Design Method and Application Research of Deployable Heat Radiator for Spacecraft

被引:0
|
作者
Li, Jin [1 ,2 ]
Zhao, Qiwei [1 ,2 ]
Zheng, Hongyang [1 ,2 ]
Yu, Xingang [1 ,2 ]
Zhang, Yang [1 ,2 ]
机构
[1] Beijing Institute of Spacecraft System Engineering, Beijing,100094, China
[2] National Key Laboratory of Spacecraft Thermal Control, Beijing,100094, China
来源
Yuhang Xuebao/Journal of Astronautics | 2024年 / 45卷 / 10期
关键词
D O I
10.3873/j.issn.1000-1328.2024.10.004
中图分类号
学科分类号
摘要
15
引用
收藏
页码:1552 / 1559
相关论文
共 50 条
  • [41] Design of thick-panel origami-inspired deployable protective shields for spacecraft
    Zhang, Xiaozhao
    Gao, Chengjun
    Chen, Wujun
    Yang, Tianyang
    Yang, Shaochen
    Fang, Guangqiang
    THIN-WALLED STRUCTURES, 2024, 202
  • [42] Research and Design of Hierarchical FDIR in Spacecraft
    Jia, Xiaodong
    Zeng, Chunping
    Cui, Yufu
    SIGNAL AND INFORMATION PROCESSING, NETWORKING AND COMPUTERS (ICSINC), 2019, 550 : 260 - 267
  • [43] RESEARCH ON FLUID HEAT TRANSFER CHARACTERISTICS OF HEAT PIPE RADIATOR DIRECTLY DRIVEN BY HEAT PUMP
    NIU, Jianhui
    LIANG, Zheng
    XU, Shuxue
    Thermal Science, 2024, 28 (05): : 3617 - 3631
  • [44] Research of Flat Heat Pipe Radiator applied in LED Lighting
    Liu Yi-Bing
    MEASUREMENT TECHNOLOGY AND ENGINEERING RESEARCHES IN INDUSTRY, PTS 1-3, 2013, 333-335 : 2039 - 2043
  • [45] Research and application of analysis leads design method
    School of Mechanical Engineering and Automation, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
    Beijing Hangkong Hangtian Daxue Xuebao, 2009, 8 (980-985):
  • [46] The Impact of Tube Optimization Design on Radiator Heat Rejection Performance
    Ismael, Toure
    Sheng, Buyun
    PROCEEDINGS OF THE 2017 INTERNATIONAL CONFERENCE ON APPLIED MATHEMATICS, MODELING AND SIMULATION (AMMS 2017), 2017, 153 : 425 - 429
  • [47] DESIGN AND TEST OF A SELF-CONTROLLED HEAT PIPE RADIATOR
    SWERDLIN.B
    HEMBACH, R
    MECHANICAL ENGINEERING, 1973, 95 (10) : 70 - 70
  • [48] DESIGN AND DEVELOPMENT OF A LIGHTWEIGHT SPACECRAFT HEAT SHIELD
    LOEGERIN.GA
    MECHANICAL ENGINEERING, 1965, 87 (02) : 75 - &
  • [49] Research and development method of software on spacecraft
    Lyu L.
    Guofang Keji Daxue Xuebao/Journal of National University of Defense Technology, 2021, 43 (02): : 61 - 65
  • [50] Mean method for estimating heat transfer efficiency of space radiator
    Zhang, Ning-Li
    Jiang, Jun
    2008, Harbin Institute of Technology (40):