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dc.contributor.authorSkelding, Robert Matthew, 1933-
dc.creatorSkelding, Robert Matthew, 1933-en_US
dc.date.accessioned2014-06-04T09:44:29Z
dc.date.available2014-06-04T09:44:29Z
dc.date.issued1962en_US
dc.identifier.urihttp://hdl.handle.net/10150/319448
dc.language.isoen_USen_US
dc.publisherThe University of Arizona.en_US
dc.rightsCopyright © is held by the author. Digital access to this material is made possible by the University Libraries, University of Arizona. Further transmission, reproduction or presentation (such as public display or performance) of protected items is prohibited except with permission of the author.en_US
dc.subjectArtificial satellites -- Control systems.en_US
dc.titleThe dynamic behavior of an artificial satellite stabilized by gravity-gradienten_US
dc.typetexten_US
dc.typeThesis-Reproduction (electronic)en_US
dc.identifier.oclc28250130en_US
thesis.degree.grantorUniversity of Arizonaen_US
thesis.degree.levelmastersen_US
thesis.degree.disciplineGraduate Collegeen_US
thesis.degree.nameM.S.en_US
dc.identifier.bibrecord.b28934325en_US
dc.identifier.callnumberE9791 1962 209en_US
refterms.dateFOA2018-06-24T22:05:08Z


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