淡江大學機構典藏:Item 987654321/77292
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    Please use this identifier to cite or link to this item: https://tkuir.lib.tku.edu.tw/dspace/handle/987654321/77292


    Title: The Design and Analysis of a Thermal Control System for Micro-satellite TUUSAT-1A
    Authors: Lee, Tzung-hang;Hong, Zuu-chang;Li, Yao-tsung;Li, Shih-wei;Dai, Ji-chien
    Contributors: 淡江大學機械與機電工程學系
    Keywords: Thermal control;Coating;Micro-satellite
    Date: 2007-08
    Issue Date: 2012-06-14 11:17:26 (UTC+8)
    Publisher: 台南市：中華民國航空太空學會
    Abstract: This study simulated and analyzed a passive thermal control system for the design of a TUUSAT-1A microsatellite. The passive attitude magnet microsatellite is a 28 cm cube. This study analyzed satellite temperature distribution via both the node grid analysis model and the numerical iteration method to solve the nonlinear energy equation and achieve normal satellite components operation within a safe temperature. We also calculated temperatures with further considerations at various orbital altitudes of 500 Km, 300 Km and 700 Km, with sun-angles between plus and minus 45 degrees and at different spin speeds. The results were compared with various components of operating temperature and within their allowable ranges with an uncertainty margin of 5℃. The results show that without any thermal control system. The temperature of the simulation is about 51℃~62℃. And external coating protects the microsatellite operating temperature is maintained between 5~40℃ at different altitudes, sun angles and spin speeds. The simulated parameters of thermal control design proposed here could be helpful in future tasks.
    Relation: Journal of Aeronautics, Astronautics and Aviation. Series A=航空太空及民航學刊 43(1), pp.67-76
    Appears in Collections:[Graduate Institute & Department of Mechanical and Electro-Mechanical Engineering] Journal Article

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