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

Linnell, Jesse A.
Gallimore, Alec D.

Publication date

January 2005

DOI

10.2514/6.2005-4402

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Language

English

Citation count (estimate)

8

Abstract

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

Extracted data

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Gallimore, Alec D.

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Magnetic field topology has been found to be a central design concern for high-efficiency Hall thrus...

An experimental investigation of the internal magnetic field topography of an operating Hall thruster

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Haas, James M.

October 2002

Magnetic field measurements were made in the discharge channel of the 5 kW-class P5 laboratory-model...

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Haas, James M.
Gallimore, Alec D.

February 2001

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

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Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76851/1/AIAA-2003-4556-551.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

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

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

Internal plasma potential measurements of a Hall thruster using xenon and krypton propellant

Linnell, Jesse A.
Gallimore, Alec D.

September 2006

For krypton to become a realistic option for Hall thruster operation, it is necessary to understand ...

Internal Langmuir Probe Mapping of a Hall Thruster with Xenon and Krypton Propellant

Linnell, Jesse A.
Gallimore, Alec D.

January 2006

Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77012/1/AIAA-2006-4470-572.pd

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

January 2011

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

Development of a high-speed, reciprocating electrostatic probe system for Hall thruster interrogation

Haas, James M.
Gallimore, Alec D.
McFall, Keith
Spanjers, Gregory G.

November 2000

The use of electrostatic probes to measure local plasma parameters inside the discharge chamber of a...

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...

Interpretation of Wall-mounted Probe Characteristics in Hall Thrusters

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

January 2008

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

Performance testing and internal probe measurements of a high specific impulse Hall thruster

Warner, Noah Zachary, 1978-

January 2003

Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2003.Th...

Development and characterization of high -efficiency, high -specific impulse xenon Hall thrusters.

Hofer, Richard Robert

January 2004

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