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        <datestamp>2023-06-21T01:04:04Z</datestamp>
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        <setSpec>1896:1898:1899:1991</setSpec>
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          <dc:title xml:lang="en">Pump Assisted Heat Pipe</dc:title>
          <jpcoar:creator>
            <jpcoar:creatorName xml:lang="en">MIYAZAKI, Yoshiro</jpcoar:creatorName>
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          <jpcoar:creator>
            <jpcoar:creatorName xml:lang="en">OSHIMA, Shigeto</jpcoar:creatorName>
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          <datacite:description descriptionType="Other">A labortory model of a pump assisted heat pipe has been fablicated and tested. An arterial heat pipe with axial grooves and a gear pump with a magnetic coupling have been developed for the model. The test has been carried out successfully. The reasonable thermal conductance has been obtained so far as the necessary working fluid flow rate is supplied. The necessary flow rate exceeds the theoretical one and the excess flow rate increases as the heat load increases.</datacite:description>
          <datacite:description descriptionType="Other">資料番号: SA0033572000</datacite:description>
          <dc:publisher>宇宙科学研究所</dc:publisher>
          <dc:publisher>Institute of Space and Astronautical Science</dc:publisher>
          <datacite:date dateType="Issued">1987-03</datacite:date>
          <dc:language>eng</dc:language>
          <dc:type rdf:resource="http://purl.org/coar/resource_type/c_6501">departmental bulletin paper</dc:type>
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          <jpcoar:sourceIdentifier identifierType="ISSN">0288-433X</jpcoar:sourceIdentifier>
          <jpcoar:sourceIdentifier identifierType="NCID">AA10455137</jpcoar:sourceIdentifier>
          <jpcoar:sourceTitle xml:lang="en">The Institute of Space and Astronautical Science report. S.P. : The Proceedings of the Symposium on Mechanics for Space Flight 1986</jpcoar:sourceTitle>
          <jpcoar:volume>5</jpcoar:volume>
          <jpcoar:pageStart>149</jpcoar:pageStart>
          <jpcoar:pageEnd>154</jpcoar:pageEnd>
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