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PRELIMINARY DESIGN CONSIDERATIONS OF HE-XE MIXTURE COOLED SPACE NUCLEAR REACTOR

机译:He-Xe混合冷却空间核反应堆的初步设计注意事项

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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.
机译:上世纪60年代以来,对空间核反应堆进行了广泛的研究。然而,随着《不扩散核武器条约》(NPT)的签署以及冷战的结束,太空核技术逐渐淡出了公众和研究人员的视野。近年来,由于美国的“月球与火星计划”和中国的“深空科学计划”的提出,太空核技术正迎来新的研发机会。在本文中,对Prometheus项目设计进行了分析,然后基于其对多千瓦He-Xe冷却空间核系统进行了初步设计。给出了系统效率,压缩机比率,温度等参数,并进行了中子计算,以评估其物理性能并为将来的优化提供指导。还可以对计算机程序进行编码,然后可以使用该计算机程序来计算热管散热器的性能。最后,总结了有关较大功率空间反应堆设计的一些考虑准则。

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