<italic>International Space Station</italic> Internal Thermal Control System Cold Plate/Fluid-Stability Test Setup and Preliminary Test Results

2001-01-2334

07/09/2001

Event
31st International Conference On Environmental Systems
Authors Abstract
Content
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.
Meta TagsDetails
DOI
https://doi.org/10.4271/2001-01-2334
Pages
17
Citation
Ray, C., and Daugherty, R., "International Space Station Internal Thermal Control System Cold Plate/Fluid-Stability Test Setup and Preliminary Test Results," SAE Technical Paper 2001-01-2334, 2001, https://doi.org/10.4271/2001-01-2334.
Additional Details
Publisher
Published
Jul 9, 2001
Product Code
2001-01-2334
Content Type
Technical Paper
Language
English