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Developing a space shuttle experiment for Hall and pulsed plasma thrusters

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Author(s)
Thomas, Stephanie (Stephanie Jeanne), 1977-
Advisor(s)
Manuel Martinez-Sanchez.
Date Issued
2001
Publisher
Massachusetts Institute of Technology
Abstract
Very little data on Hall and Pulsed Plasma Thrusters has been taken in the hard vacuum of space. The Environment Effects Verifatication experiment is designed to take archival-quality data in space in the plume and far-field regions of these thrusters. Student involvement is a key element of the experiment, which is supported by the Massachusetts Space Grant and the Education branch of NASA. Design of the experiment is currently in the preliminary phase. A new facility at MIT, called the Micro Propulsion Lab, is available for testing related to this experiment, and some initial ground tests of a lab model Hall thruster have been completed.
Description
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2001.
Includes bibliographical references (p. 93-96).
Subjects
Aeronautics and Astronautics.
MIT Department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Terms of Use
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.
http://dspace.mit.edu/handle/1721.1/7582
Persistent DSpace Link
http://hdl.handle.net/1721.1/8899
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