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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Bibliographische Detailangaben
Hauptverfasser:	YANG, KOON HO, JUN, HYOUNG YOLL, KIM, JUNG HOON, YU, MYOUNG JONG
Format:	Patent
Sprache:	eng ; kor
Schlagworte:	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
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Beschreibung
Zusammenfassung:	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.