Design and Validation of Closed Two-phase Thermosyphon Loop in Lunar Gravity Environment during China Lunar Project CE-4 | |
Guo, Yuandong1; Wang, Lu2; Miao, Jianyin2; Zhang, He2; Zhang, Youwei2; Zhang, Hongxing2; Chen, Jianxin2; Xu, Yawei2; Wang, Yalong2; Zhao JF(赵建福)3,4 | |
发表期刊 | MICROGRAVITY SCIENCE AND TECHNOLOGY |
2022-05-31 | |
卷号 | 34期号:3页码:38 |
ISSN | 0938-0108 |
摘要 | The structural design, heat transfer capability analysis, ground equivalent validation, and on-orbit flight of the two-phase fluid loop based on flat-plate evaporation module of the Chang'e-4 detector are introduced. Within the temperature range of - 30 degrees C similar to -10 degrees C, the designed two-phase fluid loop has a heat transfer capacity of greater than 200 W. An equivalent test prototype is designed and manufactured to examine the heat transfer performance of the two-phase fluid loop under the ground condition of 1 g. The driving force of the equivalent test prototype is less than that of the flight prototype, while the flow resistance is equivalent to that of the flight prototype. The test heat transfer capacity is smaller than that of the flight prototype on the lunar surface. According to the equivalent test prototype, the heat transfer capacity is no less than 130 W, which meets the requirements of Chang'e-4. During the 14-moon day- night cycle, the temperature of the two-phase fluid loop gradually decreased to an equilibrium value of -10 degrees C. During the wake-up process of the detector in moon day, the control valve was closed, and the temperature of the flat-plate evaporation module rose rapidly, indicating that the function of blocking heat transfer is normal. |
关键词 | Gravity driven Thermosyphon Validation Experiment Operating characteristics |
DOI | 10.1007/s12217-022-09957-0 |
收录类别 | SCI ; EI |
语种 | 英语 |
WOS记录号 | WOS:000803977400002 |
关键词[WOS] | NON-CONDENSABLE GAS ; HEAT-TRANSFER ; PERFORMANCE |
WOS研究方向 | Engineering ; Thermodynamics ; Mechanics |
WOS类目 | Engineering, Aerospace ; Thermodynamics ; Mechanics |
资助项目 | Chinese lunar exploration program |
项目资助者 | Chinese lunar exploration program |
论文分区 | 二类 |
力学所作者排名 | 3+ |
RpAuthor | Wang, Lu |
引用统计 | |
文献类型 | 期刊论文 |
条目标识符 | http://dspace.imech.ac.cn/handle/311007/89556 |
专题 | 微重力重点实验室 |
通讯作者 | Wang, Lu |
作者单位 | 1.Beihang Univ, Sch Aeronaut Sci & Engn, Lab Fundamental Sci Ergon & Environm Control, Beijing 100191, Peoples R China; 2.China Acad Space Technol, Beijing Inst Spacecraft Syst Engn, Beijing Key Lab Space Thermal Control Technol, Beijing 100094, Peoples R China; 3.Chinese Acad Sci, Inst Mech, Natl Micrograv Lab, CAS Key Lab Micrograv, Beijing 100190, Peoples R China; 4.Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China |
推荐引用方式 GB/T 7714 | Guo, Yuandong,Wang, Lu,Miao, Jianyin,et al. Design and Validation of Closed Two-phase Thermosyphon Loop in Lunar Gravity Environment during China Lunar Project CE-4[J]. MICROGRAVITY SCIENCE AND TECHNOLOGY,2022,34,3,:38. |
APA | Guo, Yuandong.,Wang, Lu.,Miao, Jianyin.,Zhang, He.,Zhang, Youwei.,...&Zhao JF.(2022).Design and Validation of Closed Two-phase Thermosyphon Loop in Lunar Gravity Environment during China Lunar Project CE-4.MICROGRAVITY SCIENCE AND TECHNOLOGY,34(3),38. |
MLA | Guo, Yuandong,et al."Design and Validation of Closed Two-phase Thermosyphon Loop in Lunar Gravity Environment during China Lunar Project CE-4".MICROGRAVITY SCIENCE AND TECHNOLOGY 34.3(2022):38. |
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