Modelling and Preliminary Prediction of Thermal Balance Test for COMS
COMS (Communication, Ocean and Meteorological Satellite) is a geostationary satellite and developed by KARI for communication, ocean and meteorological observations. It will be tested under vacuum and very low temperature conditions in order to verify thermal design of COMS. The test will be perform...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
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The Korean Space Science Society
2009-09-01
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| Series: | Journal of Astronomy and Space Sciences |
| Subjects: |
| _version_ | 1827392412267315200 |
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| author | Hyoung Yoll Jun Jung-Hoon Kim Cho Young Han |
| author_facet | Hyoung Yoll Jun Jung-Hoon Kim Cho Young Han |
| author_sort | Hyoung Yoll Jun |
| collection | DOAJ |
| description | COMS (Communication, Ocean and Meteorological Satellite) is a geostationary satellite and developed by KARI for communication, ocean and meteorological observations. It will be tested under vacuum and very low temperature conditions in order to verify thermal design of COMS. The test will be performed by using KARI large thermal vacuum chamber, which was developed by KARI, and the COMS will be the first flight satellite tested in this chamber. The purposes of thermal balance test are to correlate analytical model used for design evaluation and predicting temperatures, and to verify and adjust thermal control concept. KARI has plan to use heating plates to simulate space hot condition especially for radiator panels of satellite such as north and south panels. They will be controlled from 90 K to 273 K by circulating GN2 and LN2 alternatively according to the test phases, while the main shroud of the vacuum chamber will be under constant temperature, 90 K, during all thermal balance test. This paper presents thermal modelling including test chamber, heating plates and the satellite without solar array wing and Ka-band reflectors and discusses temperature prediction during thermal balance test. |
| first_indexed | 2024-03-08T17:32:00Z |
| format | Article |
| id | doaj.art-a819874139d9411b89235eb9b9f3906c |
| institution | Directory Open Access Journal |
| issn | 2093-5587 2093-1409 |
| language | English |
| last_indexed | 2024-03-08T17:32:00Z |
| publishDate | 2009-09-01 |
| publisher | The Korean Space Science Society |
| record_format | Article |
| series | Journal of Astronomy and Space Sciences |
| spelling | doaj.art-a819874139d9411b89235eb9b9f3906c2024-01-02T14:59:18ZengThe Korean Space Science SocietyJournal of Astronomy and Space Sciences2093-55872093-14092009-09-0126340341610.5140/JASS.2009.26.3.403Modelling and Preliminary Prediction of Thermal Balance Test for COMSHyoung Yoll Jun0Jung-Hoon Kim1Cho Young Han2Satellite Thermal & Propulsion System Department, KARI, Daejeon 305-333, KoreaSatellite Thermal & Propulsion System Department, KARI, Daejeon 305-333, KoreaSatellite Thermal & Propulsion System Department, KARI, Daejeon 305-333, KoreaCOMS (Communication, Ocean and Meteorological Satellite) is a geostationary satellite and developed by KARI for communication, ocean and meteorological observations. It will be tested under vacuum and very low temperature conditions in order to verify thermal design of COMS. The test will be performed by using KARI large thermal vacuum chamber, which was developed by KARI, and the COMS will be the first flight satellite tested in this chamber. The purposes of thermal balance test are to correlate analytical model used for design evaluation and predicting temperatures, and to verify and adjust thermal control concept. KARI has plan to use heating plates to simulate space hot condition especially for radiator panels of satellite such as north and south panels. They will be controlled from 90 K to 273 K by circulating GN2 and LN2 alternatively according to the test phases, while the main shroud of the vacuum chamber will be under constant temperature, 90 K, during all thermal balance test. This paper presents thermal modelling including test chamber, heating plates and the satellite without solar array wing and Ka-band reflectors and discusses temperature prediction during thermal balance test.COMSgeostationary orbitthermal controlthermal analysisthermal balance testthermal vacuum chamber |
| spellingShingle | Hyoung Yoll Jun Jung-Hoon Kim Cho Young Han Modelling and Preliminary Prediction of Thermal Balance Test for COMS Journal of Astronomy and Space Sciences COMS geostationary orbit thermal control thermal analysis thermal balance test thermal vacuum chamber |
| title | Modelling and Preliminary Prediction of Thermal Balance Test for COMS |
| title_full | Modelling and Preliminary Prediction of Thermal Balance Test for COMS |
| title_fullStr | Modelling and Preliminary Prediction of Thermal Balance Test for COMS |
| title_full_unstemmed | Modelling and Preliminary Prediction of Thermal Balance Test for COMS |
| title_short | Modelling and Preliminary Prediction of Thermal Balance Test for COMS |
| title_sort | modelling and preliminary prediction of thermal balance test for coms |
| topic | COMS geostationary orbit thermal control thermal analysis thermal balance test thermal vacuum chamber |
| work_keys_str_mv | AT hyoungyolljun modellingandpreliminarypredictionofthermalbalancetestforcoms AT junghoonkim modellingandpreliminarypredictionofthermalbalancetestforcoms AT choyounghan modellingandpreliminarypredictionofthermalbalancetestforcoms |