摘要
以极月轨道上太阳电池阵作为研究对象,详细分析了该轨道上电池阵所得各外热流的确定方法．以此为基础,对太阳电池阵进行在轨温度数值模拟,得到月球轨道上电池阵所得外热流以及温度的周期分布．计算结果与地球卫星的相应数据进行比较,明确了月球轨道上电池阵所得外热流以及温度的周期分布特点,为月球卫星上太阳电池阵以及整个卫星的设计提供了有利的数据参考．
Lunar detection is the beginning of the deep space detection. The energy for the satellite running around the moon is provided by the power system of solar arrays. The lunar orbital environment has the direct effects on the operations of the solar arrays. The characteristics of the surface of the moon and of the lunar orbit have been analyzed. The research object is a rigid solar array in polar lunar orbit. The method to determine the external heat fluxes received by solar array has been shown detailedly on the basis of fully considering the packing factor and the solar cell conversion efficiency. The process of heat transfer in solar array is treated as 3-D anisotropic transient heat conduction problem without internal heat source. Grid division has been made in the solar array and the fully implicit discrete equations have been acquired. The numerical simulation of solar array in polar lunar orbit has been made and the periodic distributions of the external heat fluxes and the temperature of solar array have been obtained. Comparison between the numerical results in earth orbit and that in lunar orbit shows the characteristics of the periodic distribution for thermal parameters of the solar array in lunar orbit, which will provide powerful references for the design of the solar array and the whole lunar satellite.
出处
《空间科学学报》
CAS
CSCD
北大核心
2006年第4期303-308,共6页
Chinese Journal of Space Science
关键词
太阳电池阵
极月轨道
热分析
数值模拟
Solar array, Polar lunar orbit, Thermal analysis, Numerical simulation
