheed Martin Michoud. Work included the design of piping, ducts, and flow
valve systems on the E-complex test stands. I worked on the TRW 650K Pintle engine, the Boeing
Consortium 250K Hybrid Rocket Demonstrator, FASTRAC, and the X-34 project.
Wrote NASA work documents and directed technicians in the performance of valve and instrument
installation, cryogenic liquid transfer, high pressure gas generation, pre -test preparation and post-test
securing and test article removal.
Supervisor during the third shift and managed over 10 engineers and technicians in support of cryogenic
transfer operations.
COMPUTER SKILLS
Creo & Pro/Engineer, Wildfire, Windchill, COMSOL Multiphysics FEA, MATLAB, FORTRAN, ADA,
Assembly, ANSYS, LabVIEW, Java, JavaScript, HTML, Jess AI, Adobe Photoshop, MS Office
TECHNICAL SKILLS
Published expert in hybrid rocket motors, both in design and operation.
Command-certified for ISS operations
Passed course in Welding from Nunez Community College, Chalmette, L A.
CNC machine programmer, operator, and trainer
Certified in Liquid Hydrogen transfer (NASA Stennis)
Award-winner for writing (both Newspaper and Fiction)
LEADERSHIP
2014 – 2015
AIAA, Houston Section, Chair