This paper describes the internal thermal control system (ITCS) cold plate/fluid-stability test setup and summarizes the test results obtained to date. The test investigates ITCS-coolant stability and cold-plate debonding over time (3 yr). The setup is consistent with flight materials, cleaning procedures, and loop-servicing procedures. The components include two flight cold plates, a qualification interface heat exchanger, qualification pump package assembly (PPA) gas trap and fluid filter, and a representative–length Teflon hose. A biofilm section of the test setup is included to evaluate long-term effects of microbial growth on representative ITCS materials. The flight-like test facility was developed at NASA Marshall Space Flight Center (MSFC) at the environmental control and life support systems (ECLSS) ITCS test facility.
International Space Station Internal Thermal Control System Cold Plate/Fluid-Stability Test Setup and Preliminary Test Results
Sae Technical Papers
31st International Conference On Environmental Systems ; 2001
09.07.2001
Aufsatz (Konferenz)
Englisch
British Library Conference Proceedings | 2001
|British Library Conference Proceedings | 2003
|SAE Technical Papers | 2003
|Preliminary design of the space station internal thermal control system
Tema Archiv | 1987
|