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Behavior of compacted lunar simulants using new vacuum triaxial deviceThe objectives of this study are to create a lunar simulant locally from a basaltic rock and to design and develop a vacuum triaxial test device that can permit testing of compacted lunar simulant under cyclic loading with different levels of initial vacuum. Triaxial testing is performed in the device itself without removing the compacted specimen. Preliminary constrained compression and triaxial shear tests are performed to identify effects of initial confinements and vacuums. The results are used to define deformation and strength parameters. At this time, vacuum levels up to 0.0001 are possible. The research can aid in the development of compacted materials for various construction applications.
Document ID
19920073980
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Desai, Chandra S.
(NASA Headquarters Washington, DC United States)
Saadatmanesh, Hamid
(Arizona, University Tucson, United States)
Allen, Thomas
(Chem-Northern, Inc. Glenwood Springs, CO, United States)
Date Acquired
August 15, 2013
Publication Date
October 1, 1992
Publication Information
Publication: Journal of Aerospace Engineering
Volume: 5
Issue: 4, Oc
ISSN: 0893-1321
Subject Category
Lunar And Planetary Exploration
Accession Number
92A56604
Distribution Limits
Public
Copyright
Other

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