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dc.contributor.authorForsythe, Conrad Orville, 1936-
dc.creatorForsythe, Conrad Orville, 1936-en_US
dc.date.accessioned2014-06-03T15:10:32Z
dc.date.available2014-06-03T15:10:32Z
dc.date.issued1965en_US
dc.identifier.urihttp://hdl.handle.net/10150/318452
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 -- Orbits.en_US
dc.subjectSpace trajectories.en_US
dc.titleOrbital altitude for maximum lifetime of a satellite capable of sustained thrusten_US
dc.typetexten_US
dc.typeThesis-Reproduction (electronic)en_US
dc.identifier.oclc28555935en_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.b28505487en_US
dc.identifier.callnumberE9791 1965 39en_US
refterms.dateFOA2018-08-31T00:44:06Z


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