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dc.contributor.advisorRichard H. Battin.en_US
dc.contributor.authorSpratlin, Kenneth Miltonen_US
dc.contributor.otherMassachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.en_US
dc.date.accessioned2006-02-02T18:38:24Z
dc.date.available2006-02-02T18:38:24Z
dc.date.copyright1987en_US
dc.date.issued1987en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/31006
dc.descriptionThesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1987.en_US
dc.descriptionMICROFICHE COPY AVAILABLE IN ARCHIVES AND AERONAUTICS.en_US
dc.descriptionBibliography: p. 211-213.en_US
dc.description.statementofresponsibilityby Kenneth Milton Spratlin.en_US
dc.format.extent213 p.en_US
dc.format.extent6260090 bytes
dc.format.extent6287312 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 Astronautics.en_US
dc.titleAn adaptive numeric predictor-corrector guidance algorithm for atmospheric entry vehiclesen_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc17349673en_US


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