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. Department of Aeronautics and Astronautics | |
dc.identifier.oclc | 11117309 | en_US |