<?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>2026-09-20T01:56:05Z</responseDate><request verb="GetRecord" identifier="oai:dspace.mit.edu:1721.1/119060" metadataPrefix="dim">https://dspace.mit.edu/server/oai/request</request><GetRecord><record><header><identifier>oai:dspace.mit.edu:1721.1/119060</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">Jeffrey A. Hoffman.</dim:field>
   <dim:field mdschema="dc" element="contributor" qualifier="author" lang="en_US">Bhattaru, Srinivasa Aditya</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">2018-11-15T16:34:53Z</dim:field>
   <dim:field mdschema="dc" element="date" qualifier="available">2018-11-15T16:34:53Z</dim:field>
   <dim:field mdschema="dc" element="date" qualifier="copyright" lang="en_US">2018</dim:field>
   <dim:field mdschema="dc" element="date" qualifier="issued" lang="en_US">2018</dim:field>
   <dim:field mdschema="dc" element="identifier" qualifier="uri">http://hdl.handle.net/1721.1/119060</dim:field>
   <dim:field mdschema="dc" element="identifier" qualifier="oclc" lang="en_US">1057726335</dim:field>
   <dim:field mdschema="dc" element="description" lang="en_US">Thesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 2018.</dim:field>
   <dim:field mdschema="dc" element="description" lang="en_US">Cataloged from PDF version of thesis.</dim:field>
   <dim:field mdschema="dc" element="description" lang="en_US">Includes bibliographical references (pages 75-78).</dim:field>
   <dim:field mdschema="dc" element="description" qualifier="abstract" lang="en_US">The development of any spaceflight instrument involves a systematic, iterative process of design, testing, and validation. This ensures that the system developed will meet the needs of stakeholders while minimizing costs and risks. Here, the needs for a life-detection instrument targeting nucleic acids are identified, the objectives for that instrument are determined, and system engineering analysis is used to demonstrate that a Search for Extra-Terrestrial Genomes instrument would fulfill those objectives and is feasible for a rover mission. Additionally, we show our design and build process for a testbed to rapidly prototype SETG components and subsystems, which has successfully automated nucleic acid extraction, sequencer loading, and parts of library preparation. We also experiment with thermal simulations and conduct a sequencing test at Martian conditions, using a custom built thermal vacuum chamber system. Finally, this thesis explores potential avenues for future development and identifies short term and long term engineering goals that would assist the SETG team in developing an instrument prototype.</dim:field>
   <dim:field mdschema="dc" element="description" qualifier="statementofresponsibility" lang="en_US">by Srinivasa Aditya Bhattaru.</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">78 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">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.</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">Design, testing, and validation of the search for Extra-Terrestrial Genomes instrument</dim:field>
   <dim:field mdschema="dc" element="type" lang="en_US">Thesis</dim:field>
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	&lt;Language>eng&lt;/Language>
   	&lt;Title>Design, testing, and validation of the search for Extra-Terrestrial Genomes instrument&lt;/Title>
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   	&lt;PublicationDate>2018&lt;/PublicationDate>
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        	&lt;DisplayName>Bhattaru, Srinivasa Aditya&lt;/DisplayName>
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    &lt;License>http://dspace.mit.edu/handle/1721.1/7582&lt;/License>
    &lt;Keyword>Aeronautics and Astronautics.&lt;/Keyword&gt;
   	&lt;Abstract>The development of any spaceflight instrument involves a systematic, iterative process of design, testing, and validation. This ensures that the system developed will meet the needs of stakeholders while minimizing costs and risks. Here, the needs for a life-detection instrument targeting nucleic acids are identified, the objectives for that instrument are determined, and system engineering analysis is used to demonstrate that a Search for Extra-Terrestrial Genomes instrument would fulfill those objectives and is feasible for a rover mission. Additionally, we show our design and build process for a testbed to rapidly prototype SETG components and subsystems, which has successfully automated nucleic acid extraction, sequencer loading, and parts of library preparation. We also experiment with thermal simulations and conduct a sequencing test at Martian conditions, using a custom built thermal vacuum chamber system. Finally, this thesis explores potential avenues for future development and identifies short term and long term engineering goals that would assist the SETG team in developing an instrument prototype.&lt;/Abstract>
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