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    Mechanical Equipment Requirements for Inflatable Lunar Structures

    Source: Journal of Aerospace Engineering:;1992:;Volume ( 005 ):;issue: 002
    Author:
    James M. Hines
    ,
    Craig E. Miller
    ,
    Richard M. Drake
    DOI: 10.1061/(ASCE)0893-1321(1992)5:2(248)
    Publisher: American Society of Civil Engineers
    Abstract: Inflatable 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.
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      Mechanical Equipment Requirements for Inflatable Lunar Structures

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/44734
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    • Journal of Aerospace Engineering

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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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