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    Performance-Based Engineering Framework to Quantify Micrometeoroid Damage to Lunar Surface Structures

    Source: Journal of Aerospace Engineering:;2021:;Volume ( 034 ):;issue: 005::page 04021055-1
    Author:
    Maria I. Allende
    ,
    Anne S. Kiremidjian
    ,
    Michael D. Lepech
    ,
    David J. Loftus
    DOI: 10.1061/(ASCE)AS.1943-5525.0001300
    Publisher: ASCE
    Abstract: Extended-duration missions to the Moon require the construction of long-term infrastructure that protects inhabitants and protects life-support systems from the Moon’s hazardous environment. Notable hazards of the lunar environment include ionizing radiation, extreme thermal cycles, and hypervelocity micrometeoroid impacts. Of these hazards, micrometeoroids are a top research priority because they are stochastic in nature and arrive without warning. To design structures that will be impacted by randomly distributed micrometeoroids, a risk-based approach should be used. This paper describes the development of a risk-based design framework termed performance-based impact engineering. This proposed framework allows the risk of micrometeoroid impact to be considered in the design of lunar infrastructure by developing site-specific hazard models and material-specific damage models. The methodologies for micrometeoroid hazard estimation on the lunar surface and material damage prediction are described. A case study for the design of a tiled lunar landing pad using the performance-based impact engineering framework is demonstrated.
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      Performance-Based Engineering Framework to Quantify Micrometeoroid Damage to Lunar Surface Structures

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    http://yetl.yabesh.ir/yetl1/handle/yetl/4269747
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    contributor authorMaria I. Allende
    contributor authorAnne S. Kiremidjian
    contributor authorMichael D. Lepech
    contributor authorDavid J. Loftus
    date accessioned2022-01-31T23:27:17Z
    date available2022-01-31T23:27:17Z
    date issued9/1/2021
    identifier other%28ASCE%29AS.1943-5525.0001300.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4269747
    description abstractExtended-duration missions to the Moon require the construction of long-term infrastructure that protects inhabitants and protects life-support systems from the Moon’s hazardous environment. Notable hazards of the lunar environment include ionizing radiation, extreme thermal cycles, and hypervelocity micrometeoroid impacts. Of these hazards, micrometeoroids are a top research priority because they are stochastic in nature and arrive without warning. To design structures that will be impacted by randomly distributed micrometeoroids, a risk-based approach should be used. This paper describes the development of a risk-based design framework termed performance-based impact engineering. This proposed framework allows the risk of micrometeoroid impact to be considered in the design of lunar infrastructure by developing site-specific hazard models and material-specific damage models. The methodologies for micrometeoroid hazard estimation on the lunar surface and material damage prediction are described. A case study for the design of a tiled lunar landing pad using the performance-based impact engineering framework is demonstrated.
    publisherASCE
    titlePerformance-Based Engineering Framework to Quantify Micrometeoroid Damage to Lunar Surface Structures
    typeJournal Paper
    journal volume34
    journal issue5
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0001300
    journal fristpage04021055-1
    journal lastpage04021055-9
    page9
    treeJournal of Aerospace Engineering:;2021:;Volume ( 034 ):;issue: 005
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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