Cryocooler options for NGST and other space applications

被引:0
|
作者
Lindensmith, CA [1 ]
Bowman, RC [1 ]
Wade, LA [1 ]
Crumb, D [1 ]
机构
[1] CALTECH, Jet Prop Lab, Pasadena, CA 91109 USA
来源
关键词
D O I
暂无
中图分类号
P1 [天文学];
学科分类号
0704 ;
摘要
We have assessed the technology status of long-life cryocoolers for space applications below 20 K. Two-stage Joule-Thomson (J-T) cryocoolers are found to be the best candidates for a possible Next Generation Space Telescope (NGST) mid-infrared camera. A combination of a 20 K hydrogen J-T cooler using a sorption compressor precooling a 4 K helium J-T cooler using a mechanical compressor will be flight proven on Planck and provides the lowest risk option for NGST. The 4 K mechanical cooler can be replaced by a 6 K cooler that uses helium as a working gas and charcoal sorbent material in a J-T cycle to provide a vibration-free continuous-cycle cooler. We present a conceptual design and predicted performance for such a helium/charcoal sorption cooler. To provide 10 mW heat lift at 6 K such a cooler would require a total input power of approximately 93.4 W, and have a system mass of approximate to 33 kg. These coolers will also provide enabling technology for future missions, such as TPF, SPECS and IRSI.
引用
收藏
页码:106 / 115
页数:8
相关论文
共 50 条
  • [1] Turbo-Brayton cryocooler for NGST
    Zagarola, MV
    Swift, WL
    NGST SCIENCE AND TECHNOLOGY EXPOSITION, 2000, 207 : 196 - 202
  • [2] A 10 K cryocooler for space applications
    Glaister, DS
    Gully, WJ
    Wright, GP
    Simmons, DW
    Tomlinson, BJ
    CRYOCOOLERS 11, 2001, : 505 - 511
  • [3] Cryocooler reliability issues for space applications
    Marquardt, ED
    CRYOGENICS, 2001, 41 (11-12) : 845 - 849
  • [4] DILUTION REFRIGERATOR FOR SPACE APPLICATIONS WITH A CRYOCOOLER
    BENOIT, A
    PUJOL, S
    CRYOGENICS, 1994, 34 (05) : 421 - 423
  • [5] Joule-Thomson cryocooler for space applications
    Levenduski, R
    Scarlotti, R
    CRYOGENICS, 1996, 36 (10) : 859 - 866
  • [6] Assessment of the state of cryocooler technology for space applications
    Glaister, D.S.
    Donabedian, M.
    Curran, D.G.T.
    Davis, T.
    IEEE Aerospace Applications Conference Proceedings, 1999, 5 : 367 - 382
  • [7] Hybrid 10 K cryocooler for space applications
    Levenduski, R
    Gully, W
    Lester, J
    CRYOCOOLERS 10, 1999, : 505 - 511
  • [8] Miniature pulse tube cryocooler for space applications
    Nast, TC
    Champagne, PJ
    Kotsubo, V
    Olson, J
    Collaco, A
    Evtimov, B
    Renna, T
    Clappier, R
    CRYOCOOLERS 11, 2001, : 145 - 154
  • [9] Characterization of the NGST 150 K mini pulse tube cryocooler
    Abhyankar, NS
    Davis, TM
    Curran, DGT
    CRYOCOOLERS 13, 2005, : 85 - 92
  • [10] Design of a Miniature Pulse Tube Cryocooler for space applications
    Trollier, T
    Ravex, A
    Charles, I
    Duband, L
    Mullié, J
    Bruins, P
    Benschop, T
    Linder, M
    ADVANCES IN CRYOGENIC ENGINEERING, VOLS. 49A AND B, 2004, 710 : 1318 - 1325