A systems analysis of CubeSat constellations with distributed sensors

Thesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 2017. === Cataloged from PDF version of thesis. === Includes bibliographical references (pages 95-103). === This thesis explores the use of CubeSat constellations as "gap fillers" and supplemen...

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Main Author: Hein, Ayesha Georgina (Ayesha Georgina Iwalanai)
Other Authors: Kerri Cahoy.
Format: Others
Language:English
Published: Massachusetts Institute of Technology 2017
Subjects:
Online Access:http://hdl.handle.net/1721.1/112464
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spelling ndltd-MIT-oai-dspace.mit.edu-1721.1-1124642019-05-02T15:47:18Z A systems analysis of CubeSat constellations with distributed sensors Hein, Ayesha Georgina (Ayesha Georgina Iwalanai) Kerri Cahoy. Massachusetts Institute of Technology. Department of Aeronautics and Astronautics. Massachusetts Institute of Technology. Department of Aeronautics and Astronautics. Aeronautics and Astronautics. Thesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 2017. Cataloged from PDF version of thesis. Includes bibliographical references (pages 95-103). This 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. by Ayesha Georgina Hein. S.M. 2017-12-05T19:13:59Z 2017-12-05T19:13:59Z 2017 2017 Thesis http://hdl.handle.net/1721.1/112464 1011035557 eng MIT 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. http://dspace.mit.edu/handle/1721.1/7582 104 pages application/pdf Massachusetts Institute of Technology
collection NDLTD
language English
format Others
sources NDLTD
topic Aeronautics and Astronautics.
spellingShingle Aeronautics and Astronautics.
Hein, Ayesha Georgina (Ayesha Georgina Iwalanai)
A systems analysis of CubeSat constellations with distributed sensors
description Thesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 2017. === Cataloged from PDF version of thesis. === Includes bibliographical references (pages 95-103). === This 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. === by Ayesha Georgina Hein. === S.M.
author2 Kerri Cahoy.
author_facet Kerri Cahoy.
Hein, Ayesha Georgina (Ayesha Georgina Iwalanai)
author Hein, Ayesha Georgina (Ayesha Georgina Iwalanai)
author_sort Hein, Ayesha Georgina (Ayesha Georgina Iwalanai)
title A systems analysis of CubeSat constellations with distributed sensors
title_short A systems analysis of CubeSat constellations with distributed sensors
title_full A systems analysis of CubeSat constellations with distributed sensors
title_fullStr A systems analysis of CubeSat constellations with distributed sensors
title_full_unstemmed A systems analysis of CubeSat constellations with distributed sensors
title_sort systems analysis of cubesat constellations with distributed sensors
publisher Massachusetts Institute of Technology
publishDate 2017
url http://hdl.handle.net/1721.1/112464
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