Capillary Pumped Loops for Aerospace Application

The Capillary Pumped Loop (CPL) is a two phase aerospace thermal transport system with many advantageous performance characteristics. While retaining the passive nature of the heat pipe, it has demonstrated an order of magnitude greater thermal transport capacity over high performance arterial heat...

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Veröffentlicht in:	SAE transactions 1989-01, Vol.98, p.1701-1706
1. Verfasser:	Gottschlich, Joseph M.
Format:	Artikel
Sprache:	eng
Schlagworte:	Evaporators Fluids Heat Heat pipes Liquids Pressure reduction Pumping Pumps Spacecraft Vapors
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description	The Capillary Pumped Loop (CPL) is a two phase aerospace thermal transport system with many advantageous performance characteristics. While retaining the passive nature of the heat pipe, it has demonstrated an order of magnitude greater thermal transport capacity over high performance arterial heat pipes. In this survey paper, the CPL is described and its brief history discussed. A postulated analytical design model based on thermodynamic principles is presented. Both demonstrated and potential performance advantages are given. Finally, opportunities for future research are suggested.
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Finally, opportunities for future research are suggested.</description><subject>Evaporators</subject><subject>Fluids</subject><subject>Heat</subject><subject>Heat pipes</subject><subject>Liquids</subject><subject>Pressure reduction</subject><subject>Pumping</subject><subject>Pumps</subject><subject>Spacecraft</subject><subject>Vapors</subject><issn>0096-736X</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1989</creationdate><recordtype>article</recordtype><sourceid/><recordid>eNpjYeA0MLA00zU3NovgYOAqLs4yMDA2NDU34mQwcE4syMzJSSyqVAgozS1ITVHwyc8vKFZIyy9ScEwtyi8uSExOVXAsKMjJTE4syczP42FgTUvMKU7lhdLcDLJuriHOHrpZxSX5RfEFRZm5QMPiTUxMzA3NzYyNCckDAK9RLlM</recordid><startdate>19890101</startdate><enddate>19890101</enddate><creator>Gottschlich, Joseph M.</creator><general>Society of Automotive Engineers, Inc</general><scope/></search><sort><creationdate>19890101</creationdate><title>Capillary Pumped Loops for Aerospace Application</title><author>Gottschlich, Joseph M.</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-jstor_primary_444717633</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1989</creationdate><topic>Evaporators</topic><topic>Fluids</topic><topic>Heat</topic><topic>Heat pipes</topic><topic>Liquids</topic><topic>Pressure reduction</topic><topic>Pumping</topic><topic>Pumps</topic><topic>Spacecraft</topic><topic>Vapors</topic><toplevel>online_resources</toplevel><creatorcontrib>Gottschlich, Joseph M.</creatorcontrib><jtitle>SAE transactions</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Gottschlich, Joseph M.</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Capillary Pumped Loops for Aerospace Application</atitle><jtitle>SAE transactions</jtitle><date>1989-01-01</date><risdate>1989</risdate><volume>98</volume><spage>1701</spage><epage>1706</epage><pages>1701-1706</pages><issn>0096-736X</issn><abstract>The Capillary Pumped Loop (CPL) is a two phase aerospace thermal transport system with many advantageous performance characteristics. While retaining the passive nature of the heat pipe, it has demonstrated an order of magnitude greater thermal transport capacity over high performance arterial heat pipes. In this survey paper, the CPL is described and its brief history discussed. A postulated analytical design model based on thermodynamic principles is presented. Both demonstrated and potential performance advantages are given. Finally, opportunities for future research are suggested.</abstract><pub>Society of Automotive Engineers, Inc</pub></addata></record>
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language	eng
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subjects	Evaporators Fluids Heat Heat pipes Liquids Pressure reduction Pumping Pumps Spacecraft Vapors
title	Capillary Pumped Loops for Aerospace Application
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