The 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.
Thermal conductivity of Apollo 16 lunar fines
Lunar Science Conference ; 1974 ; Houston, TX
1974-01-01
Miscellaneous
No indication
English
Thermal conductivity of Apollo 15 lunar fines
NTRS | 1974
|Thermal characteristics of Apollo 16 lunar fines
NTRS | 1974
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NTRS | 1972
|Thermal conductivity of fines from Apollo 12
NTRS | 1971
|Physical properties of the Apollo 12 lunar fines
NTRS | 1971
|