Article ID Journal Published Year Pages File Type
647602 Applied Thermal Engineering 2011 9 Pages PDF
Abstract

A mechanically pumped CO2 two-phase loop cooling system was developed for the temperature control of the silicon tracker of AMS-02, a cosmic particle detector to work in the International Space Station. The cooling system (called TTCS, or Tracker Thermal Control System), consists of two evaporators in parallel to collect heat from the tracker’s front-end electronics, two radiators in parallel to emit the heat into space, and a centrifugal pump that circulates the CO2 fluid that carries the heat to the radiators, and an accumulator that controls the pressure, and thus the temperature of the evaporators. Thermal vacuum tests were performed to check and qualify the system operation in simulated space thermal environment. In this paper, we reported the test results which show that the TTCS exhibited excellent temperature control ability, including temperature homogeneity and stability, and self-adaptive ability to the various external heat flux to the radiators.

Graphical abstractFigure optionsDownload full-size imageDownload as PowerPoint slideHighlights► The active-pumped CO2 two-phase cooling loop passed the thermal vacuum test. ► It provides high temperature homogeneity and stability thermal boundaries. ► Its working temperature is controllable in vacuum environment. ► It possesses self-adaptive ability to imbalanced external heat fluxes.

Keywords
Related Topics
Physical Sciences and Engineering Chemical Engineering Fluid Flow and Transfer Processes
Authors
, , , , , , , , , , , ,