%0 Journal Article
%T Development of a Thermal Control System with Mechanically Pumped CO2 Two-Phase Loops for the AMS-02 Tracker on the ISS
%A G. Alberti
%A A. Alvino
%A G. Ambrosi
%A M. Bardet
%A R. Battiston
%A S. Borsini
%A J. F. Cao
%A Y. Chen
%A J. van Es
%A C. Gargiulo
%A K. H. Guo
%A L. Guo
%A Z. H. He
%A Z. C. Huang
%A V. Koutsenko
%A E. Laudi
%A A. Lebedev
%A S. C. Lee
%A T. X. Li
%A Y. L. Lin
%A S. S. Lv
%A M. Menichelli
%A J. Y. Miao
%A D. C. Mo
%A J. Q. Ni
%A A. Pauw
%A X. M. Qi
%A G. M. Shue
%A D. J. Sun
%A X. H. Sun
%A C. P. Tang
%A B. Verlaat
%A Z. X. Wang
%A Z. L. Weng
%A W. J. Xiao
%A N. S. Xu
%A F. K. Yang
%A C. C. Yeh
%A Z. Zhang
%A T. Zwartbol
%J Physics
%D 2013
%I arXiv
%X To provide a stable thermal environment for the AMS-Tracker, a thermal control system based on mechanically pumped CO2 two-phase loops was developed. It has been operating reliably in space since May 19, 2011. In this article, we summarize the design, construction, tests, and performance of the AMS-Tracker thermal control system (AMS-TTCS).
%U http://arxiv.org/abs/1302.4294v1