THERMAL CONTROL STRUCTURE OF GEOSTATIONARY SATELLITE
PURPOSE: A thermal control structure of a geostationary satellite is provided to reduce the overheating/overcooling of satellite panels by thermally connecting southern and northern panels. CONSTITUTION: A thermal control structure of a geostationary satellite comprises a northern panel(100), a sout...
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| creator | YANG, KOON HO JUN, HYOUNG YOLL KIM, JUNG HOON YU, MYOUNG JONG |
| description | PURPOSE: A thermal control structure of a geostationary satellite is provided to reduce the overheating/overcooling of satellite panels by thermally connecting southern and northern panels. CONSTITUTION: A thermal control structure of a geostationary satellite comprises a northern panel(100), a southern panel(300), and connection heat pipes(400) which connect the northern and southern panels. The northern/southern panel includes an aluminum plate(160) in which heat pipes(110) are installed and a honeycomb layer in which heat pipes are installed. The connection heat pipes connect the aluminum plates or heat pipes of the northern/southern panels. |
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CONSTITUTION: A thermal control structure of a geostationary satellite comprises a northern panel(100), a southern panel(300), and connection heat pipes(400) which connect the northern and southern panels. The northern/southern panel includes an aluminum plate(160) in which heat pipes(110) are installed and a honeycomb layer in which heat pipes are installed. 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The connection heat pipes connect the aluminum plates or heat pipes of the northern/southern panels.</description><subject>AIRCRAFT</subject><subject>AVIATION</subject><subject>BLASTING</subject><subject>COSMONAUTICS</subject><subject>HEAT EXCHANGE IN GENERAL</subject><subject>HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS,IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT</subject><subject>HEATING</subject><subject>LIGHTING</subject><subject>MECHANICAL ENGINEERING</subject><subject>PERFORMING OPERATIONS</subject><subject>TRANSPORTING</subject><subject>VEHICLES OR EQUIPMENT THEREFOR</subject><subject>WEAPONS</subject><fulltext>true</fulltext><rsrctype>patent</rsrctype><creationdate>2011</creationdate><recordtype>patent</recordtype><sourceid>EVB</sourceid><recordid>eNrjZDAJ8XAN8nX0UXD29wsJ8vdRCA4JCnUOCQ1yVfB3U3B39Q8OcQzx9PdzDIpUCHYMcfXx8Qxx5WFgTUvMKU7lhdLcDMpuriHOHrqpBfnxqcUFicmpeakl8d5BRgaGhgYGhiYWpmaOxsSpAgCbwSiz</recordid><startdate>20110214</startdate><enddate>20110214</enddate><creator>YANG, KOON HO</creator><creator>JUN, HYOUNG YOLL</creator><creator>KIM, JUNG HOON</creator><creator>YU, MYOUNG JONG</creator><scope>EVB</scope></search><sort><creationdate>20110214</creationdate><title>THERMAL CONTROL STRUCTURE OF GEOSTATIONARY SATELLITE</title><author>YANG, KOON HO ; JUN, HYOUNG YOLL ; KIM, JUNG HOON ; YU, MYOUNG JONG</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-epo_espacenet_KR20110014856A3</frbrgroupid><rsrctype>patents</rsrctype><prefilter>patents</prefilter><language>eng ; kor</language><creationdate>2011</creationdate><topic>AIRCRAFT</topic><topic>AVIATION</topic><topic>BLASTING</topic><topic>COSMONAUTICS</topic><topic>HEAT EXCHANGE IN GENERAL</topic><topic>HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS,IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT</topic><topic>HEATING</topic><topic>LIGHTING</topic><topic>MECHANICAL ENGINEERING</topic><topic>PERFORMING OPERATIONS</topic><topic>TRANSPORTING</topic><topic>VEHICLES OR EQUIPMENT THEREFOR</topic><topic>WEAPONS</topic><toplevel>online_resources</toplevel><creatorcontrib>YANG, KOON HO</creatorcontrib><creatorcontrib>JUN, HYOUNG YOLL</creatorcontrib><creatorcontrib>KIM, JUNG HOON</creatorcontrib><creatorcontrib>YU, MYOUNG JONG</creatorcontrib><collection>esp@cenet</collection></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext_linktorsrc</fulltext></delivery><addata><au>YANG, KOON HO</au><au>JUN, HYOUNG YOLL</au><au>KIM, JUNG HOON</au><au>YU, MYOUNG JONG</au><format>patent</format><genre>patent</genre><ristype>GEN</ristype><title>THERMAL CONTROL STRUCTURE OF GEOSTATIONARY SATELLITE</title><date>2011-02-14</date><risdate>2011</risdate><abstract>PURPOSE: A thermal control structure of a geostationary satellite is provided to reduce the overheating/overcooling of satellite panels by thermally connecting southern and northern panels. CONSTITUTION: A thermal control structure of a geostationary satellite comprises a northern panel(100), a southern panel(300), and connection heat pipes(400) which connect the northern and southern panels. The northern/southern panel includes an aluminum plate(160) in which heat pipes(110) are installed and a honeycomb layer in which heat pipes are installed. The connection heat pipes connect the aluminum plates or heat pipes of the northern/southern panels.</abstract><oa>free_for_read</oa></addata></record> |
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| language | eng ; kor |
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| subjects | AIRCRAFT AVIATION BLASTING COSMONAUTICS HEAT EXCHANGE IN GENERAL HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS,IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT HEATING LIGHTING MECHANICAL ENGINEERING PERFORMING OPERATIONS TRANSPORTING VEHICLES OR EQUIPMENT THEREFOR WEAPONS |
| title | THERMAL CONTROL STRUCTURE OF GEOSTATIONARY SATELLITE |
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