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contributor authorA. Smith
date accessioned2017-05-08T23:40:13Z
date available2017-05-08T23:40:13Z
date copyrightJune, 1993
date issued1993
identifier issn0003-6900
identifier otherAMREAD-25646#268_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/111260
description abstractThe construction of a lunar base has been thought about for almost five decades. The earliest concepts dealt with size and shape concepts rather than actual design of structures and equipment. As the exploration of space has received emphasis in more recent times, the need to consider the factors of design and design approaches have received more attention. It still is not possible to completely rationalize the design of a habitat, for example, but we are now very aware of the need to include the fracture and fatigue properties of the materials of which the hardware of a lunar infrastructure is constructed. It is reasonably certain that the same techniques used for terrestrial designs can be used for lunar bases provided the space environment is taken into account. The extensive amount of research on fracture and fatigue that has been and is being conducted, along with the ease and speed of computation of their effects on alternative design features will be invaluable in providing a highly reliable, safe lunar base.
publisherThe American Society of Mechanical Engineers (ASME)
titleMechanics of Materials in Lunar Base Design
typeJournal Paper
journal volume46
journal issue6
journal titleApplied Mechanics Reviews
identifier doi10.1115/1.3120354
journal fristpage268
journal lastpage271
identifier eissn0003-6900
keywordsDesign
keywordsFracture (Process)
keywordsComputation
keywordsShapes
keywordsFatigue properties
keywordsFatigue
keywordsConstruction AND Hardware
treeApplied Mechanics Reviews:;1993:;volume( 046 ):;issue: 006
contenttypeFulltext


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