YaBeSH Engineering and Technology Library

    • Journals
    • PaperQuest
    • YSE Standards
    • YaBeSH
    • Login
    View Item 
    •   YE&T Library
    • ASCE
    • Journal of Aerospace Engineering
    • View Item
    •   YE&T Library
    • ASCE
    • Journal of Aerospace Engineering
    • View Item
    • All Fields
    • Source Title
    • Year
    • Publisher
    • Title
    • Subject
    • Author
    • DOI
    • ISBN
    Advanced Search
    JavaScript is disabled for your browser. Some features of this site may not work without it.

    Archive

    Shear Strength and Stiffness Characterization of Lunar Simulant GRC-3

    Source: Journal of Aerospace Engineering:;2018:;Volume ( 031 ):;issue: 004
    Author:
    Dewoolkar Mandar M.;Edwards Michael;Walsh Dylan
    DOI: 10.1061/(ASCE)AS.1943-5525.0000848
    Publisher: American Society of Civil Engineers
    Abstract: Physical modeling experiments related to lunar in situ resource utilization activities use suitable soil simulants such as GRC-3. Only the index properties (e.g., specific gravity, particle size distribution, and maximum and minimum densities) compression indices, and shear strength parameters (peak angle of internal friction) of GRC-3 are currently available in the literature. In addition to the shear strength parameters, this work determined other important mechanical parameters such as critical state angle of internal friction, dilatancy angle, elastic modulus, and Poisson’s ratio using triaxial compression tests conducted at three different confining stresses of 25, 5, and 1 kPa. An additional set of triaxial specimens incorporated bender elements, which were used to determine small-strain shear wave velocity and shear modulus of GRC-3 at confining stresses ranging between 12.5 and 15 kPa. The confining stresses used in this work were lower than those used in other works on GRC-3 found in the literature. For extrapolating the behavior of terrestrial simulants to in situ surface lunar regolith, results obtained at smaller confining stresses are generally more relevant. The shear strength parameters of GRC-3 determined as part of this investigation compared well with those for GRC-3 and lunar regolith found in the literature, as well as lunar simulants GRC-1 and JSC-1A. Simple empirical correlations relating mechanical properties (angle of internal friction, dilatancy angle, elastic modulus, small-strain shear wave velocity, and maximum shear modulus) of GRC-3 as a function of its relative density or void ratio and confining stress are provided, so these properties can be readily estimated to support further analytical studies involving GRC-3.
    • Download: (1.619Mb)
    • Show Full MetaData Hide Full MetaData
    • Get RIS
    • Item Order
    • Go To Publisher
    • Statistics

      Shear Strength and Stiffness Characterization of Lunar Simulant GRC-3

    URI
    https://yetl.yabesh.ir/yetl1/handle/yetl/4247699
    Collections
    • Journal of Aerospace Engineering

    Show full item record

    contributor authorDewoolkar Mandar M.;Edwards Michael;Walsh Dylan
    date accessioned2019-02-26T07:32:17Z
    date available2019-02-26T07:32:17Z
    date issued2018
    identifier other%28ASCE%29AS.1943-5525.0000848.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4247699
    description abstractPhysical modeling experiments related to lunar in situ resource utilization activities use suitable soil simulants such as GRC-3. Only the index properties (e.g., specific gravity, particle size distribution, and maximum and minimum densities) compression indices, and shear strength parameters (peak angle of internal friction) of GRC-3 are currently available in the literature. In addition to the shear strength parameters, this work determined other important mechanical parameters such as critical state angle of internal friction, dilatancy angle, elastic modulus, and Poisson’s ratio using triaxial compression tests conducted at three different confining stresses of 25, 5, and 1 kPa. An additional set of triaxial specimens incorporated bender elements, which were used to determine small-strain shear wave velocity and shear modulus of GRC-3 at confining stresses ranging between 12.5 and 15 kPa. The confining stresses used in this work were lower than those used in other works on GRC-3 found in the literature. For extrapolating the behavior of terrestrial simulants to in situ surface lunar regolith, results obtained at smaller confining stresses are generally more relevant. The shear strength parameters of GRC-3 determined as part of this investigation compared well with those for GRC-3 and lunar regolith found in the literature, as well as lunar simulants GRC-1 and JSC-1A. Simple empirical correlations relating mechanical properties (angle of internal friction, dilatancy angle, elastic modulus, small-strain shear wave velocity, and maximum shear modulus) of GRC-3 as a function of its relative density or void ratio and confining stress are provided, so these properties can be readily estimated to support further analytical studies involving GRC-3.
    publisherAmerican Society of Civil Engineers
    titleShear Strength and Stiffness Characterization of Lunar Simulant GRC-3
    typeJournal Paper
    journal volume31
    journal issue4
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0000848
    page4018024
    treeJournal of Aerospace Engineering:;2018:;Volume ( 031 ):;issue: 004
    contenttypeFulltext
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian
     
    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian