Discrete Element Modeling of Strength Properties of Johnson Space Center (JSC-1A) Lunar Regolith Simulant
Publication: Journal of Aerospace Engineering
Volume 23, Issue 3
Abstract
This paper simulates the three-dimensional axisymmetric triaxial compression of JSC-1A lunar regolith simulant under lunar and terrestrial gravity environments under a wide range of confining pressures and relative densities. To accomplish this, the discrete element method (DEM), using Particle Flow Code In Three-Dimensional (PFC3D) software, was employed. The paper focuses on the peak and the critical state (CS) friction angles, which were predicted in the ranges of 35.4°–82.7° and 31.2°–79.8°, respectively, depending on the specimen density and confining pressure. A significant increase in peak and CS friction angles was predicted at near-zero confining pressure. The DEM results validated an empirical model that relates the peak friction angle with the CS friction angle, relative density, and mean effective stress at the CS. Comparison of DEM results with lunar in situ measurements of friction angle, from Apollo missions and other extraterrestrial laboratory experiments under a microgravity environment, shows a favorable agreement.
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Acknowledgments
The writers would like to acknowledge the financial support provided by the Louisiana Board of Regents–Louisiana Space Consortium under Contract No. UNSPECIFIEDNASA/LEQSF(2006)-DART-22.
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Received: Dec 7, 2008
Accepted: Jun 8, 2009
Published online: Jan 18, 2010
Published in print: Jul 2010
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