Image Details
Caption: Figure 5.
(A) Plot of radius decrease ΔR and areal contractional strain ε as a function of fault plane dip θ. ΔR are determined by combining fractional areal strain for the highlands εLS and for maria εSMR. Area shaded in gray marks the likely range of θ of typical thrust faults (25°–35°). (B) Plot of estimated compressional stress as a function of the amount of radial contraction of the Moon.
© 2026. The Author(s). Published by the American Astronomical Society.