Instruments design and testing for a Hall thruster plume experiment on the space shuttle

Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2002.

Bibliographic Details
Main Author: Pacros, Anne (Anne Elsa), 1979-
Other Authors: Manuel Martinez-Sanchez.
Format: Thesis
Language:eng
Published: Massachusetts Institute of Technology 2005
Subjects:
Online Access:http://hdl.handle.net/1721.1/16872
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author Pacros, Anne (Anne Elsa), 1979-
author2 Manuel Martinez-Sanchez.
author_facet Manuel Martinez-Sanchez.
Pacros, Anne (Anne Elsa), 1979-
author_sort Pacros, Anne (Anne Elsa), 1979-
collection MIT
description Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2002.
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spelling mit-1721.1/168722019-04-09T18:03:42Z Instruments design and testing for a Hall thruster plume experiment on the space shuttle Pacros, Anne (Anne Elsa), 1979- Manuel Martinez-Sanchez. Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Aeronautics and Astronautics. Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2002. Includes bibliographical references (p. 113-116). This electronic version was submitted by the student author. The certified thesis is available in the Institute Archives and Special Collections. The Electric Thruster Environmental Effects Verification experiment (ETEEV) is designed to obtain in-space measurements in the plume and backflow regions of lowpower thrusters. The ETEEV payload will be installed on a Hitchhiker-palette onboard the Shuttle and will use plasma diagnostics mounted on the palette as well as on an articulated boom. Other objectives include contamination measurements, performance evaluation and optical diagnostics. This work presents first a review of recent papers on the instruments that are available to achieve these mission objectives; then the requirements and status of the ETEEV payload components are explained. Finally, a more precise design of some of the diagnostics is presented, as well as results of ground-based testing at MIT's Space Propulsion Laboratory facility. by Anne Pacros. S.M. 2005-05-19T15:06:31Z 2005-05-19T15:06:31Z 2002 2002 Thesis http://hdl.handle.net/1721.1/16872 51686398 eng 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 144 p. 4190685 bytes 4190432 bytes application/pdf application/pdf application/pdf Massachusetts Institute of Technology
spellingShingle Aeronautics and Astronautics.
Pacros, Anne (Anne Elsa), 1979-
Instruments design and testing for a Hall thruster plume experiment on the space shuttle
title Instruments design and testing for a Hall thruster plume experiment on the space shuttle
title_full Instruments design and testing for a Hall thruster plume experiment on the space shuttle
title_fullStr Instruments design and testing for a Hall thruster plume experiment on the space shuttle
title_full_unstemmed Instruments design and testing for a Hall thruster plume experiment on the space shuttle
title_short Instruments design and testing for a Hall thruster plume experiment on the space shuttle
title_sort instruments design and testing for a hall thruster plume experiment on the space shuttle
topic Aeronautics and Astronautics.
url http://hdl.handle.net/1721.1/16872
work_keys_str_mv AT pacrosanneanneelsa1979 instrumentsdesignandtestingforahallthrusterplumeexperimentonthespaceshuttle