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Massachusetts Institute of Technology

Instrument development and plasma measurements on a 200-watt Hall thruster plume

Abstract

dc:description.abstract

Plume diagnostic instruments were developed and the BHT-200 Hall thruster plume was characterized in order to support ongoing computational plume models. The instruments included a Faraday probe to measure current density, a hot emissive probe to measure plasma potential, and a cold Langmuir probe to measure electron temperature and electron density. Plasma measurements consisted of studying facility and thruster effects on the plume. Facility effects included background pressure and sweep radius, while thruster effects included discharge voltage and flow rate. Experimental results showed that current density is more sensitive to background pressure than to thruster effects, plasma potential is a more direct indicator of plasma density than current flux, and electron temperature and electron density vary substantially across the plume following a polytropic relationship. These experimental results were compared to solutions of a self-similar plume model. Data analyses were also performed using a consistency analysis of the experimental data by deducing plasma potential from Faraday and cold emissive probe data and comparing it to the measured plasma potential from the hot emissive probe. Good agreement was achieved between all experimental data and analysis except in charge exchange dominated regions, since the analyses do not take into account collision effects. Thus, the experimental data obtained can be used to validate computational results.

Degree

thesis:*
Department dc:contributor.department
Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.
Grantor dc:publisher
Massachusetts Institute of Technology
Year dc:date.issued
2003

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Azziz, Yassir, 1979-
Advisor dc:contributor.advisor
  • Manuel Martinez-Sanchez.

Subjects

dc:subject × 1

Rights

dc:rights
Statement dc:rights
  • M.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission.
Language dc:language.iso
eng

Identifiers

dc:identifier.*
Handle dc:identifier.uri
http://hdl.handle.net/1721.1/37856
OAI identifier oai:identifier
oai:dspace.mit.edu:1721.1/37856

Chain of custody

source
Harvested from
MIT
Base URL
dspace.mit.edu/oai/request
Last updated
2026-07-22
Source record
OAI-PMH GetRecord
citation

Azziz, Yassir, 1979-. Instrument development and plasma measurements on a 200-watt Hall thruster plume. Massachusetts Institute of Technology, 2003. http://hdl.handle.net/1721.1/37856