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Development of loop heat pipe deployable radiator for use on Engineering Test Satellite VIII (ETS-VIII)

机译:用于工程试验卫星VIII的环路热管可展开散热器的开发(ETS-VIII)

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This paper presents a design of deployable radiator and engineering model test for ETS-VIII (Engineering Test Satellite VIII). ETS-VIII will be launched in 2003, which establishes and verifies an advanced 3-ton-class spacecraft bus and an advanced communication technology via satellite. Developed deployable radiator uses LHP (Loop Heat Pipe) whose reservoir is embedded in an evaporator (RELHP) and wick is 0.5 micron fine pore radius stainless steel. Further, CFRP (Carbon Fiber Reinforced Plastic) face-skin with high thermal conductive graphite fiber is used for panel face-skin to reduce panel thickness as well as the panel weight. Thin panel is necessary to reduce stowed panel space. RELHP (Reservoir Embedded Loop Heat Pipe) condenser, aluminum alloy channel, is embedded in the CFRP face-skin radiator panel. Further, engineering model test of the developed deployable radiator has already finished. Deployment, thermal performance, vibration, acoustic and thermal vacuum/balance test, has been carried out successfully. Furthermore, analytical results were compared with thermal balance test. Analytical results have good agreement with tested results.
机译:本文介绍了ETS-VIII(工程试验卫星VIII)的可部署散热器和工程模型试验的设计。 ETS-VIII将于2003年推出,该总线建立和验证先进的3吨级航天器总线和先进的通信技术。开发的可展开散热器使用其储存器嵌入蒸发器(RELHP)和芯片中的LHP(环路热管),芯片为0.5微米细孔径半径不锈钢。此外,具有高导热石墨纤维的CFRP(碳纤维增强塑料)面部皮肤用于面板面部皮肤,以减小面板厚度以及面板重量。薄面板是必要的,以减少被收起的面板空间。 RELHP(储液嵌入式环热管)冷凝器,铝合金通道,嵌入CFRP面部皮肤散热器面板中。此外,开发的可展开散热器的工程模型测试已经完成。部署,热性能,振动,声学和热真空/平衡测试已成功进行。此外,将分析结果与热平衡测试进行了比较。分析结果与测试结果有良好的一致性。

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