| 低地球轨道航天器不同攻角原子氧通量密度计算模型 |
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| 引用本文： | 郑阔海,李中华,王敬宜,赵琳.低地球轨道航天器不同攻角原子氧通量密度计算模型[J].宇航学报,2010,31(7). |
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| 作者姓名： | 郑阔海 李中华 王敬宜 赵琳 |
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| 作者单位： | 兰州物理研究所,真空低温技术与物理国家级重点实验室,兰州,730000 |
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| 摘 要： | "低地球轨道原子氧与航天器表面材料相互作用,可导致材料因氧化剥蚀而发生性能衰退,是低地球轨道航天器设计者最关心的环境因素.本文扼要地介绍了兰州物理研究所原子氧实验室采用VB语言编制的""航天器原子氧通量密度计算模型"",该模型以地球大气模式为核心,采用麦克斯韦速度分布对航天器不同攻角遭受到的原子氧进行计算,计算过程中考虑了大气风的影响.模型还可跟踪卫星在轨运行,对不同表面遭受的原子氧通量进行实时计算.计算结果与NASA的原子氧计算模型FluxAV相接近,可为卫星设计者在材料选择时提供数据参考."
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| 关 键 词： | 原子氧 计算模型 大气模型 |
Model of Atomic Oxygen Fluence for Different Spacecraft Surface in Low Earth Orbit |
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| ZHENG Kuo-hai,LI Zhong-hua,WANG Jing-yi,ZHAO Lin.Model of Atomic Oxygen Fluence for Different Spacecraft Surface in Low Earth Orbit[J].Journal of Astronautics,2010,31(7). |
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| Authors: | ZHENG Kuo-hai LI Zhong-hua WANG Jing-yi ZHAO Lin |
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| Institution: | ZHENG Kuo-hai,LI Zhong-hua,WANG Jing-yi,ZHAO Lin(National Key Laboratory of Vacuum & Cryogenics Technology,Physics Lanzhou Institute of Physics Raw and Processed Materials Assurance Center (Branch),CAST Lanzhou 730000,China) |
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| Abstract: | Atomic oxygen is the most important environmental element spacecraft designer cared in LEO which can oxidize materials by impaction. This paper presents the atomic oxygen calculation model briefly developed by the Lab. of atomic oxygen effects & protection,Lanzhou Institute of Physics with VB program. The model uses atmosphere model as its calculation core,and can calculate atomic oxygen fluence/flux of different surface with Maxwell velocity distribution,and the influence of the atmosphere wind is also inv... |
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| Keywords: | LEO LDEF FluxAV |
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