Development of continuous ADR system for weak gravity missions

被引:5
作者
Numazawa, T. [1 ]
Kamiya, K. [1 ]
Shirron, P. [2 ]
Mitsuda, K. [3 ]
机构
[1] NIMS, Tsukuba Magnet Lab, 3-13 Sakura, Tsukuba, Ibaraki 3050003, Japan
[2] NASA, Goddard Space Flight Ctr, Greenbelt, MD 20771 USA
[3] JAXA, ISAS, Sagamihara, Kanagawa 2298510, Japan
来源
25TH INTERNATIONAL CONFERENCE ON LOW TEMPERATURE PHYSICS (LT25), PART 1: CRYOGENIC TECHNOLOGIES AND APPLICATIONS | 2009年 / 150卷
关键词
D O I
10.1088/1742-6596/150/1/012032
中图分类号
O414.1 [热力学];
学科分类号
摘要
Adiabatic Demagnetization Refrigeration (ADR) does not use working fluids contrary to conventional refrigerators that make use of the fluid density difference, which leads to superiority of the ADR under the weak gravity condition. In this study, we developed a continuous ADR system to provide constant cooling temperatures similar to 0.1 K. The system consists of four stages of magnetic materials and magnets cascaded with heat switches. The magnetic materials CPA and GdLiF4 are used for 3 stages between 0.1K and 1.4 K, and single stage between 1.4 K and 4 K, respectively. Passive heat switches are used for the stages > 0.3 K and a superconducting heat switch is used for the continuous stage at similar to 0.1 K. A G-M cycle cooler with a 100 V compressor unit is used to cool the ADR and cryostat shieldings. Total mass of flight model is less than 60 kg. Cooling tests with Transition Edge Sensor on the ground showed that the ADR provided continuous cooling temperatures between 105 mK and 120 mK and it successfully operated the TES. Airborne flight experiments confirmed the ability of the cooling system under the mili-gravity condition. The experimental results showed that the ADR could provide stable temperature under the weak gravity, however, strong vibrations coming from turbulence or takeoff affected to the stability of ADR cycle.
引用
收藏
页数:4
相关论文
共 4 条
[1]   Continuous cooling from 10 to 4 K using a toroidal ADR [J].
DiPirro, M ;
Canavan, E ;
Shirron, P ;
Tuttle, J .
CRYOGENICS, 2004, 44 (6-8) :559-564
[2]  
Numazawa T., 2006, AIP C P UNPUB
[3]  
Shirron P.J., 2000, Advances in Cryogenic Engineering, P1629, DOI DOI 10.1007/978-1-4615-4215-586
[4]  
SHIRRON PJ, 2002, P 12 INT CRYOC C JUN