Japan Geoscience Union Meeting 2025

Presentation information

[J] Oral

P (Space and Planetary Sciences ) » P-PS Planetary Sciences

[P-PS08] Lunar Science and Exploration

Fri. May 30, 2025 3:30 PM - 5:00 PM 302 (International Conference Hall, Makuhari Messe)

convener:Yusuke Nakauchi(Ritsumeikan University), Keisuke Onodera(Institute for Planetary Materials, Okayama University), Yoshiaki Ishihara(Japan Aerospace Exploration Agency), Ayame Ikeda(Geological Survey of Japan, AIST), Chairperson:Keisuke Onodera(Institute for Planetary Materials, Okayama University), Yoshiaki Ishihara(Japan Aerospace Exploration Agency)

3:30 PM - 3:45 PM

[PPS08-19] Pressure Dependence of Thermal Conductivity in Lunar Regolith from Apollo17 and Its Implications for Lunar Heat Flow Estimation

*Satoshi Tanaka1, Naoya Sakatani1, Sota Arakawa2, Akira Tsuchiyama6, Taizo Kobayashi6, Rie Endo4, Tsuyoshi Nishi5, Satoshi Matsumura3, Akihiko Kondo3 (1.Department of Solid Planetary Sciences Institute of Space and Astronautical Science, 2.Japan Agency for Marine Earth Science and Technology, 3.National Institute of Maritime, Port and Aviation Technology, Port and Airport Research Institute, 4.Shibaura Institute of Technology, 5.Ibaraki University, 6.Ritsumeikan University)

Keywords:heat flow, regolith, thermal conductivity

We have organized an analysis team primarily focused on physical property measurements and obtained lunar regolith samples. The samples were collected from the Apollo 15 and 17 sites near the locations where the lunar crust heat flux had been measured. These samples, Fine Regolith (70000, 0161, and 15031), were collected in 5g amounts from each site.

To date, we have measured the thermal conductivity of the Apollo 17 regolith using a pressurized thermal conductivity measurement device (Sakatani et al., 2020) under vacuum and ambient conditions, up to a pressure of 150 kPa.

The results showed that, in an uncompressed state, the thermal conductivity was 0.004 W/m/K. Under the measured pressure range, the thermal conductivity increased approximately linearly with pressure, and the pressure dependence was about 10-5 (W/m/K/kPa). The crustal heat flow data from Langseth et al. (1976) assumed a thermal conductivity of 0.01 W/m/K for the lunar regolith. Based on the data obtained in this study, it suggests that the lunar crustal heat flow may be estimated to be approximately half of what was previously assumed, which could have significant implications for constraining the thermal history of the Moon.


references)
Langseth, M.G., Keihm, S., and Peters, K.(1976), Revised heat-flow values, Proc. Lunar Sci. Conf.(7th), 3143-3171.

Sakatani, N., Tanaka, S., & Arakawa, S. (2022). Development of a Small-Sized Line Heat Source Apparatus for the Thermal Conductivity Measurement of Extraterrestrial Soils. International Journal of Thermophysics, 43(6). https://doi.org/10.1007/s10765-022-03007-y