1970
DOI: 10.1126/science.168.3928.211
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Apollo 13 Lunar Heat Flow Experiment

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Cited by 32 publications
(44 citation statements)
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“…The probes were inserted into predrilled holes, which were fitted with a fiberglass borestem. [Langseth et al, 1973] as well as the attenuation of the annual temperature wave [Langseth et al, 1976]. For the calculation of thermal conductivities from thermal diffusivities a heat capacity of 670 J kg −1 K −1 has been assumed.…”
Section: Introductionmentioning
confidence: 99%
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“…The probes were inserted into predrilled holes, which were fitted with a fiberglass borestem. [Langseth et al, 1973] as well as the attenuation of the annual temperature wave [Langseth et al, 1976]. For the calculation of thermal conductivities from thermal diffusivities a heat capacity of 670 J kg −1 K −1 has been assumed.…”
Section: Introductionmentioning
confidence: 99%
“…[2] Lunar heat flow has been measured at the Hadley Rille and Taurus-Littrow sites during the Apollo 15 and 17 missions and values of 21 and 16 mW m −2 have been obtained [Langseth et al, 1972a[Langseth et al, , 1972b[Langseth et al, , 1973[Langseth et al, , 1976. Uncertainties for these values are given at ±15%, which mainly stem from the uncertainty connected to the regolith's thermal conductivity, although no rigorous error analysis was presented.…”
Section: Introductionmentioning
confidence: 99%
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“…Up to now they have only been performed successfully at two places on the Moon, in the frame of the Apollo 15 and 17 missions (Langseth et al 1972(Langseth et al , 1976. These pioneering in situ measurements showed that the uppermost layers of the lunar regolith have an extremely low thermal conductivity, which is probably caused by the loose packing and irregular shape of the lunar soil particles (Pilbeam and Vaisnys 1973).…”
Section: Introductionmentioning
confidence: 99%