卫星
热的
太阳能电池
环境科学
太阳能
被动式太阳能建筑设计
光伏系统
功率(物理)
气象学
材料科学
遥感
航空航天工程
工程类
光电子学
电气工程
物理
地质学
量子力学
作者
Tianyu Feng,Xueqin Chen,Jinqiu Zhang,Jinsheng Guo
出处
期刊:Aerospace
[Multidisciplinary Digital Publishing Institute]
日期:2023-01-21
卷期号:10 (2): 108-108
被引量:3
标识
DOI:10.3390/aerospace10020108
摘要
Satellite performance and capability have increased dramatically, particularly for micro- and nanosatellites, requiring more power supply and higher thermal conditions. Problems worth considering include how to provide more power with little or no weight increase, and how to reduce satellite thermal control difficulties. A new way to decrease the temperature of the solar panels on a satellite was proposed. Firstly, the model of solar cells is presented, and the relationship between solar irradiation and the electricity generated explained. Based on this, a new method to reduce the temperature of the solar cell is proposed. Details about current generation and temperature rise calculations for various types of solar cells are also provided. Finally, an experiment was conducted on original and proposed solar cells. While the experiment showed some degree of effectiveness, further experiments are needed.
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