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dc.contributor.authorSnyder, Virgil Warden_US
dc.creatorSnyder, Virgil Warden_US
dc.date.accessioned2013-04-25T10:35:11Z
dc.date.available2013-04-25T10:35:11Z
dc.date.issued1968en_US
dc.identifier.urihttp://hdl.handle.net/10150/284952
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.subjectRockets (Aeronautics)en_US
dc.subjectAerodynamic measurements.en_US
dc.subjectMass (Physics)en_US
dc.subjectwnne Aerobee rocketsen_US
dc.titleA THEORETICAL STUDY OF THE DYNAMICS OF A VARIABLE MASS SYSTEM (APPLIED TOAEROBEE ROCKET)en_US
dc.typetexten_US
dc.typeDissertation-Reproduction (electronic)en_US
dc.identifier.oclc29626336en_US
thesis.degree.grantorUniversity of Arizonaen_US
thesis.degree.leveldoctoralen_US
dc.identifier.proquest6808310en_US
thesis.degree.disciplineGraduate Collegeen_US
thesis.degree.disciplineAerospace and Mechanical Engineeringen_US
thesis.degree.namePh.D.en_US
dc.identifier.bibrecord.b31234380en_US
refterms.dateFOA2018-08-28T19:27:35Z


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