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    Development of Ionic Wind Pump Used in Martian Environment

    Source: Journal of Aerospace Engineering:;2021:;Volume ( 034 ):;issue: 005::page 04021050-1
    Author:
    Hiroyuki Kawamoto
    ,
    Ryo Ichikawa
    DOI: 10.1061/(ASCE)AS.1943-5525.0001308
    Publisher: ASCE
    Abstract: An ionic wind pump consisting of simple concentric cylinders was developed for future Mars exploration. The ionic wind pump uses gas flow driven by the corona discharge generated at the edge of the inner cylinder electrode. It is suitable for applications such as air circulation in a module and heat transfer of equipment. The relationships between the applied voltage and the corona current, generated gas flow rate, and pressure rise were measured with reduced pressure of air and carbon dioxide gas that simulated the Mars environment. A substantial gas flow was generated at atmospheric pressure, but the pressure rise was less at low pressure. The performance was improved by adopting a multistage configuration. Some effective methods to measure gas velocity in a low-pressure environment were also developed. Numerical calculations were performed for the corona discharge field and the ionic wind induced by the migration of ions generated by the corona discharge. The experimental results agreed well with the numerical calculations. The pump can be effectively applied for Mars exploration because it is extremely simple, consumes less power, and has no mechanical moving parts.
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      Development of Ionic Wind Pump Used in Martian Environment

    URI
    http://yetl.yabesh.ir/yetl1/handle/yetl/4269769
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    contributor authorHiroyuki Kawamoto
    contributor authorRyo Ichikawa
    date accessioned2022-01-31T23:27:55Z
    date available2022-01-31T23:27:55Z
    date issued9/1/2021
    identifier other%28ASCE%29AS.1943-5525.0001308.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4269769
    description abstractAn ionic wind pump consisting of simple concentric cylinders was developed for future Mars exploration. The ionic wind pump uses gas flow driven by the corona discharge generated at the edge of the inner cylinder electrode. It is suitable for applications such as air circulation in a module and heat transfer of equipment. The relationships between the applied voltage and the corona current, generated gas flow rate, and pressure rise were measured with reduced pressure of air and carbon dioxide gas that simulated the Mars environment. A substantial gas flow was generated at atmospheric pressure, but the pressure rise was less at low pressure. The performance was improved by adopting a multistage configuration. Some effective methods to measure gas velocity in a low-pressure environment were also developed. Numerical calculations were performed for the corona discharge field and the ionic wind induced by the migration of ions generated by the corona discharge. The experimental results agreed well with the numerical calculations. The pump can be effectively applied for Mars exploration because it is extremely simple, consumes less power, and has no mechanical moving parts.
    publisherASCE
    titleDevelopment of Ionic Wind Pump Used in Martian Environment
    typeJournal Paper
    journal volume34
    journal issue5
    journal titleJournal of Aerospace Engineering
    identifier doi10.1061/(ASCE)AS.1943-5525.0001308
    journal fristpage04021050-1
    journal lastpage04021050-6
    page6
    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
    yabeshDSpacePersian