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Thermal Modeling and Validation Testing of a Miniature Xenon Ion Thruster

Abstract

dc:description.abstract

<p>To support the research of miniature ion propulsion, Cal Poly's Miniature Xenon</p> <p>Ion (MiXI) thruster has been modeled and tested. Using ANSYS Fluent, a two-</p> <p>dimensional model of the transient thermal environment of MiXI-CP-V3 was</p> <p>created. Validation testing was conducted in order to assess the accuracy of the</p> <p>thermal model. During testing, temperature was measured at eight locations</p> <p>across MiXI. From the test data it was determined that the thermal model did a</p> <p>poor job of predicting temperature due to incident radiation at the four locations</p> <p>nearest the keeper electrode. The four remaining locations were affected mostly</p> <p>by conduction and followed a trend that closely resembled the test data. The</p> <p>difference between the test data and the model's predicted temperature varied</p> <p>depending on time and location; the difference between the predicted data and</p> <p>the test data fell within 10C, for most of the operation but reached 27.1C at</p> <p>one location. The thermal model was used to assess ways to shunt heat transfer</p> <p>to the permanent magnets in order to postpone demagnetization, which occurs at</p> <p>300C. Sheathing the entire keeper electrode with Macor was shown to reduce the</p> <p>temperature by as much as 13.3C at certain times and locations. Due to its lower</p> <p>thermal conductivity, it was hypothesized that a thruster made of titanium would</p> <p>impede heat transfer to the magnets, however, the model showed an increase in</p> <p>temperature rise when properties of certain titanium alloys are applied. Applying</p> <p>a thermally insulative coatings to the anode was considered, but not modeled</p> <p>because the available coatings have a melting point below 350C.</p>

Degree

thesis:*
Name thesis:degree_name
MS in Aerospace Engineering
Discipline thesis:degree_discipline
Aerospace Engineering
Year dc:date.available
2013

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Parker, Samuel R
Contributors dc:contributor
  • Kira Abercromby

Identifiers

dc:identifier.*
OAI identifier oai:identifier
oai:digitalcommons.calpoly.edu:theses-2212

Chain of custody

source
Harvested from
Cal Poly
Base URL
digitalcommons.calpoly.edu/do/oai/
Last updated
2026-07-24
Source record
OAI-PMH GetRecord
related terms
citation

Parker, Samuel R. Thermal Modeling and Validation Testing of a Miniature Xenon Ion Thruster. 2013. https://digitalcommons.calpoly.edu/theses/1115