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Solid-state Distributed Temperature Control for International Space StationA newly developed solid-state temperature controller will offer greater flexibility in the thermal control of aerospace vehicle structures. A status of the hardware development along with its implementation on the Multi- Purpose Logistics Module will be provided. Numerous advantages of the device will also be discussed with regards to current and future flight vehicle implementations.
Document ID
20040085963
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Holladay, Jon B. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Reagan, Shawn E. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Day, Greg (Boeing Co. United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2004
Subject Category
Spacecraft Instrumentation And Astrionics
Report/Patent Number
SAE-2004-01-2430
Meeting Information
Meeting: 34th International Conference on Environmental Systems
Location: Colorado Springs, CO
Country: United States
Start Date: July 19, 2004
End Date: July 22, 2004
Sponsors: Society of Automotive Engineers International
Distribution Limits
Public
Copyright
Public Use Permitted.

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