<?xml version="1.0" encoding="UTF-8"?><?xml-stylesheet type="text/xsl" href="static/style.xsl"?><OAI-PMH xmlns="http://www.openarchives.org/OAI/2.0/" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xsi:schemaLocation="http://www.openarchives.org/OAI/2.0/ http://www.openarchives.org/OAI/2.0/OAI-PMH.xsd"><responseDate>2026-09-19T22:35:12Z</responseDate><request verb="GetRecord" identifier="oai:dspace.mit.edu:1721.1/90611" metadataPrefix="dim">https://dspace.mit.edu/server/oai/request</request><GetRecord><record><header><identifier>oai:dspace.mit.edu:1721.1/90611</identifier><datestamp>2022-01-13T07:53:53Z</datestamp><setSpec>com_1721.1_7582</setSpec><setSpec>com_1721.1_7581</setSpec><setSpec>col_1721.1_131023</setSpec></header><metadata><dim:dim xmlns:dim="http://www.dspace.org/xmlns/dspace/dim" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xmlns:doc="http://www.lyncode.com/xoai" xsi:schemaLocation="http://www.dspace.org/xmlns/dspace/dim http://www.dspace.org/schema/dim.xsd">
   <dim:field mdschema="dc" element="contributor" qualifier="advisor" lang="en_US">David W. Miller and Alvar Saenz-Otero.</dim:field>
   <dim:field mdschema="dc" element="contributor" qualifier="author" lang="en_US">Sternberg, David Charles, Ph. D. Massachusetts Institute of Technology</dim:field>
   <dim:field mdschema="dc" element="contributor" qualifier="other" lang="en_US">Massachusetts Institute of Technology. Department of Aeronautics and Astronautics.</dim:field>
   <dim:field mdschema="dc" element="contributor" qualifier="department">Massachusetts Institute of Technology. Department of Aeronautics and Astronautics</dim:field>
   <dim:field mdschema="dc" element="date" qualifier="accessioned">2014-10-07T19:18:04Z</dim:field>
   <dim:field mdschema="dc" element="date" qualifier="available">2014-10-07T19:18:04Z</dim:field>
   <dim:field mdschema="dc" element="date" qualifier="copyright" lang="en_US">2014</dim:field>
   <dim:field mdschema="dc" element="date" qualifier="issued" lang="en_US">2014</dim:field>
   <dim:field mdschema="dc" element="identifier" qualifier="uri">http://hdl.handle.net/1721.1/90611</dim:field>
   <dim:field mdschema="dc" element="identifier" qualifier="oclc" lang="en_US">891582650</dim:field>
   <dim:field mdschema="dc" element="description" lang="en_US">Thesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 2014.</dim:field>
   <dim:field mdschema="dc" element="description" lang="en_US">This electronic version was submitted by the student author.  The certified thesis is available in the Institute Archives and Special Collections.</dim:field>
   <dim:field mdschema="dc" element="description" lang="en_US">Cataloged from student-submitted PDF version of thesis.</dim:field>
   <dim:field mdschema="dc" element="description" lang="en_US">Includes bibliographical references (pages 138-142).</dim:field>
   <dim:field mdschema="dc" element="description" qualifier="abstract" lang="en_US">A means for reducing the risk for an on-orbit robotic servicing and assembly mission through the development of a series of testbeds that build successively upon one another is investigated. Robotic Servicing and Assembly (RSA) missions are believed to enable life extension programs for existing spacecraft while also enabling much larger and more complex satellites to be developed through on-orbit construction. Unfortunately, many of the new and innovative technologies required for RSA to be economically and technically feasible are still in their formative development stages. Consequently, such RSA missions are highly risk prone. This thesis investigates the development of an incremental and iterative testing facility which can be used to reduce these RSA risks by conducting demonstration testing in authentic operational environments while leveraging existing infrastructures to reduce the costs associated with testing. The Defense Advanced Research Project Agency's (DARPA) Phoenix project, a satellite repurposing mission, serves as an example of a full-scale flight mission requiring risk-reduction testing. The thesis presents research that shows how the newly developed testing facility, which expands on the Synchronized Position Hold Engage and Reorient Experimental Satellites (SPHERES) facility, can reduce the risk of many technologies required for Phoenix. In particular, testing is discussed and analyzed for the risk reduction of resource aggregation and physical reconfiguration technologies. This testing is both incremental and iterative in nature as part of two ground test programs and a flight program aboard the International Space Station. The testing progression matures these technologies from base principles tested in the ground environment at the MIT Space Systems Laboratory to the planned implementation aboard the International Space Station prior to the final flight mission. The newly developed testing facility is small in scale as compared to the final RSA flight satellites, so newly developed scaling laws are presented. This process relies on the scaling of testbed results using the combined application of hybrid scaling laws and nondimensional parameters. In doing so, the results from the new testing facility can be applied to the Phoenix mission to raise the probability of mission success.</dim:field>
   <dim:field mdschema="dc" element="description" qualifier="statementofresponsibility" lang="en_US">by David Charles Sternberg.</dim:field>
   <dim:field mdschema="dc" element="description" qualifier="degree" lang="en_US">S.M.</dim:field>
   <dim:field mdschema="dc" element="format" qualifier="extent" lang="en_US">142 pages</dim:field>
   <dim:field mdschema="dc" element="language" qualifier="iso" lang="en_US">eng</dim:field>
   <dim:field mdschema="dc" element="publisher" lang="en_US">Massachusetts Institute of Technology</dim:field>
   <dim:field mdschema="dc" element="rights" lang="en_US">M.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.</dim:field>
   <dim:field mdschema="dc" element="rights" qualifier="uri" lang="en_US">http://dspace.mit.edu/handle/1721.1/7582</dim:field>
   <dim:field mdschema="dc" element="subject" lang="en_US">Aeronautics and Astronautics.</dim:field>
   <dim:field mdschema="dc" element="title" lang="en_US">Development of an incremental and iterative risk reduction facility for robotic servicing and assembly missions</dim:field>
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   	&lt;Title>Development of an incremental and iterative risk reduction facility for robotic servicing and assembly missions&lt;/Title>
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   	&lt;PublicationDate>2014&lt;/PublicationDate>
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        	&lt;DisplayName>Sternberg, David Charles, Ph. D. Massachusetts Institute of Technology&lt;/DisplayName>
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    &lt;Keyword>Aeronautics and Astronautics.&lt;/Keyword>
   	&lt;Abstract>A means for reducing the risk for an on-orbit robotic servicing and assembly mission through the development of a series of testbeds that build successively upon one another is investigated. Robotic Servicing and Assembly (RSA) missions are believed to enable life extension programs for existing spacecraft while also enabling much larger and more complex satellites to be developed through on-orbit construction. Unfortunately, many of the new and innovative technologies required for RSA to be economically and technically feasible are still in their formative development stages. Consequently, such RSA missions are highly risk prone. This thesis investigates the development of an incremental and iterative testing facility which can be used to reduce these RSA risks by conducting demonstration testing in authentic operational environments while leveraging existing infrastructures to reduce the costs associated with testing. The Defense Advanced Research Project Agency&amp;apos;s (DARPA) Phoenix project, a satellite repurposing mission, serves as an example of a full-scale flight mission requiring risk-reduction testing. The thesis presents research that shows how the newly developed testing facility, which expands on the Synchronized Position Hold Engage and Reorient Experimental Satellites (SPHERES) facility, can reduce the risk of many technologies required for Phoenix. In particular, testing is discussed and analyzed for the risk reduction of resource aggregation and physical reconfiguration technologies. This testing is both incremental and iterative in nature as part of two ground test programs and a flight program aboard the International Space Station. The testing progression matures these technologies from base principles tested in the ground environment at the MIT Space Systems Laboratory to the planned implementation aboard the International Space Station prior to the final flight mission. The newly developed testing facility is small in scale as compared to the final RSA flight satellites, so newly developed scaling laws are presented. This process relies on the scaling of testbed results using the combined application of hybrid scaling laws and nondimensional parameters. In doing so, the results from the new testing facility can be applied to the Phoenix mission to raise the probability of mission success.&lt;/Abstract>
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