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dc.contributor.advisorWalter Wrigley.en_US
dc.contributor.authorPrussing, John Een_US
dc.date.accessioned2005-08-10T23:40:11Z
dc.date.available2005-08-10T23:40:11Z
dc.date.issued1967en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/13807
dc.descriptionMassachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1967. Sc.D.en_US
dc.descriptionMICROFICHE COPY ALSO AVAILABLE IN AERONAUTICS LIBRARY.en_US
dc.descriptionVita.en_US
dc.descriptionBibliography: p. 120-122.en_US
dc.format.extent[11], 123 p.en_US
dc.format.extent7891484 bytes
dc.format.extent7891241 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.titleOptimal multiple-impulse orbital rendezvous.en_US
dc.typeThesisen_US
dc.description.degreeSc.D.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc24528115en_US


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