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Numerical simulation of ion thruster plume backflow for spacecraft contamination assessment

dc.contributor.advisorDaniel F. Hastings.en_US
dc.contributor.authorSamanta Roy, Robie Ien_US
dc.date.accessioned2005-08-17T18:09:35Z
dc.date.available2005-08-17T18:09:35Z
dc.date.copyright1995en_US
dc.date.issued1995en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/11397
dc.descriptionThesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1995.en_US
dc.descriptionIncludes bibliographical references (p. 237-246).en_US
dc.description.statementofresponsibilityby Robie I. Samanta Roy.en_US
dc.format.extent246 p.en_US
dc.format.extent21201463 bytes
dc.format.extent21201221 bytes
dc.format.mimetypeapplication/pdf
dc.format.mimetypeapplication/pdf
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/1721.1/7582
dc.subjectAeronautics and Astronauticsen_US
dc.titleNumerical simulation of ion thruster plume backflow for spacecraft contamination assessmenten_US
dc.typeThesisen_US
dc.description.degreePh.D.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc33226974en_US


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