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Flexible Cryogenic Heat Pipe Development ProgramA heat pipe was designed for operation in the 100 - 200 K temperature range with maximum heat transport as a primary design goal; another designed for operation in the 15 - 100 K temperature range with maximum flexibility as a design goal. Optimum geometry and materials for the container and wicking systems were determined. The high power (100 - 200 K) heat pipe was tested with methane at 100 - 140 K, and test data indicated only partial priming with a performance limit of less than 50 percent of theoretical. A series of tests were conducted with ammonia at approximately 280 K to determine the performance under varying fluid charge and test conditions. The low temperature heat pipe was tested with oxygen at 85 - 95 K and with methanol at 295 - 315 K. Performance of the low temperature heat pipe was below theoretical predictions. Results of the completed testing are presented and possible performance limitation mechanisms are discussed. The lower-than-expected performance was felt to be due to small traces of non-condensible gases which prevented the composite wick from priming.
Document ID
19770022507
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 3, 2013
Publication Date
July 1, 1976
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-152027
SD-77-AP-0088
Report Number: NASA-CR-152027
Report Number: SD-77-AP-0088
Accession Number
77N29451
Funding Number(s)
CONTRACT_GRANT: NAS2-8830
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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