[1] |
ZHENG Kai, XIANG Yanchao, RAO Wei, ZHANG Bingqiang, XUE Shuyan, DAI Chenghao, ZHANG Dong, WANG Yuying.
Design and verification of thermal control system for Tianwen-1 Mars entry capsule
[J]. Chinese Space Science and Technology, 2022, 42(5): 108-116.
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[2] |
HAN Ruoyu, HE Baiyan, NIE Rui, FAN Yesen, MA Xiaofei.
Optimization design of mesh antenna considering thermal deformation in service
[J]. Chinese Space Science and Technology, 2022, 42(4): 111-119.
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[3] |
TONG Yelong, TAO Zechao, LI Yifan, LIU Zhanjun, JIANG Lifeng, YIN Yazhou.
Carbon materials with high thermal conductivity and its application in spacecraft
[J]. Chinese Space Science and Technology, 2022, 42(1): 131-138.
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[4] |
NING Xianwen, JIANG Fan, CHEN Yang, ZHANG Dong, WANG Yuying, XUE Shuyan.
Design and implementation of thermal balance test scheme for Chang'e-5 probe
[J]. Chinese Space Science and Technology, 2021, 41(6): 132-137.
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[5] |
ZHANG Bingqiang, XIANG Yanchao, XUE Shuyan, ZHENG Kai, ZHONG Qi, ZHANG Youwei.
Analysis of the influence of Mars surface thermal environment on spacecraft thermal control
[J]. Chinese Space Science and Technology, 2021, 41(2): 55-62.
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[6] |
ZHAO Xingying, LI Qiang.
Optimal design of droplet layer in liquid droplet radiator
[J]. Chinese Space Science and Technology, 2020, 40(2): 10-.
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[7] |
LI Tao, XIAO Zhiwei, ZHANG Xiaoxiao.
On-orbit temperature field calculation and deploying opportunity analysis for large net-shape antennas′ deploying process
[J]. Chinese Space Science and Technology, 2018, 38(4): 44-50.
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[8] |
CHEN Xin, WEI Bingyi, WEN Xin.
Study of support vector machine based faults diagnosis for satellite′s actuators
[J]. Chinese Space Science and Technology, 2018, 38(2): 47-55.
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[9] |
SONG Xin, ZHANG You-Wei, ZHOU Xiang-Dong, LIU Zi-Jun.
Thermal Control Design for Topography Camera of Chang'e-3 Under High Temperature Environment o fLunar Surface
[J]. , 2014, 34(6): 65-.
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[10] |
LI Jin-Wang, ZOU Yong, CHENG Lin.
StartupandOperatingCharacteristics ofCapillaryWickEvaporator
[J]. , 2012, 32(2): 43-47.
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[11] |
NING Xian-Wen, ZHANG Jia-Xun.
Spacecraft Thermal Control Technology Based onVariable Frequency Pump
[J]. , 2011, 31(2): 47-52.
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[12] |
HU Tai-Bin, ZHANG Wei.
Effect of AIT Environment on Properties of Satellite Thermal Control Coatings
[J]. , 2010, 30(5): 59-63.
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[13] |
MA Mian-Jun, HUO Hong-Qing, ZHANG Xiao-Qing.
Passive Thermal Control Technologies of Exploration Instrument for Soft landing on Moon Surface
[J]. , 2010, 30(5): 64-68.
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[14] |
Tu Zhengkai1 Liu Wei2 Liu Zhichun2 Fan Aiwu2 (1 State Key Laboratory of Advanced Technology for Materials Synthesis and Progressing,Wuhan University of Technology,Wuhan 430070) (2 College of Energy and Power Engineering,Huazhong University of Science and Technology,Wuhan 430074).
Stability of the Condensing Interface in a Capillary Loop with Phase Change
[J]. , 2010, 30(04): 64-70.
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[15] |
Yang Huning Zhong Qi(Beijing Institute of Spacecraft System Engineering,Beijing 100094).
Monte Carlo Method for Thermal Model of Spacecraft Parametric Analysis and Robustness Determination
[J]. , 2009, 29(05): 21-27.
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