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dc.contributor.advisorOlivier L. de Weck and Richard de Neufville.en_US
dc.contributor.authorChaize, Mathieu, 1980-en_US
dc.contributor.otherMassachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.en_US
dc.date.accessioned2005-09-26T19:34:31Z
dc.date.available2005-09-26T19:34:31Z
dc.date.copyright2003en_US
dc.date.issued2003en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/28285
dc.descriptionThesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2003.en_US
dc.descriptionIncludes bibliographical references (p. 171-175).en_US
dc.description.abstractThe "traditional" way of designing constellations of communications satellites is to optimize the design for a specific global capacity. This approach is based on a forecast of the expected number of users and their activity level, both of which are highly uncertain. It can lead to economic failure if the actual demand is smaller than the one predicted. This thesis presents an alternative approach to the design process to reduce the economic risks. It proposes to deploy constellations in a staged manner, starting with a smaller, more affordable capacity that can be increased if necessary. When the capacity is increased, additional satellites have to be launched and the existing constellation needs to be reconfigured on orbit. Technically, it implies that particular design elements are initially embedded in the design to allow the reconfiguration. Such elements are called "real options" and give decision makers the right but not the obligation to increase the capacity of the system after its initial deployment. This approach reframes the design objectives. Instead of determining an optimal design for a specific capacity, paths of architectures are sought in the trade space. A general framework is presented to identify the paths that offer the most flexibility given different demand scenarios. It is then applied to LEO constellations of communications satellites. Improvements in the life cycle costs on the order of 30% can be obtained for different discount rates and volatilities. This value of flexibility has to be compared to the actual price of the real options. A general method is proposed to study this problem and two technical solutions are proposed.en_US
dc.description.statementofresponsibilityby Mathieu Chaize.en_US
dc.format.extent175 p.en_US
dc.format.extent8673974 bytes
dc.format.extent8696219 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 Astronautics.en_US
dc.titleEnhancing the economics of satellite constellations via staged deployment and orbital reconfigurationen_US
dc.typeThesisen_US
dc.description.degreeS.M.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc54075863en_US


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