首页> 外文会议>Advances in Electronic Packaging 2005 pt.C >THERMAL MANAGEMENT OF A FAST UV SLITLESS SPECTROMETER FOR A METEOR RESEARCH EXPERIMENT
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THERMAL MANAGEMENT OF A FAST UV SLITLESS SPECTROMETER FOR A METEOR RESEARCH EXPERIMENT

机译:用于流星研究实验的快速紫外无谱仪的热管理

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This paper presents the proposed thermal management design for an ultra-violet slitless spectrometer to be flown on either the Space Shuttle or on the International Space Station as a scientific experiment to capture the ultraviolet spectrum of meteors as they are heated by the Earth's atmosphere. The proposed telescope was initially planned as a Hitchhiker experiment for the Space Shuttle. The Space Station environment is thermally more critical than the Hitchhiker application. The final thermal design is essentially passive; however, heaters will be used to maintain the component temperatures at acceptable levels during telescope non-operating conditions. The major difference between the Space Station design and the Hitchhiker design is the use of external multi-layer insulation and thermal strapping on the former application.
机译:本文介绍了拟议的热管理设计,该技术将用于在航天飞机或国际空间站上飞行的紫外无缝光谱仪,作为一项科学实验来捕获流星被地球大气加热时的紫外线光谱。提议的望远镜最初是作为航天飞机的Hitchhiker实验计划的。空间站环境在热方面比Hitchhiker应用程序更为关键。最终的散热设计本质上是被动的。但是,在望远镜非工作状态下,将使用加热器将组件温度保持在可接受的水平。空间站设计与Hitchhiker设计之间的主要区别在于,在以前的应用程序中使用了外部多层绝缘和热捆扎。

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