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首页> 外文期刊>Journal of Spacecraft Technology >Estimation of the Thermodynamic Equilibrium Temperature of Chandrayaan-2 Rover Solar Panel during Long Lunar Nights
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Estimation of the Thermodynamic Equilibrium Temperature of Chandrayaan-2 Rover Solar Panel during Long Lunar Nights

机译:农历长夜Chandrayaan-2 Rover太阳电池板热力学平衡温度的估算

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摘要

The rover proposed in the mission Chandrayaan-2, to primarily carry out in-situ scientific experiments on Moon surface, is planned to land near lunar South Pole where the number of sunlit days and nights vary with different lunar site latitudes. Extent of lunar night/s can be from 15 earth days (at 60° south latitude landing site) to 20 earth days at 88° south latitude. Thus, rover solar panel will be undergoing a continuous cold lunar night spanning 20 earth days unlike 72 minutes of peak eclipse duration for Geosynchronous Earth Orbit (GEO) spacecrafts. Thus, an analysis is carried out to evaluate the thermodynamic equilibrium temperature of Chandrayaan-2 rover solar panel during these long lunar nights for different landing sites and results are presented.
机译:计划在Chandrayaan-2任务中提出的漫游车,主要是在月球表面进行原位科学实验,计划将其降落在南极月球附近,那里的日夜昼夜数随月球纬度的不同而不同。农历夜晚的范围可以从15个地球日(在南纬60度着陆点)到20个地球日在南纬88度。因此,与地球同步地球轨道(GEO)宇宙飞船的最高月食持续时间72分钟不同,漫游者太阳能电池板将经历连续20天的连续阴冷夜。因此,进行了分析以评估Chandrayaan-2漫游者太阳能电池板在这些漫长的月夜期间针对不同着陆点的热力学平衡温度,并给出了结果。

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