NASA NTRS ยท 19760016258
Space tug thermal control follow-on
Abstract
The Space Tug Thermal Control Follow-On program was conducted to further explore some of the thermal control concepts proposed for use in space tug in a breadboard test program. The objectives were to demonstrate the thermal control capabilities of a louver/battery configuration and a thermal conditioning panel/heat pipe radiator configuration. An additional objective was added to model the header pipe and radiator of the second test and correlate the analysis with the test results. These three objectives were achieved and are discussed within this report.
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Ward, T. L.. 1975-10-01. Space tug thermal control follow-on. https://ntrs.nasa.gov/citations/19760016258
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