The Astro-E2/XRS-2 helium insert system

被引:6
作者
Shirron, PJ [1 ]
DiPirro, MJ
Panek, J
Kelley, R
Mitsuda, K
Fujimoto, R
Hirabayashi, M
McCammon, D
机构
[1] NASA, Goddard Space Flight Ctr, Greenbelt, MD 20771 USA
[2] ISAS, JAXA, Sagamihara, Kanagawa 2298510, Japan
[3] Sumitomo Heavy Ind, Niihama, Ehime 7928588, Japan
[4] Univ Wisconsin, Dept Phys, Madison, WI 53706 USA
关键词
space cryogenics; space atronomy; superfluid helium; magnetic refrigeration;
D O I
10.1016/j.nima.2005.12.098
中图分类号
TH7 [仪器、仪表];
学科分类号
0804 ; 080401 ; 081102 ;
摘要
The X-ray Spectrometer (XRS-2) instrument on the Japanese Space Agency (JAXA) Astro-E2 spacecraft will measure faint X-ray emissions in the energy range of 0.2-10 keV. A square array of 32 X-ray microcalorimeters used will be able to distinguish individual photons to better than 10 eV at 6 keV, with a quantum efficiency near 100%. The detectors are cooled to 60 mK by means of an adiabatic demagnetization refrigerator (ADR). The ADR rejects heat to a 1.3 K superfluid helium tank, which is surrounded by a 17 K solid neon tank. A Stirling cycle cryocooler precools an outer shield around the neon tank. This system will provide an estimated 3 years of on-orbit lifetime. This paper describes the helium insert, the ADR, the high temperature superconducting leads, and early on-orbit performance. Published by Elsevier B.V.
引用
收藏
页码:666 / 668
页数:3
相关论文
共 5 条
[1]  
Breon SR, 1996, ADV CRYOG ENG, P1129
[2]   The Astro-E High Resolution X-ray Spectrometer [J].
Kelley, RL ;
Audley, MD ;
Boyce, KR ;
Breon, SR ;
Fujimoto, R ;
Gendreau, KC ;
Holt, SS ;
Ishisaki, Y ;
McCammon, D ;
Mihara, T ;
Mitsuda, K ;
Moseley, SH ;
Mott, DB ;
Porter, FS ;
Stahle, CK ;
Szymkowiak, AE .
EUV, X-RAY, AND GAMMA-RAY INSTRUMENTATION FOR ASTRONOMY X, 1999, 3765 :114-127
[3]  
Serlemitsos AT, 1998, ADV CRYOG ENG, V43, P957
[4]  
Shirron PJ, 1998, ADV CRYOG ENG, V43, P949
[5]  
Tuttle JG, 1998, ADV CRYOG ENG, V43, P965