中国科学院机构知识库网格
Chinese Academy of Sciences Institutional Repositories Grid
Design and Verification of Temperature-adjustable System for the Space Environment Simulator

文献类型:会议论文

作者Chao, H.E.1; Zhang, Min2; Zhou, Ying1; Li, Gao1; Ding, Wenjing1; Zhang, Lei1; Gu, Zhifei1; Zhang, Yi1; Li, Ang1; Wang, Xuezhang1
出版日期2019
会议日期April 8, 2019 - April 11, 2019
会议地点Prague, Czech republic
卷号Part F147717
DOI10.18462/iir.cryo.2019.0089
页码393-399
英文摘要

The temperature-adjustable system of the Space Environment Simulator was introduced, which can keep the thermal shield in the temperature range from 123 K to 423 K. Design method of the main equipments was supplied, and applied to KM2 space environment simulator. The main parameters such as the thermal load of the system, gaseous nitrogen’s mass flow, etc. were calculated, and the fan, main spray equipment and heater were selected according to the calculation result, numerical simulation was also conducted. Test verification has been completed, during the test the cool-down rate is 1.03 K/min and the Uniformity of the thermal shield temperature is better than ±5 K, which match well with the technical index. So the design method can be applied in the development of the similar system. © 2019 International Institute of Refrigeration. All rights reserved.

会议录Refrigeration Science and Technology
ISSN号0151-1637
源URL[http://ir.nssc.ac.cn/handle/122/7028]  
专题国家空间科学中心_空间科学部
作者单位1.Beijing Institute of Spacecraft Environment Engineering, Beijing; 100094, China;
2.National Space Science Center, Chinese Academy of Sciences, Beijing; 100190, China
推荐引用方式
GB/T 7714
Chao, H.E.,Zhang, Min,Zhou, Ying,et al. Design and Verification of Temperature-adjustable System for the Space Environment Simulator[C]. 见:. Prague, Czech republic. April 8, 2019 - April 11, 2019.

入库方式: OAI收割

来源:国家空间科学中心

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