氦-氙混合冷却空间核反应堆的初步设计考虑

Tao Meng, Sichao Tan, Yuhao He, D. Yuan, Kun Cheng
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引用次数: 1

摘要

自上世纪60年代以来,空间核反应堆得到了广泛的研究。然而,随着《不扩散核武器条约》的签署和冷战的结束,空间核技术逐渐淡出了公众和研究人员的视野。近年来,由于美国“月球和火星工程”和中国“深空科学工程”的提出,空间核技术迎来了新的研究和发展机遇。本文对“普罗米修斯”项目设计进行了分析,并以此为基础进行了多千瓦He-Xe冷却空间核系统的初步设计。给出了系统效率、压缩比、温度等参数,并进行了中子计算,以评价其物理性能,为今后的优化提供指导。并编写了计算热管散热器性能的计算机程序。最后,总结了大功率空间堆设计的一些考虑准则。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Preliminary Design Considerations of He-Xe Mixture Cooled Space Nuclear Reactor
The space nuclear reactor has been widely studied since 60s in the last century. However, upon the signing of the Treaty on the Non-Proliferation of Nuclear Weapons (NPT) and the ending of the Cold War, the space nuclear technology gradually faded out the public and researchers view. In recent years, due to the proposal of the United States’ Moon and Mars Project and China’s Deep Space Scientific Project, space nuclear technology are welcoming new opportunities for research and development. In this paper, the Prometheus project design has been analyzed and thereafter been based for multi-kilowatt He-Xe cooled space nuclear system preliminary design. Parameters like system efficiency, compressor ratio, temperature are given and neutron calculations are conducted in order to evaluate its physical performance and provide guidelines for future optimization. A computer program, which can calculate performance of heat pipe radiator, is also coded and thereafter used. At last, some consideration guidelines are concluded for larger power space reactor design.
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