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Experimental study of ion thruster operation with oxygen as the propellant

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dc.contributor.advisor Manuel Martinez-Sanchez. en_US
dc.contributor.author Aguilar, Robert Bartoldo en_US
dc.contributor.other Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. en_US
dc.date.accessioned 2012-11-19T19:04:10Z
dc.date.available 2012-11-19T19:04:10Z
dc.date.copyright 1983 en_US
dc.date.issued 1983 en_US
dc.identifier.uri http://hdl.handle.net/1721.1/74748
dc.description Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1983. en_US
dc.description Microfiche copy available in Archives and Barker en_US
dc.description Includes bibliographical references. en_US
dc.description.statementofresponsibility by Robert Bartoldo Aguilar. en_US
dc.format.extent 98 leaves en_US
dc.language.iso eng en_US
dc.publisher Massachusetts Institute of Technology en_US
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. en_US
dc.rights.uri http://dspace.mit.edu/handle/1721.1/7582 en_US
dc.subject Aeronautics and Astronautics. en_US
dc.title Experimental study of ion thruster operation with oxygen as the propellant en_US
dc.type Thesis en_US
dc.description.degree M.S. en_US
dc.contributor.department Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. en_US
dc.identifier.oclc 11117309 en_US


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