期刊文献+

Perspective on liquid metal enabled space science and technology 被引量:5

原文传递
导出
摘要 With the rapid development of deep space exploration and commercial flight, a series of tough scientific and technological challenges were raised, which urgently require ever advanced technologies to tackle with. Recently, liquid metals, as a kind of newly emerging functional material, are attracting various attention and many breakthroughs have been made on earth. Such a scientific trend also suggests promising approaches for solving those extreme challenges in space environment. To fulfill the increasing needs thus involved, this article is dedicated to systematically introducing liquid metal material and its related disciplines into space science and technology. Firstly, existing application of liquid metal cooling for space nuclear power was summarized. Then, some potential space practices were tentatively put forward, such as liquid metal thermal interface medium,liquid metal phase change material, liquid metal convection cooling, metal alloy thermal storage, liquid metal electromagnetic shielding and liquid metal electronic printing. Fundamental as well as practical issues that would differ with earth were interpreted. Finally, potential liquid metal space experiments were proposed to investigate the liquid metal hydrodynamic characteristic, wettability and phase change mechanism in space physical environment. Overall, liquid metal enabled space science and technology investigation will not only help efficiently solve the current and future space technological problems, but also aid to stimulate the advancement of liquid metal space material science.
出处 《Science China(Technological Sciences)》 SCIE EI CAS CSCD 2020年第7期1127-1140,共14页 中国科学(技术科学英文版)
基金 supported by the Key Project of the National Natural Science Foundation of China (Grant No. 91748206) the Frontier Project of the Chinese Academy of Sciences and Dean’s Research Funding。
  • 相关文献

参考文献6

二级参考文献61

  • 1胡中为.新视野号飞船启程探访冥王星和柯伊伯带[J].科学,2006,58(2):6-9. 被引量:1
  • 2Vladimir V M,Natalia S K,Vladimir A A.Joint optimization of the thermal control system and cooled instruments characteristics. SAE Journal . 1994
  • 3Cal C H,Badawi T.A comparison of power/weight/space require- ments for water-recycling processors. SAE Journal . 1994
  • 4Ernst Messerschmid,Reinhold Bertrand.Spacestation: systems and utilization. . 1999
  • 5Herring R L,Collins P K.Aircraft subsystem waste energy recovery and management. SAE Journal . 1990
  • 6Agazzani A,Massardo A.Advanced solar dynamic space power systems, part 1: efficiency and surface optimization. Journal of Solar Energy Engineering Transactions of the ASME . 1995
  • 7Choi M K.An innovation thermal management concept of waste heat utilization in space. IECEC Paper . 1995
  • 8Harrison W E,Binns K E,Anderson S D,et al.High heat sink fuels for improved aircraft thermal management. SAE Journal . 1993
  • 9Ewert M K,Keller J R,Hughes B.Conceptual design of a solar powered heat pump for lunar base thermal control system. SAE Journal . 1996
  • 10Goldman J H,Lovell T,Ewert M K,et al.High temperature lift heat pump refrigerant and thermodynamic cycle selection. SAE Journal . 1994

共引文献35

同被引文献43

引证文献5

二级引证文献11

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部