Air Liquide space cryocooler systems
暂无分享,去创建一个
J. Tanchon | T. Trollier | A. Ravex | P. Crespi | J. Buquet | T. Trollier | J. Tanchon | J. Buquet | P. Crespi | Alain Ravex
[1] Jérôme Guichard,et al. Design and Qualification of HERSCHEL Instrument Helium Cooling System , 2005 .
[2] Achim Seidel,et al. A −180°C Cryogenic Freezer for the International Space Station , 2005 .
[3] L. Duband,et al. Performance Test Results of a Miniature 50 to 80 K Pulse Tube Cooler , 2005 .
[4] L. Duband,et al. Performance testing of a large heat lift 40 to 80K pulse tube cooler for space applications , 2007, SPIE Defense + Commercial Sensing.
[5] Lionel Duband,et al. Design of a large heat lift 40 K to 80 K pulse tube cryocooler for space applications , 2007 .
[6] P. Camus,et al. Cryogenic Tests of a 0.1 K Dilution Cooler for Planck-HFI , 2005 .
[7] Achim Seidel,et al. Cryogenic Tests of a Development Model for the 90 K Freezer for the International Space Station , 2005 .