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Thermal Aspects of Satellite Downscaling

机译:卫星缩小的热方面

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The strong trend toward nanosatellites creates new challenges in terms of thermal balance control. The thermalnbalance of a satellite is determined by the heat dissipation in its subsystems and by the thermal connections betweennthem. As satellites become smaller, heat dissipation in their subsystems tends to decrease and thermal connectivitynscales down with dimension. However, these two terms do not necessarily scale in the same way, and so the thermalnbalancemay alter and the temperature of subsystems may reach undesired levels. This paper focuses on low-Earth-norbit satellites. We constructed a generalized lumped thermal model that combines a generalized low-Earth-orbitnsatellite configuration with scaling trends in subsystem heat dissipation and thermal connectivity. Using satellitenmass as a scaling parameter, we show that subsystems do not become thermally critical by scaling mass alone.
机译:纳米卫星的强劲趋势在热平衡控制方面提出了新的挑战。卫星的热平衡是由其子系统中的散热和团之间的热连接决定的。随着卫星变得越来越小,其子系统中的散热趋于减少,并且热连通性随尺寸减小。但是,这两个术语不一定按相同的方式缩放,因此,热平衡可能会发生变化,子系统的温度可能会达到不希望的水平。本文重点关注低地球轨道卫星。我们构建了一个广义的集总热模型,该模型将广义的低地球-轨道-星云构造与子系统散热和热连通性的缩放趋势相结合。使用satellitenmass作为缩放参数,我们表明仅通过缩放质量,子系统就不会成为热关键。

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