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Design Study of Nuclear Power Systems for Deep Space Explorers (2) Electricity Supply Capabilities of Solid Cores

机译:深度空间探险勘探器核电系统的设计研究(2)固体核心的电力供应能力

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This study has been carried out in series with the other study, "Criticality of Low Enriched Uranium Fueled Core" to explore the possibilities of a solid reactor electricity generation system for supplying propulsion power of a deep space explorer. The design ranges of two different systems are determined with respect to the electric power, the radiator mass, and the operating temperatures of the heat-pipes and thermoelectric converters. The two systems are the core surface cooling with heat-pipe system (CSHP), and the core direct cooling with heat-pipe system (CDHP). The evaluated electric powers widely cover the 1 to 100 kW range, which had long been claimed to be the range that lacked the power sources in space. Therefore, the concepts shown by this study may lead to a breakthrough of the human activities in space. The working temperature ranges of the main components, namely the heat-pipes and thermoelectric converters, are wide and covers down to relatively low temperatures. This is desirable from the viewpoints of broadening the choices, reducing the development needs, and improving the reliabilities of the devices. Hence, it is advantageous for an early establishment of the concept.
机译:本研究系列中进行了与其他研究中,“低浓铀的推动核心的临界”探索提供了深刻的太空探险的推进力了坚实的反应堆发电系统的可能性。两种不同的系统的设计范围相对于所述电力,散热器质量以及热管和热电转换器的工作温度来确定。这两个系统是核心表面与热管系统(CSHP)冷却,和芯直接与热管系统(CDHP)冷却。所评估的电功率广泛覆盖1至100千瓦范围内,这早就声称是,缺乏在空间中的动力源的范围内。因此,这项研究显示的概念,可能导致空间的人类活动的一个突破。的主要部件的工作温度范围内,即热管和热电转换器,是宽和盖子下降到相对低的温度。这是从扩大的选择,降低了发展的需要,提高了设备​​的可靠性的观点不可取。因此,它是一个早期成立的理念是有利的。

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