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dc.contributor.advisorDavid W. Miller and Alvar Saenz-Otero.en_US
dc.contributor.authorHilton, Andrew Roberten_US
dc.contributor.otherMassachusetts Institute of Technology. Department of Aeronautics and Astronautics.en_US
dc.date.accessioned2015-09-17T17:42:32Z
dc.date.available2015-09-17T17:42:32Z
dc.date.copyright2015en_US
dc.date.issued2015en_US
dc.identifier.urihttp://hdl.handle.net/1721.1/98559
dc.descriptionThesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 2015.en_US
dc.descriptionThis electronic version was submitted by the student author. The certified thesis is available in the Institute Archives and Special Collections.en_US
dc.descriptionCataloged from student-submitted PDF version of thesis.en_US
dc.descriptionIncludes bibliographical references (pages 117-120).en_US
dc.description.abstractSpace systems are inherently difficult to verify prior to launch due to the challenges of replicating the space environment through ground testing. The SPHERES testbed on the International Space Station has provided a risk-tolerant test facility for evaluating enabling technology. The operational execution of the SPHERES facility has resulted in the development of best practices for working with experiments in the operational space environment that can be continually refined through successive generations of SPHERES projects. This thesis presents an experiment framework for developing space technology using the International Space Station that focuses on incrementally building toward technology demonstration through the achievement of specific results at each step that are designed to enable an effective demonstration. The operational nature of the ISS constrains both the time available for testing and the control that the scientist can exercise over the experiment. Therefore, this framework addresses the need to design experiment campaigns that can eciently achieve the desired results using data gathered from tests that exhibit unexpected behavior in addition to the tests that exhibit expected behavior. The framework is inspired by the lessons learned from the RINGS project, an attachment to the SPHERES facility that tests Electromagnetic Formation Flight using electromagnetic coils attached to the vehicle. The RINGS experiment campaign is reviewed with a focus on the lessons learned from the operational phase of the project. From these lessons, the experiment framework is developed and presented so that researchers can have a guide in the planning and designing of their experiments for use on remote, operational facilities. The framework is then applied to the next-generation SPHERES project, the Universal Docking Port, as well as the RINGS project, in order provide examples of how this framework can be implemented.en_US
dc.description.statementofresponsibilityby Andrew Robert Hilton.en_US
dc.format.extent120 pagesen_US
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/1721.1/7582en_US
dc.subjectAeronautics and Astronautics.en_US
dc.titleA performance-driven experiment framework for space technology development using the International Space Stationen_US
dc.typeThesisen_US
dc.description.degreeS.M.en_US
dc.contributor.departmentMassachusetts Institute of Technology. Department of Aeronautics and Astronautics
dc.identifier.oclc920686010en_US


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