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. These properties along with the reflectance and emittance are used in a calculation of temperature in the lunar surface layer.


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    Titel :

    Thermal characteristics of Apollo 16 lunar fines


    Beteiligte:
    Cremers, C. J. (Autor:in) / Hsia, H. S. (Autor:in) / Birkebak, R. C. (Autor:in)

    Kongress:

    Heat transfer 1974 ; 1974 ; Tokyo, Japan


    Erscheinungsdatum :

    01.01.1974


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Thermal conductivity of Apollo 15 lunar fines

    Cremers, C. J. / Hsia, H. S. | NTRS | 1974


    Thermal conductivity of Apollo 16 lunar fines

    Cremers, C. J. / Hsia, H. S. | NTRS | 1974


    Physical properties of the Apollo 12 lunar fines

    Campbell, M. / Gold, T. / Oleary, B. T. | NTRS | 1971


    Physical Properties of the APOLLO 12 Lunar Fines

    M. Campbell / T. Gold / B. T. Oleary | NTIS | 1971


    Physical Properties of the APOLLO 12 Lunar Fines

    M. Campbell / T. Gold / B. T. Oleary | NTIS | 1971