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dc.contributor.advisorW.E. Vander Velde and T.N. Edelbaum.en_US
dc.contributor.authorBeebee, William Scrippsen_US
dc.date.accessioned2005-08-02T19:33:50Z
dc.date.available2005-08-02T19:33:50Z
dc.date.issued1975en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/16434
dc.descriptionThesis. 1975. Sc.D.--Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.en_US
dc.descriptionVita.en_US
dc.descriptionBibliography: leaves 318-319.en_US
dc.format.extent320 leaves(8 fold.)en_US
dc.format.extent19216514 bytes
dc.format.extent19216274 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.subject.lcshGuided missiles Trackingen_US
dc.subject.lcshAntimissile missilesen_US
dc.titleOptimal hypersonic pursuit evasion.en_US
dc.typeThesisen_US
dc.description.degreeSc.D.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Dept. of Aeronautics and Astronauticsen_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc01379997en_US


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