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 |
DOI | 10.18462/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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