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dc.contributor.advisorKerri Cahoy.en_US
dc.contributor.authorHein, Ayesha Georgina (Ayesha Georgina Iwalanai)en_US
dc.contributor.otherMassachusetts Institute of Technology. Department of Aeronautics and Astronautics.en_US
dc.date.accessioned2017-12-05T19:13:59Z
dc.date.available2017-12-05T19:13:59Z
dc.date.copyright2017en_US
dc.date.issued2017en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/112464
dc.descriptionThesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 2017.en_US
dc.descriptionCataloged from PDF version of thesis.en_US
dc.descriptionIncludes bibliographical references (pages 95-103).en_US
dc.description.abstractThis thesis explores the use of CubeSat constellations as "gap fillers" and supplements to traditionally complex, multi-sensored satellites, increasing resiliency of the system at very low cost. In standard satellite acquisitions, satellites can take years and billions of dollars to reach operational status. Should there be delays in schedule or on-orbit failures, gaps in data integral to US operations can be lost. CubeSats present a low cost temporary solution. In this thesis, the weather sensing satellite, JPSS-1, is used as a reference case for a traditional multi-sensored satellite. The sensors from JPSS-1 are paired with state-of-the-art CubeSat sensors of similar functions. These CubeSats are used to make up three different constellation architectures which are examined for the revisit times and coverage they offer. These architectures are based on some of the common methods of launching and implementing a CubeSat constellation, a single mass launch, a series of available launches, and a planned configuration. This analysis shows that in some areas, like radiometry, CubeSat sensors are comparable with operational heritage sensors. In the other cases, like optical imaging and hyperspectral imagers, CubeSats have not yet advanced enough or cannot be advanced much more based on the limitations of their size and power. A practical use of a CubeSat constellation is to supplement and augment a traditional system, increasing the overall redundancy and providing data over larger geographic regions and with lower revisit times for a approximately 4.5% of the cost of a traditional satellite.en_US
dc.description.statementofresponsibilityby Ayesha Georgina Hein.en_US
dc.format.extent104 pagesen_US
dc.language.isoengen_US
dc.publisherMassachusetts Institute of Technologyen_US
dc.rightsMIT theses are protected by copyright. They may be viewed, downloaded, or printed from this source but further reproduction or distribution in any format is prohibited without written permission.en_US
dc.rights.urihttp://dspace.mit.edu/handle/1721.1/7582en_US
dc.subjectAeronautics and Astronautics.en_US
dc.titleA systems analysis of CubeSat constellations with distributed sensorsen_US
dc.typeThesisen_US
dc.description.degreeS.M.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc1011035557en_US


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