Research on Sinking Movement of Liquid Propellant in Space Vehicle
Peng-Fei, Guo3; Hai-Ou, Xie3; Zhou, Bing-Hong2; Zheng, Xiao-Ping1
2019
会议日期May 24, 2019 - May 26, 2019
会议地点Shanghai, China
卷号608
期号1
DOI10.1088/1757-899X/608/1/012028
英文摘要Considering the requirement of rocket engine restart on the liquid propellant location, this paper dedicates to the simulation research on sinking movement of liquid propellant in space vehicle. The extrusion, thrust and structural types of liquid propellant management for space vehicle are summarized. The numerical simulation and drop tower test are compared to study how the liquid propellant moves in the gravity environment, and the relationship between the sinking time and flight acceleration for a new-type space vehicle are provided. These results have considerable significance for the liquid propellant management and acceleration design of space vehicle. © 2019 IOP Publishing Ltd. All rights reserved.
会议录IOP Conference Series: Materials Science and Engineering
语种英语
ISSN号1757-8981
内容类型会议论文
源URL[http://ir.nssc.ac.cn/handle/122/7172]  
专题国家空间科学中心_空间技术部
作者单位1.School of Aerospace, Tsinghua University, Beijing; 100084, China
2.National Space Science Center, Beijing; 100190, China;
3.China Academy of Launch Vehicle Technology, Beijing; 100076, China;
推荐引用方式
GB/T 7714
Peng-Fei, Guo,Hai-Ou, Xie,Zhou, Bing-Hong,et al. Research on Sinking Movement of Liquid Propellant in Space Vehicle[C]. 见:. Shanghai, China. May 24, 2019 - May 26, 2019.
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