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http://dx.doi.org/10.5139/JKSAS.2005.33.11.106

Space Simulation Test and Thermal Verification of HAUSAT-2 STM (Structural-Thermal Model) by Using Surface Heaters  

Lee, Mi-Hyeon (한국항공대학교 대학원)
Kim, Dong-Woon (한국항공대학교 대학원)
Hwang, Ki-Lyong (한국항공대학교 대학원)
Chang, Young-Keun (한국항공대학교 항공우주 및 기계공학부)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.33, no.11, 2005 , pp. 106-114 More about this Journal
Abstract
This study addresses space simulation test results and thermal modelling verification of HAUSAT-2 nanosatellite STM (Structural-Thermal Model). The thermal modelling of the HAUSAT-2 has been modified in accordance with test results. Thermal analysis results were repeatedly compared with test results for modified thermal modelling. It is verified that the analysis results for modified thermal modelling agree well with test results. Some surface heaters were implemented to simulate solar illumination for HAUSAT-2 Thermal Vacuum/Balance Test. A low-cost and effective thermal test methodology, which is applicable to ultra-small satellite system, was proposed and verified by test results in this study.
Keywords
HAUSAT-2; Nanosatellite; Thermal Vacuum Test; Thermal Balance Test; Structural Thermal Model;
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  • Reference
1 David G. Gilmore, 'Satellite Thermal Control Handbook', Aerospace Corp., 1994, PP. 709-756
2 장영근, 이동호, '인공위성 시스템 설계공학', 경문사, 1997, PP. 448-455
3 Gyu-Sun Kim, ' KOMPSAT-2 PDR Data Package - Structure Thermal Model', Korea Aerospace Research Institute, 2001. 6
4 H. Mapson-Menard and C. V. Goodall', EIS MTM/TTM THERMAL BALANCE TEST SPEOFICATICN, PROCEDURES AND PREDICTICNS', The University of Birmingham, 2002. 2. 21
5 MIL-STD-1540B, 'Test requirements for space vehicles, United State Air Force, 1992. 10
6 최석원, 최준민, '다목적실용위성 비행모델 열진공시험 Modeling 및 Correlation' , 한국항공 우주학회 추계학술발표회, 항공우주연구원, 2000, 4