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contributor authorJames M. Hines
contributor authorCraig E. Miller
contributor authorRichard M. Drake
date accessioned2017-05-08T21:15:42Z
date available2017-05-08T21:15:42Z
date copyrightApril 1992
date issued1992
identifier other%28asce%290893-1321%281992%295%3A2%28248%29.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/44734
description abstractInflatable structures have been proposed by a number of authors. Several structural forms have been conceptually designed, including spherical, pillow‐shaped, semicylindrical, and domed saucer. Regardless of structural form, all inflatables require mechanical equipment to initiate and maintain inflation. This paper identifies the mechanical equipment and operations required to support an inflatable structure. A previously proposed semicylindrical structure is selected for this study, but the principal results are applicable to all inflatable structures. The results indicate that air for inflatable structures should be transported to the moon in a liquid (cryogenic) state. The liquefied air can be evaporated and heated to the proper temperature using solar energy and a conventional pumping system. Removing the air from the facility is an entirely different problem and requires different equipment. There are two alternatives: (1) Discharge the air to the moon; and (2) reclaim the air for reuse. The first alternative is not likely to be cost‐effective and might well be scientifically unacceptable. The second alternative presents numerous technical problems but appears technically feasible.
publisherAmerican Society of Civil Engineers
titleMechanical Equipment Requirements for Inflatable Lunar Structures
typeJournal Paper
journal volume5
journal issue2
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)0893-1321(1992)5:2(248)
treeJournal of Aerospace Engineering:;1992:;Volume ( 005 ):;issue: 002
contenttypeFulltext


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