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Thermal conductivity of Apollo 16 lunar finesThe vacuum thermal conductivity of the Apollo 16 fines is presented as a function of temperature for the approximate range of diurnal temperatures on the moon. The density used is 1500 kg/cu m, which is approximately the density of the core-tube samples returned from the landing site. The thermal diffusivity was calculated from the conductivity, density, and specific heat and is also presented.
Document ID
19750055641
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Cremers, C. J.
Hsia, H. S.
(Kentucky, University Lexington, Ky., United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1974
Subject Category
Lunar And Planetary Exploration
Meeting Information
Meeting: Lunar Science Conference
Location: Houston, TX
Start Date: March 18, 1974
End Date: March 22, 1974
Accession Number
75A39713
Funding Number(s)
CONTRACT_GRANT: NGR-18-001-060
Distribution Limits
Public
Copyright
Other

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