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Experimental Characterization of the Near-Wall Plasma in a 6-kW Hall Thruster and Comparison to Simulation

Shastry, Rohit
Gallimore, Alec D.
Hofer, Richard R.

Publication date

January 2011

DOI

10.2514/6.2011-5589

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Citation count (estimate)

3

Abstract

Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/90711/1/AIAA-2011-5589-977.pd

Extracted data

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Smirnov, Artem
Staack, David
Keidar, Michael
Fisch, Nathaniel J.

January 2005

Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77205/1/AIAA-2005-4404-466.pd

Experimental Characterization of the Near-Wall Region in Hall Thrusters and its Implications on Performance and Lifetime.

Shastry, Rohit

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Hall thruster lifetime codes presently under development at NASA aim to provide predictive tools tha...

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Shastry, Rohit

January 2011

Hall thruster lifetime codes presently under development at NASA aim to provide predictive tools tha...

Interpretation of Wall-mounted Probe Characteristics in Hall Thrusters

Shastry, Rohit
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January 2008

Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76069/1/AIAA-2008-4723-414.pd

Electron-wall interaction in Hall thrusters

Raitses, Yevgeny
Staack, David
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May 2005

Electron-wall interaction effects in Hall thrusters are studied through measurements of the plasma r...

Plasma Potential Measurements in the Discharge Channel of a 6-kW Hall Thruster

Reid, Bryan Michael
Gallimore, Alec D.

January 2008

Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76785/1/AIAA-2008-5185-902.pd

Hall thruster discharge chamber plasma characterization using a high-speed axial reciprocating electrostatic probe

Haas, James M.
Hofer, Richard R.
Gallimore, Alec D.

January 1999

Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76997/1/AIAA-1999-2426-285.pd

Internal plasma potential profiles in a laboratory-model Hall thruster

Haas, James M.
Gallimore, Alec D.

February 2001

The Plasmadynamics and Electric Propulsion Laboratory High-speed Axial Reciprocating Probe system is...

Considerations on the role of the Hall current in a laboratory-model thruster

Haas, James M.
Gallimore, Alec D.

January 2001

Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76645/1/AIAA-2001-3507-148.pd

Analyses of the anode region of a Hall Thruster cahnnel

Keidar, Michael
Boyd, Iain D.
Beilis, Isak I.

January 2002

Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77093/1/AIAA-2002-4107-729.pd

Plasma properties downstream of a low-power Hall thruster

Beal, Brian E.
Gallimore, Alec D.
Hargus, William A.

December 2005

Triple Langmuir probes and emissive probes were used to measure the electron number density, electro...

Internal Plasma Structure Measurements of a Hall Thruster Using Plasma Lens Focusing

Linnell, Jesse A.
Gallimore, Alec D.

January 2005

Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76358/1/AIAA-2005-4402-911.pd

An investigation of internal ion number density and electron temperature profiles in a laboratory-model Hall thruster

Haas, James M.
Gallimore, Alec D.

January 2000

Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76158/1/AIAA-2000-3422-584.pd

Plasma Potential Measurements in the Discharge Channel of a 6-kW Hall Thruster

Bryan M. Reid
Alec D. Gallimore

January 2008

In an effort to understand the role of neutral flow dynamics in the operation of Hall thrusters, a f...