NASA NTRS · 19790001965
Spacecraft active thermal control technology status
Abstract
Four 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.
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Ellis, W. E.. 1978-09-01. Spacecraft active thermal control technology status. https://ntrs.nasa.gov/citations/19790001965
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