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International Space Station Internal Thermal Control System Cold Plate/Fluid-Stability Test: Two Year UpdateOperation of the Internal Thermal Control System (ITCS) Cold Plate/Fluid-Stability Test Facility commenced on September 5, 2000. The facility was intended to provide advance indication of potential problems on board the International Space Station (ISS) and was designed:
- To be materially similar to the flight ITCS.
- To allow for monitoring during operation.
- To run continuously for three years.

During the first two years of operation the conditions of the coolant and components were remarkably stable. During this same period of time, the conditions of the ISS ITCS significantly diverged from the desired state. Due to this divergence, the test facility has not been providing information useful for predicting the flight ITCS condition.

Results of the first two years are compared with flight conditions over the same time period, showing the similarities and divergences. To address the divergences, the test facility was modified slightly to more closely match the flight conditions, and to gain insight into the reasons for the divergence. Results of the modifications are discussed and provide insight into the development of the conditions on orbit.
Document ID
20030068420
Acquisition Source
Marshall Space Flight Center
Document Type
Reprint (Version printed in journal)
Authors
Paul Wieland
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Mike Holt
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Monsi Roman
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Harold Cole
(Boeing (United States) Chicago, Illinois, United States)
Steve Daugherty
(Boeing (United States) Chicago, Illinois, United States)
Date Acquired
August 21, 2013
Publication Date
January 1, 2003
Publication Information
Publication: International Space Station Internal Thermal Control System Cold Plate/Fluid-Stability Test - Two Year Update
Publisher: SAE International
ISSN: 0148-7191
e-ISSN: 2688-3627
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
SAE Paper-2003-01-2518
Meeting Information
Meeting: 33rd International Conference on Environmental Systems
Location: Vancouver, British Columbia
Country: CA
Start Date: July 7, 2003
End Date: July 10, 2003
Sponsors: SAE International
Funding Number(s)
PROJECT: RTOP 336-33-30
Distribution Limits
Public
Copyright
Public Use Permitted.
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