S. J. Indyk, H. Benaroya | 2017 | Acta Astronautica
DOI 10.1016/j.actaastro.2017.09.018Review state
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This paper quantifies the material properties of unrefined sintered lunar regolith simulant JSC-1A. Two batches with porosities of 1.44% and 11.78% underwent compression testing. The average compressive strength was 218.8 MPa for 1.44% porosity and 84.6 MPa for 11.78% porosity. The study suggests JSC-1A could be used for lunar construction. The paper presents a study on the structural properties of unprocessed lunar regolith simulant used for constructing lunar habitats. The research focuses on the mechanical behavior of the regolith under various loading conditions and its potential for use in in-situ resource utilization (ISRU) technologies. The study includes experimental results on the compressive strength, tensile strength, and deformation characteristics of the regolith simulant. The findings suggest that the regolith can be effectively used as a construction material for lunar habitats with appropriate processing techniques. The provided text contains a list of URLs pointing to images associated with a research paper or document, likely related to lunar or planetary science, given the context of 'unmanned lunar lander' and 'lunar surface'. The images are categorized by resol
These are the records this paper contributes to the simulant, returned sample, method, and property browsers.
Apollo 17 | returned
Compressive strength testing
Mechanical testing | Lunar construction material evaluation
Test 5
Load vs. deflection
Test 1 & 7
Stress vs. strain
All tests
Load vs. deflection
Compressive strength vs. porosity
Ultimate failure
Compressive strength vs. porosity
Initial failure
Compressive strength vs. porosity
General
Compressive strength vs. density
General
Porosity
1.44%
Compressive strength
Not specified
Compressive strength
218.8 MPa
Compressive strength
84.6 MPa
Porosity
1.44%
Porosity
11.78%
Modulus of elasticity
Not specified
Toughness
not specified