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首页> 外文期刊>Acta astronautica >Thermal design, analysis and comparison on three concepts of space solar power satellite
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Thermal design, analysis and comparison on three concepts of space solar power satellite

机译:空间太阳能卫星三个概念的热设计,分析与比较

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摘要

Space solar power satellites (SSPS) have been widely studied as systems for collecting solar energy in space and transmitting it wirelessly to earth. A previously designed planar SSPS concept collects solar power in two huge arrays and then transmits it through one side of the power-conduction joint to the antenna. However, the system's one group of power-conduction joints may induce a single point of failure. As an SSPS concept, the module symmetrical concentrator (MSC) architecture has many advantages. This architecture can help avoid the need for a large, potentially failure-prone conductive rotating joint and limit wiring mass. However, the thermal control system has severely restricted the rapid development of MSC, especially in the sandwich module. Because of the synchronous existence of five suns concentration and solar external heat flux, the sandwich module will have a very high temperature, which will surpass the permissible temperature of the solar cells. Recently, an alternate multi-rotary joints (MR) SSPS concept was designed by the China Academy of Space Technology (CAST). This system has multiple joints to avoid the problem of a single point of failure. Meanwhile, this concept has another advantage for reducing the high power and heat removal in joints. It is well known to us that, because of the huge external flux in SSPS, the thermal management sub-system is an important component that cannot be neglected. Based on the three SSPS concepts, this study investigated the thermal design and analysis of a 1-km, gigawatt-level transmitting antenna in SSPS. This study compares the thermal management sub-systems of power-conduction joints in planar and MR SSPS. Moreover, the study considers three classic thermal control architectures of the MSC's sandwich module: tile, step, and separation. The study also presents an elaborate parameter design, analysis and discussion of step architecture. Finally, the results show the thermal characteristics of each SSPS concept, and the three concepts are compared. The design layouts, analysis results and parameter discussions of the thermal management sub-system proposed in this study can help inform future SSPS thermal designs.
机译:太空太阳能卫星(SSPS)已被广泛研究为收集太空太阳能并将其无线传输到地球的系统。先前设计的平面SSPS概念将太阳能收集成两个巨大的阵列,然后将其通过导电接头的一侧传输到天线。但是,系统的一组导电接头可能会导致单点故障。作为SSPS概念,模块对称集中器(MSC)体系结构具有许多优点。这种架构可以帮助避免需要大的,可能容易发生故障的导电旋转接头,并限制了接线质量。但是,热控制系统严重限制了MSC的快速发展,特别是在三明治模块中。由于五个太阳的聚集和太阳能外部热通量的同时存在,三明治模块将具有非常高的温度,它将超过太阳能电池的允许温度。最近,由中国空间技术研究院(CAST)设计了一种替代的多旋转关节(MR)SSPS概念。该系统具有多个接头,以避免出现单点故障的问题。同时,该概念还有另一个优点,可以减少接头的高功率和散热。众所周知,由于SSPS中巨大的外部流量,热管理子系统是不可忽视的重要组件。基于三个SSPS概念,本研究调查了SSPS中1 km吉瓦级发射天线的热设计和分析。这项研究比较了平面和MR SSPS中功率传导接头的热管理子系统。此外,该研究还考虑了MSC三明治模块的三种经典的热控制架构:平铺,阶梯式和分隔式。该研究还提出了详细的参数设计,步骤体系结构的分析和讨论。最后,结果显示了每个SSPS概念的热特性,并比较了这三个概念。本研究中提出的热管理子系统的设计布局,分析结果和参数讨论可以帮助为将来的SSPS热设计提供信息。

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