contributor author | Masafumi Iai | |
contributor author | Ronaldo Luna | |
date accessioned | 2017-05-08T21:33:47Z | |
date available | 2017-05-08T21:33:47Z | |
date copyright | October 2011 | |
date issued | 2011 | |
identifier other | %28asce%29as%2E1943-5525%2E0000082.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/56225 | |
description abstract | A series of direct shear tests were conducted on the JSC-1A lunar regolith simulant in a 101.6-mm- (4-in.-) diameter container. The direct shear test provides a unique mode of failure that aids the development of excavation tools for the Moon. Relative density and normal load were varied to study the strength behavior of such granular material at peak and critical state conditions. The values of the internal friction angle ranged from 30 to 70°. A relationship between the internal friction angle of the direct shear and the published triaxial compression test results is presented. Additionally, the measured dilatancy angle is related to the difference in peak and critical state stress friction angles. | |
publisher | American Society of Civil Engineers | |
title | Direct Shear Tests on JSC-1A Lunar Regolith Simulant | |
type | Journal Paper | |
journal volume | 24 | |
journal issue | 4 | |
journal title | Journal of Aerospace Engineering | |
identifier doi | 10.1061/(ASCE)AS.1943-5525.0000082 | |
tree | Journal of Aerospace Engineering:;2011:;Volume ( 024 ):;issue: 004 | |
contenttype | Fulltext | |