학술논문
Development of a Thermal Control System with Mechanically Pumped CO2 Two-Phase Loops for the AMS-02 Tracker on the ISS
Document Type
Working Paper
Author
Alberti, G.; Alvino, A.; Ambrosi, G.; Bardet, M.; Battiston, R.; Borsini, S.; Cao, J. F.; Chen, Y.; van Es, J.; Gargiulo, C.; Guo, K. H.; Guo, L.; He, Z. H.; Huang, Z. C.; Koutsenko, V.; Laudi, E.; Lebedev, A.; Lee, S. C.; Li, T. X.; Lin, Y. L.; Lv, S. S.; Menichelli, M.; Miao, J. Y.; Mo, D. C.; Ni, J. Q.; Pauw, A.; Qi, X. M.; Shue, G. M.; Sun, D. J.; Sun, X. H.; Tang, C. P.; Verlaat, B.; Wang, Z. X.; Weng, Z. L.; Xiao, W. J.; Xu, N. S.; Yang, F. K.; Yeh, C. C.; Zhang, Z.; Zwartbol, T.
Source
Subject
Language
Abstract
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).