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Spacecraft active thermal control technology statusFour advanced space radiator concepts that were pursued in an integrated effort to develop multi-mission-use and low cost heat rejection systems which can overcome the limitations of current radiator systems are briefly discussed and described. Also, in order to establish a firm background to compare the advanced space radiator concepts, the Orbiter active thermal control system is also briefly described.
Document ID
19790001965
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ellis, W. E. (NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
August 9, 2013
Publication Date
September 1, 1978
Publication Information
Publication: NASA. Lewis Res. Center Future Orbital Power Systems Technol. Requirements
Subject Category
Spacecraft Propulsion And Power
Accession Number
79N10136
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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