FXB wintertime
François-Xavier Bagnoud (FXB) building - home of University of Michigan's Aerospace Engineering Department, located on North Campus. The FXB building was built in 1991 and contains 90,000 sq. feet of laboratories, classrooms, faculty, staff, and graduate student offices.
 
Laboratory Director:
Alec Gallimore
Affiliated Faculty:
Iain Boyd
Paul Drake
Brian Gilchrist
Post-Doctorate Fellow:
Tim Smith
Graduate Students (Candidates):
David Huang
Thomas Liu
Robert Lobbia
Michael McDonald
Bailo Bah Ngom
Sonca Nguyen
Rohit Shastry
Laura Spencer
Ricky Tang
Graduate Students (Pre-Cand.):
Roland Florenz
Raymond Liang
Adam Shabshelowitz
Prior Doctoral Graduate Students:
John Foster
Lyon King
Colleen Marrese
Sang-Wook Kim
Frank S. Gulczinski III
J. L. Van Noord
M. T. Domonkos
G. J. Williams Jr.
James M. Haas
Tim Smith
Brian E. Beal
Richard R. Hofer
P. Y. Peterson
Mitchell L. R. Walker
Daniel A. Herman
Joshua L. Rovey
Allen L. Victor
Jesse A. Linnell
Prashant Patel
David Kirtley
Bryan Reid
Kristina Lemmer
Daniel Brown

 

 

North Campus Map
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Personnel Listing | October 2007

Laboratory Director:
Arthur F. Thurnau Professor Alec D. Gallimore
DR. ALEC D. GALLIMORE is Arthur F. Thurnau Professor of Aerospace Engineering at the University of Michigan where he directs the Plasmadynamics and Electric Propulsion Laboratory. Professor Gallimore is also an Associate Dean at the Horace H. Rackham School of Graduate Studies where he helps oversee the graduate portfolio of over thirty departments in engineering, the physical sciences, and mathematics. Professor Gallimore is also on the faculty of the Applied Physics program at Michigan, is the director of the NASA-funded Michigan Space Grant Consortium, and is project director of the NSF-funded Michigan AGEP Alliance. He received his B.S. in Aeronautical Engineering from Rensselaer, and his M.A. and Ph.D. degrees in Aerospace Engineering from Princeton. His primary research interests include electric propulsion, plasma diagnostics, space/re-entry plasma simulation, use of plasma for energy production and environmental remediation, and nano-particle physics.
Affiliated Faculty:
Professor Iain D. Boyd
Professor R. Paul Drake
Professor Brian Gilchrist
Post-Doctorate Fellow:
Dr. Tim Smith
Tim Smith is a postdoctoral researcher at PEPL and a lecturer in the UM Aerospace Engineering department. For his dissertation research, he developed and validated a novel method for deconvolving xenon ion velocity distributions from laser-induced fluorescence (LIF) spectra, allowing unprecedented nonintrusive measurements of Hall thruster and ion engine plumes. Dr. Smith has 9 years of vacuum facility experience (with Hall thruster, ion engine, and hollow cathode tests) and 17 years of test experience with optical diagnostics for fluid dynamics, both passive (using emission spectroscopy) and active (LIF and optogalvanic spectroscopy with ring dye and extended-cavity diode lasers). Dr. Smith was the Principal Investigator on AFOSR program to design a magnetic deflector system to protect spacecraft laser communications systems from Hall thruster plume charge-exchange ions. He was also PI (in cooperation with Penn State) on a NASA effort to develop a low-intrusive fiber-optic plug for reentry vehicle TPS materials. His current research interests center around the modeling, development, and validation of advanced optical diagnostics for electric propulsion (EP) systems.
Graduate Students (Candidates):
David Huang,    
David Huang is a second year Aerospace student (as of Fa2007) specializing in laser induced fluorescence (LIF) diagnostics on Hall-Effect thrusters. David completed his undergraduate studies as a Mechanical/Nuclear Engineer at UC Berkeley. While at Berkeley, he worked on multi-scale stress analysis for the heat exchanger of a fourth generation High-Temperature Reactor design. That was when he learned his preference towards experimental research as opposed to simulation research. Over the summer, David worked on collecting experimental Zeeman-hyperfine splitting data for the Xenon I 834.7nm line. He also worked on collecting axial velocity profile of neutral and ionic Xenon via LIF for a 6kW laboratory research hall thruster. David’s planned thesis topic includes three-axis LIF on a 6kW laboratory hall thruster, demonstration of the use of Cavity Ring Down Spectroscopy (CRDS) for studying BN sputtering, possible combined use of LIF and CRDS to determine BN flux, and possible use of LIF to determine the velocity profile of doubly ionized Xenon. The ultimate goal of his thesis is to find out why a 6kW laboratory hall thruster can achieve an efficiency much higher than previous hall thrusters and any implications this may have on the life of the thruster.
Thomas Liu,    DOD Fellow
Thomas Liu received both his bachelor's and master's degrees in aerospace engineering from the University of Michigan (UM). He first began work with electric propulsion as an undergraduate researcher on the Field Emission Get-away-special Investigation (FEGI) project, a Space Shuttle payload and cold cathode testbed from the UM Student Space Systems Fabrication Laboratory (S3FL). His research interest in improving field emission cathode technology also encompasses the field of micropropulsion systems, and he is currently doing developmental research on the Nanoparticle Field Extraction Thruster (NanoFET), a nanoparticle electrostatic accelerator concept with the potential to become a high efficiency, scalable, variable specific impulse thruster. From personal experience, he is a strong proponent of providing undergraduate students with research and systems design-build-test-fly experiences, such as the ZESTT (Zero-g ElectroStatic Thruster Testbed) project testing the feasibility of NanoFET design concepts in microgravity.
Robert Lobbia,    Rackham GSA and GSI
Robert Lobbia completed a pair of B.S. degrees in 2003 from UCLA in Aerospace Engineering and Physics. At UCLA he researched actively controlled combustion in the Combustion Research lab. Beginning in fall 2003, Robbie joined the ranks of PEPL here at the University of Michigan to research actively controlling the plasmas of Hall Effect electric thrusters. His current research projects utilize the Busek BHT-600 4x Hall thruster cluster to focus on the high speed (<1 MHz) transients characteristic to the firing of Hall thrusters.
Michael McDonald,    Aero. Dept. Fellow & Τβπ Fellow

Bailo Bah Ngom,    Rackham Fellow
Bailo Bah Ngom is a Senegalese citizen that has been residing in the US since 1997. Bailo spent his undergraduate years at the Broward Community College (Florida) and at the Georgia Institute of Technology. Currently, he is working towards a PhD degree at the University of Michigan's Plasma dynamics and Electric Propulsion Laboratory (PEPL). Bailo’s research primarily involves studying the interaction between Hall current and magnetic field topology in Hall thrusters based on a quantum physical analysis of Laser Induced Fluorescence (LIF) spectra of neutral xenon.
Sonca Nguyen,    NSF Fellow
Sonca Nguyen received her B.S. degree in Aeronautics and Astronautics at the University of Washington and her M.S. degree in Aerospace Engineering at the University of Michigan. She was first introduced to electric propulsion research work when she was an undergraduate intern at NASA Glenn Research Center with the Ion Propulsion group. Her current thesis project is an application of plasma physics for hydrogen production. She is experimentally investigating a novel method of hydrogen production by dissociating water molecules in a radio-frequency plasma source.
Rohit Shastry,    NASA GSRP Fellow
Rohit Shastry is a third year graduate student (as of Fall 2007) who received his Bachelor's and Master's degrees in Aerospace Engineering at the University of Michigan in 2005 and 2007, respectively. He is currently working on implementing flush-mounted probes within the ceramic walls of a Hall thruster in an effort to directly measure wall characteristics such as particle fluxes and energies. His research is also closely tied to simulation work in an effort to better understand Hall thruster sheath physics and related lifetime and performance issues.
Laura Spencer,    

Ricky Tang,    NASA GSRP Fellow

Ricky Tang received both his B.S.E. and M.S.E. degree in Aerospace Engineering from the University of Michigan. He is currently studying the gasdynamic mirror (GDM) concept, which has the potential to function as an electrodeless plasma thruster driven by some external energy source such as ECRH, or as a more advanced nuclear-driven propulsion device. Along with analytical and computational investigation of the concept, experiments are set up to study ECRH, as well as to eventually validate some of the physics model that has been developed to study the plasma dynamics inside the GDM.
Graduate Students (Pre-Candidates):
Roland Florenz,    

Raymond Liang,    DOD Fellow

Adam Shabshelowitz,    NSF Fellow

Prior Doctoral Graduate Students: sorted by year
John Foster,    Graduated University of Michigan in 1996, Ph.D.

Lyon King,    Graduated University of Michigan in 1998, Ph.D.

thesis: Transport-Property and Mass Spectral Measurements in the Plasma Exhaust Plume of a Hall-Effect Space Propulsion System
status: Assistant Professor of Mechanical Engineering, Michigan Technical University, conducting electric propulsion research at his Ion Space Propulsion (ISP) laboratory.
email: lbking@mtu.edu
Colleen Marrese,    Graduated University of Michigan in 1999, Ph.D.

Sang-Wook Kim,    Graduated University of Michigan in 1999, Ph.D.

thesis: Experimental Investigations of Plasma Parameters and Species-Dependent Ion Energy Distribution in the Plasma Exhaust Plume of a Hall Thruster
status: Applications Engineer, Energy Applications and Systems Engineering, GE Energy (Japan/Korea)
email: Sang-Wook.Kim@ge.com
Frank S. Gulczinski III,    Graduated University of Michigan in 1999, Ph.D.

thesis: Examination of the Structure and Evolution of Ion Energy Properties of a 5 kW Class Laboratory Hall Effect Thruster at Various Operational Conditions
status: Research Scientist in electric propulsion, Air Force Research Laboratory (Edwards AFB)
J. L. Van Noord,    Graduated University of Michigan in 1999, Ph.D.

thesis: Thermal Model of an Ion Thruster
status: Research Scientist in electric propulsion, NASA Glenn Research Center.
email: Jonathan.L.VanNoord@nasa.gov
M. T. Domonkos,    Graduated University of Michigan in 1999, Ph.D.

thesis: Evaluation of Low-Current Orificed Hollow Cathodes
status: Research Scientist in directed energy, Air Force Research Laboratory (Kirtland AFB)
G. J. Williams Jr.,    Graduated University of Michigan in 2000, Ph.D.

thesis: The Use of Laser-Induced Fluorescence to Characterize Discharge Cathode Erosion in a 30 cm Ring-Cusp Ion Thruster
status: Now Research Scientist in electric propulsion, NASA Glenn Research Center
James M. Haas,    Graduated University of Michigan in 2001, Ph.D.

thesis: Low-Perturbation Interrogation of the Internal and Near-field Plasma Structure of a Hall Thruster using a High-Speed Probe Positioning System
status: Now Research Scientist in electric propulsion, Air Force Research Laboratory (Edwards AFB)
email: james.haas@edwards.af.mil
Tim Smith,    Graduated University of Michigan in 2002, Ph.D.

Brian E. Beal,    Graduated University of Michigan in 2004, Ph.D.

thesis: Clustering of Hall Effect Thruster for High-Power Electric Propulsion
status: Now Research Scientist in electric propulsion, Air Force Research Laboratory (Edwards AFB).
email: Brian.Beal@edwards.af.mil
Richard R. Hofer,    Graduated University of Michigan in 2004, Ph.D.

thesis: Development and Characterization of High-Efficiency, High Specific Impulse Xenon Hall Thrusters
status: Now Research Scientist in electric propulsion, NASA Jet Propulsion Laboratory
website:http://richard.hofer.com/
email: Richard.R.Hofer@jpl.nasa.gov
P. Y. Peterson,    Graduated University of Michigan in 2004, Ph.D.

thesis: The Development and Characterization of a Two-Stage Hybrid Hall/Ion Thruster
status: Now Director of Research at ElectroDynamic Applications, Inc.
email: peterson@edapplications.com
Mitchell L. R. Walker,    Graduated University of Michigan in 2005, Ph.D.

website:http://www.ae.gatech.edu/people/mwalker/
thesis: Effects of Facility Backpressure on the Performance and Plume of a Hall Thruster
status: Now Assistant Professor of Aerospace Engineering, Georgia Institute of Technology, conducting electric propulsion research in his laboratory HPEPL
email: mitchell.walker@ae.gatech.edu
Daniel A. Herman,    Graduated University of Michigan in 2005, Ph.D.

Joshua L. Rovey,    Graduated University of Michigan in 2005, Ph.D.

website:http://mae.mst.edu/facultyandstaff/facultyrovey_1_08.html
thesis: A Multiple-Cathode, High-Power, Rectangular Ion Thruster Discharge Chamber for Increasing Thruster Lifetime
status: Now Assistant Professor in the Mechanical and Aerospace Engineering Department at the Missouri University of Science & Technology
email: roveyj@mst.edu
Allen L. Victor,    Graduated University of Michigan in 2006, Ph.D.

thesis: Design and Utilization of a Top Hat Analyzer for Hall Thruster Plume Diagnostics
status: Now Member of the Technical Staff, Aerospace Corporation, Los Angeles
email: allen.victor@aero.org
Jesse A. Linnell,    Graduated University of Michigan in 2007, Ph.D.

thesis: An Evaluation of Krypton Propellant in Hall Thrusters
status: Now Member of the Technical Staff, MIT Lincoln Laboratory
email: jesse.linnell@gmail.com
Prashant Patel,    Graduated University of Michigan in 2008, Ph.D.

David Kirtley,    Graduated University of Michigan in 2008, Ph.D.

thesis: Study of the Synchronous Operation of an Annular Field Reversed Configuration Plasma Device
status: Now Propulsion Research Scientist at MSNW, LLC. email: dkirtley@msnwllc.com
Bryan Reid,    Graduated University of Michigan in 2008, Ph.D.

thesis: The Influence of Neutral Flow Rate in the Operation of Hall Thrusters
status: Now Member of the Technical Staff, MIT Lincoln Laboratory
email: bmreid@gmail.com
Kristina Lemmer,    Graduated University of Michigan in 2009, Ph.D.

thesis: Use of a Helicon Source for Development of a Re-Entry Blackout Amelioration System
status: Starting in Fall 2009, Assistant Professor at Central Michigan University
email: klemmer@umich.edu
Daniel L Brown,    Graduated University of Michigan in 2009, Ph.D.

thesis: Investigation of Low Discharge Voltage Hall Thruster Characteristics and Evaluation of Loss Mechanisms
status: Now Research Scientist in electric propulsion, Air Force Research Laboratory (Edwards AFB)
email: Daniel.Brown.ctr@edwards.af.mil
 

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