Experimental study of ion thruster operation with oxygen as the propellant

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