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Space tug thermal control follow-onThe 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.
Document ID
19760016258
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ward, T. L.
(Martin Marietta Corp. Denver, CO, United States)
Date Acquired
September 3, 2013
Publication Date
October 1, 1975
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
MCR-75-270
NASA-CR-144029
Report Number: MCR-75-270
Report Number: NASA-CR-144029
Accession Number
76N23346
Funding Number(s)
CONTRACT_GRANT: NAS8-30746
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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