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논문 기본 정보

자료유형
학술저널
저자정보
Mei Huaping (Institute of Nuclear Energy Safety Technology, Hefei Institutes of Physical Science) Yu Dali (Institute of Nuclear Energy Safety Technology, Hefei Institutes of Physical Science) Ma Shengqin (Institute of Nuclear Energy Safety Technology, Hefei Institutes of Physical Science) Zhang Jiansong (Institute of Nuclear Energy Safety Technology, Hefei Institutes of Physical Science) Sun Yongju (Institute of Nuclear Energy Safety Technology, Hefei Institutes of Physical Science) Chen Chao (Institute of Nuclear Energy Safety Technology, Hefei Institutes of Physical Science) He Meisheng (Institute of Nuclear Energy Safety Technology, Hefei Institutes of Physical Science) Wang Haixia (Institute of Nuclear Energy Safety Technology, Hefei Institutes of Physical Science) Li Yang (Institute of Nuclear Energy Safety Technology, Hefei Institutes of Physical Science) Wang Liang (Institute of Nuclear Energy Safety Technology, Hefei Institutes of Physical Science) Li Taosheng (Institute of Nuclear Energy Safety Technology, Hefei Institutes of Physical Science) Yu Jie (Institute of Nuclear Energy Safety Technology, Hefei Institutes of Physical Science)
저널정보
한국원자력학회 Nuclear Engineering and Technology Nuclear Engineering and Technology Vol.56 No.9
발행연도
2024.9
수록면
3,644 - 3,653 (10page)
DOI
10.1016/j.net.2024.04.015

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Enhancing the capabilities of unmanned space exploration, such as satellite monitoring and space science missions, requires efficient and reliable nuclear power systems. A viable solution is found in the 1–10 kWe power level of space nuclear reactor power systems, offering advantages such as a manageable research and development process, and relatively low investment requirements. This paper introduces a conceptual design for a 5 kWe space nuclear reactor power system, outlining its components and characteristics. The study includes a thorough analysis of potential challenges, encompassing heat pipe failure accidents, re-entry scenarios, and weight estimation considerations. The results demonstrate that the proposed space nuclear reactor power system effectively meets the safety requirements. The total mass of the power system is estimated at approximately 1.5 tons, with a specific mass of around 300 kg/kWe. This research contributes valuable insights for the design of space nuclear reactor power systems operating within a similar power range

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