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dc.contributor.advisorManuel Martinez-Sanchez.en_US
dc.contributor.authorNiewood, Eliahu Haymen_US
dc.date.accessioned2009-10-01T14:57:31Z
dc.date.available2009-10-01T14:57:31Z
dc.date.copyright1993en_US
dc.date.issued1993en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/47320
dc.descriptionThesis (Sc. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1993.en_US
dc.descriptionIncludes bibliographical references (p. 179-186).en_US
dc.description.statementofresponsibilityby Eliahu H. Niewood.en_US
dc.format.extent186 p.en_US
dc.language.isoengen_US
dc.publisherMassachusetts Institute of Technologyen_US
dc.rightsM.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.urihttp://dspace.mit.edu/handle/1721.1/7582en_US
dc.subjectAeronautics and Astronauticsen_US
dc.titleAn explanation for anode voltage drops in an MPD thrusteren_US
dc.typeThesisen_US
dc.description.degreeSc.D.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Dept. of Aeronautics and Astronauticsen_US
dc.identifier.oclc28732751en_US


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