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Optimal escape trajectory from a high earth orbit by use of solar radiation pressure.

dc.contributor.advisorLouis A. D'Amario and Donald C. Fraser.en_US
dc.contributor.authorGreen, Andrew Josephen_US
dc.date.accessioned2005-09-26T17:17:57Z
dc.date.available2005-09-26T17:17:57Z
dc.date.issued1977en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/27896
dc.descriptionThesis. 1977. M.S.--Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.en_US
dc.descriptionMICROFICHE COPY AVAILABLE IN ARCHIVES AND AERO.en_US
dc.descriptionBibliography : leaves 51-53.en_US
dc.format.extentv, 97 leavesen_US
dc.format.extent4288548 bytes
dc.format.extent4300696 bytes
dc.format.mimetypeapplication/pdf
dc.format.mimetypeapplication/pdf
dc.language.isoen_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.lcshBoundary value problemsen_US
dc.subject.lcshSolar sailsen_US
dc.subject.lcshSolar radiationen_US
dc.subject.lcshSpace trajectoriesen_US
dc.titleOptimal escape trajectory from a high earth orbit by use of solar radiation pressure.en_US
dc.typeThesisen_US
dc.description.degreeM.S.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc04600132en_US


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