IAG-IASPEI 2017

講演情報

Oral

IASPEI Symposia » S19. Planetary seismology

[S19-2] Apollo seismic data re-processing and future lunar seismology project

2017年7月31日(月) 10:30 〜 12:00 Room 402 (Kobe International Conference Center 4F, Room 402)

Chairs: Taichi Kawamura (National Astronomical Observatory of Japan) , Nicholas Schmerr (University of Maryland)

10:30 〜 10:45

[S19-2-01] Seismic velocity and crustal thickness inversions: Moon and Mars

Melanie Drilleau1, Jean-Francois Blanchette-Guertin1, Taichi Kawamura2, Philippe Lognonne1, Mark Wieczorek1,3 (1.Institut de Physique du Globe de Paris, Paris, France, 2.National Astronomical Observatory of Japan, Iwate, Japan, 3.Laboratoire Lagrange, Observatoire de la Cote d'Azur, Nice, France)

We present results from new inversions of seismic data arrival times acquired by the Apollo active and passive experiments. McMC inversions are used to constrain (i) 1-D lunar crustal and upper mantle velocity models and (ii) 3-D lateral crustal thickness models under the Apollo stations and the impact sites. A full 3-D model of the lunar crustal thickness is then obtained using the GRAIL gravimetric data. To avoid the use of any seismic reference model, a Bayesian inversion technique is implemented. We obtain robust probability density functions of interior structure parameters governed by uncertainties on the seismic data arrival times. The parameters of the inversion include the seismic velocities of P and S waves as a function of depth, the crustal thickness under each Apollo station and impact epicentre. The forward problem consists in a ray tracing method enabling both the relocation of the natural impact epicenters, and the computation of time corrections associated to the surface topography and the crustal thickness variations under the stations and impact sites. The results show geology-related differences between the different sites, which are due to contrasts in megaregolith thickness and to shallow subsurface composition and structure. However, we use the more precise LROC-located epicentral locations for the lunar modules and Saturn-IV upper stage artificial impacts, reducing some of the uncertainties observed in past studies. In the framework of the NASA InSight/SEIS mission to Mars, the method developed in this study will be used to constrain the Martian crustal thickness as soon as the first data will be available. For Insight, impacts will be located by MRO data differential analysis, which provide a known location enabling the direct inversion of all differential travel times with respect to P arrival time. Due to the high flexibility of the algorithm, the interior model will be refined each time a new event will be detected.