用于空间BIB探测器的0.3 [email protected] K大冷量轻量化低温系统
作者:
作者单位:

1.中国科学院上海技术物理研究所,上海 200083;2.中国科学院大学,北京 100049

作者简介:

通讯作者:

中图分类号:

TN215

基金项目:


A 0.3 [email protected] K high-capacity lightweight cryogenic system for space BIB detection
Author:
Affiliation:

1.Shanghai Institute of Technical Physics, Chinese Academy of Sciences, Shanghai 200083, China;2.University of Chinese Academy of Sciences, Beijing 100049, China

Fund Project:

Supported by the Hundred Talents Program of the Chinese Academy of Sciences, the National Natural Science Foundation Projects (51806231), the Strategic Priority Research Program of Chinese Academy of Sciences (XDB35000000, XDB35040102)

  • 摘要
  • |
  • 图/表
  • |
  • 访问统计
  • |
  • 参考文献
  • |
  • 相似文献
  • |
  • 引证文献
  • |
  • 资源附件
  • |
  • 文章评论
    摘要:

    大阵列BIB探测器由于其高量子效率和低暗电流而成为广泛的研究对象,特别是在空间应用方向。如2021年发射的詹姆斯韦伯太空望远镜,它已经进行了许多重要的天文观测。一个稳定、高效、轻量化的液氦温区低温系统对BIB探测器的运行至关重要。氦节流制冷机可取代传统的大容积液氦杜瓦,能满足空间液氦温区的制冷要求。为了同时提高4.2 K的制冷量并减轻重量,提出了一种0.3 [email protected] K的大冷量轻量化的4.2 K低温制冷系统。并且在现有0.1 [email protected] K制冷量的低温系统上进行实验,验证了该系统的设计方法。在不同的冷却温度区采用不同的冷却方法,以实现冷却的高效性和轻便性。开发了一个新的集成斯特林制冷机,在80 K时提供高效的一级预冷,制冷量为15 W,重量仅为4.5 kg;二级预冷采用主动活塞调相的15 K脉管制冷机,制冷量为0.9 W。此多级低温制冷系统通过耦合氦气JT循环,可以在4.2 K时提供0.3 W的制冷量,输入功低于1.8 kW。此系统将为正在快速发展的红外天文观测所需的空间BIB探测器提供保障。

    Abstract:

    Large-array BIB detectors have been the subject of extensive research due to their high quantum efficiency and low dark current, particularly for space applications such as the JWST, which was launched in 2021 and has made numerous significant astronomical observations. A stable, efficient, and lightweight temperature zone liquid helium cryogenic system is essential to the operation of the BIB detectors. The helium JT cryocooler is a trend that aims to meet the cooling requirements of a liquid helium temperature zone in space while supplanting the traditional, large-volume liquid helium dewar. To simultaneously increase the cooling capacity at 4.2 K and reduce its weight, a high-capacity, lightweight 4.2 K cryocooler with a cooling power of 0.3 [email protected] K is proposed. Experiments on the previous 0.1 W at 4.1 K prototype of the cryogenic system have validated the system''s design method. Different cooling methods are used in different cooling temperature zones to achieve the efficiency and lightness of cooling. A new integrated Stirling cryocooler was developed to provide efficient pre-cooling at 80 K, with a cooling capacity of 15 W and a weight of only 4.5 kg. A 0.9 W at 15 K active piston phase-shifting pulse tube cryocooler is used to improve the efficiency of the second-stage pre-cooling. The developing cryogenic system can provide a cooling capacity of 0.3 W at 4.2 K with a power consumption of less than 1.8 kW by coupling the helium JT cycle. It will provide the essential guarantee for the large-scale BIB detection required for infrared astronomical observation, which is undergoing rapid development.

    参考文献
    相似文献
    引证文献
引用本文

褚晋简,刘少帅,王鹏,丁磊,肖云龙,殷旺,陈志超,沙鑫权,蒋珍华,吴亦农.用于空间BIB探测器的0.3 [email protected] K大冷量轻量化低温系统[J].红外与毫米波学报,2023,42(6):883~894]. CHU Jin-Jian, LIU Shao-Shuai, WANG Peng, DING Lei, XIAO Yun-Long, YIN Wang, CHEN Zhi-Chao, SHA Xin-Quan, JIANG Zhen-Hua, WU Yi-Nong. A 0.3 [email protected] K high-capacity lightweight cryogenic system for space BIB detection[J]. J. Infrared Millim. Waves,2023,42(6):883~894.]

复制
分享
文章指标
  • 点击次数:
  • 下载次数:
  • HTML阅读次数:
  • 引用次数:
历史
  • 收稿日期:2023-03-08
  • 最后修改日期:2023-08-16
  • 录用日期:2023-04-11
  • 在线发布日期: 2023-08-06
  • 出版日期:
文章二维码