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Flowfield Structure and Acceleration Process in Quasi-Steady Magneto-Plasma-Dynamic (MPD) Arc Channels

Flowfield Structure and Acceleration Process in Quasi-Steady Magneto-Plasma-Dynamic (MPD) Arc Channels
准稳态磁等离子体动力 (MPD) 电弧通道中的流场结构和加速过程
批准号:
07651123
负责人:
TAHARA Hirokazu
金额:
$0.32万
依托单位:
依托单位国家:
日本
项目类别:
Grant-in-Aid for Scientific Research (C)
财政年份:
1995
资助国家:
日本
项目状态:
已结题
起止时间:
1995 至 1996

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中文摘要
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英文摘要
Plasma diagnostic measurement and flowfield analysis in quasisteady coaxial magnetoplasmadynamic (MPD) channels were made to understand blowing acceleration, i.e., one-dimensional flowfield. For Ar, measured current fractions on the anode intensively increased near the inlet. However, current fractions on the cathode gradually increased downstream, and current slightly concentrated near the inlet at high magnetic Reynolds numbers. The electron temperatures were axially kept about 1.0 eV and slightly increased near the inlet and the outlet. The electron number densities increased near the exit, and the characteristics correspond to the current distributions. The experimental results agreed roughly with analyzed ones. Accordingly, it is expected from the axial profile of Lorentz forces inferred from the measured physical properties and the calculated plasma velocities that there are two acceleration zones near the inlet and the outlet. Furthermore, it is predicted from the numerical analysis that the acceleration caused by ionization process is dominant near the inlet.
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DOI: --
发表时间:
期刊:
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作者: []
通讯作者:
Kazunori Mitsuo et al.: "Arc Structure in a Quasi-Steady MPD Channel" Proc.20th Int.Symp.Space Technol.and Sci.Vol.1. 158-165 (1996)
Kazunori Mitsuo 等人:“准稳态 MPD 通道中的弧结构”Proc.20th Int.Symp.Space Technol.and Sci.Vol.1。
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发表时间:
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通讯作者:
Hirokazu Tahara: "Plasma Features in Quasisteady MPD Chonnels" 24th Int. Electric Propulsion Cont.,Moscow. 95-116. 1-9 (1995)
Hirokazu Tahara:“准稳态 MPD 通道中的等离子体特征”第 24 届 Int。
DOI: --
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通讯作者:
Takashi Yonezawa et al.: "Spectroscopic Measurement and Numerical Analysis of Thermal Non-Equilibrium Flow in a 10-kW-Class Arcjet Thruster" Proc.20th Int.Symp.Space Technol.and Sci.Vol.1. 102-108 (1996)
Takashi Yonezawa 等人:“10 kW 级电弧喷射推进器中热非平衡流的光谱测量和数值分析”Proc.20th Int.Symp.Space Technol.and Sci.Vol.1。
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通讯作者:
15
    Development of High-Performance, Long-Lifetime and High-Power Magneto-Plasma-Dynamic Thrusters for In-Space Exploration
    • 批准号:
      17H03484
    • 项目类别:
      Grant-in-Aid for Scientific Research (B)
    • 资助金额:
      $10.48万
    • 财政年份:
      2017
    • 负责人:
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    • 依托单位:
    Research on Low-Temperature Material Processings Using Supersonic Plasma Jets
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      23656543
    • 项目类别:
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    • 资助金额:
      $2.33万
    • 财政年份:
      2011
    • 负责人:
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    • 依托单位:
    RESEARCH AND DEVELOPMENT OF HIGH-SPECIFIC-IMPULSE AND LONG-LIFETIME HALL THRUSTERS
    • 批准号:
      22360360
    • 项目类别:
      Grant-in-Aid for Scientific Research (B)
    • 资助金额:
      $11.4万
    • 财政年份:
      2010
    • 负责人:
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    • 依托单位:
    RESEARCH ON ENHANCEMENT OF IMPULSE FOR ELECTROTHERMAL PULSED PLASMA THRUSTERS ONBOARD SMALL SATELLITES
    • 批准号:
      19360382
    • 项目类别:
      Grant-in-Aid for Scientific Research (B)
    • 资助金额:
      $12.23万
    • 财政年份:
      2007
    • 负责人:
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    • 依托单位:
    海外基金