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OUTGASSING EXPERIMENT ON A SATELLITE COMPONENT USING BAKE-OUT CHAMBER

机译:烘烤腔对卫星元件的外露实验

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摘要

Satellite components can be contaminated in the process of manufacturing, transporting, andrnhandling of the components. Under orbit environment in space which is characterized as a high vacuumrnwith severe solar beam, the contamination material is outgassed and sticks to the other surface ofrnsatellite, such as optics and solar cells. As a result, the satellite is deteriorated in its important functionrnand hence cannot achieve the designed mission. To avoid such unfavorable situations and exert the bestrnperformance of the satellite, degassing process should be performed for components and subsystems ofrnthe satellite under high vacuum condition with hot temperature for a specified period of time. In thisrnpaper, outgassing experiment was carried out for a development model (DM) of solar panel for KorearnMulti-purpose Satellite(KOMPSAT-II) using the bake-out chamber, which consists of vacuum system,rnthermal system, and measurement system. Temperature and pressure of the chamber was maintainedrnaround 120℃ and 10~(-5) torr, respectively. Residual gases including H_2O, N_2, O_2, CO_2, H_2 were detectedrnand outgassing rate of total contaminant was also measured. This paper aims to introduce and review therncontamination control process for a small satellite, especially in the case of KOMPSAT-II application.
机译:卫星组件可能在组件的制造,运输和处理过程中受到污染。在空间轨道环境中,其特征是具有强烈的太阳束的高真空度,污染物被除气并粘附在卫星的另一表面,例如光学和太阳能电池。结果,卫星的重要功能恶化,因此无法完成设计任务。为了避免这种不利情况并发挥卫星的最佳性能,应在高温下在高真空条件下对卫星的组件和子系统进行脱气处理一段指定的时间。本文利用烘烤室对韩国多功能卫星(KOMPSAT-II)太阳能电池板的开发模型(DM)进行了脱气实验,该烘烤室由真空系统,热系统和测量系统组成。腔室的温度和压力分别维持在120℃和10〜(-5)托。检测出H_2O,N_2,O_2,CO_2,H_2等残留气体,并测定了总污染物的除气率。本文旨在介绍和回顾小型卫星的热污染控制过程,尤其是在KOMPSAT-II应用的情况下。

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