Plasma Flow Structure of Direct-Current Arcjet Thrusters and Its Spacecraft Interaction Research

直流电弧喷射推进器等离子流结构及其与航天器相互作用研究

基本信息

  • 批准号:
    13450398
  • 负责人:
  • 金额:
    $ 8.45万
  • 依托单位:
  • 依托单位国家:
    日本
  • 项目类别:
    Grant-in-Aid for Scientific Research (B)
  • 财政年份:
    2001
  • 资助国家:
    日本
  • 起止时间:
    2001 至 2002
  • 项目状态:
    已结题

项目摘要

Spectroscopic and electrostatic probe measurements were made to examine plasma characteristics with or without a titanium plate for a 10-kW-class direct-current arcjet thruster. Heat fluxes into the plate from the plasma were also evaluated with a Nickel slug and thermocouple arrangement. Ammonia and mixtures of nitrogen and hydrogen were used as a working gas. The NH_3 and N\2+3H_2 plasmas in the nozzle and in the downstream plume without a substrate plate were in thermodynamical nonequilibrium states. As a result, the H-atom electronic excitation temperature and the N_2 molecule-rotational excitation temperature intensively decreased downstream in the nozzle although the NH molecule-rotational excitation temperature did not show an axial decrease. Each temperature was kept in a small range in the plume without a substrate plate except for the NH rotational temperature for NH_3 working gas. On the other hand, as approaching the titanium plate, the thermodynamical nonequilibrium plasma came to be a temperature-equilibrium one because the plasma flow tended to stagnate in front of the plate. The electron temperature had a small radial variation near the plate. Both the electron number density and the heat flux decreased radially outward, and an increase in H_2 mole fraction raised them at a constant radial position. In cases with NH_3 and N_2+3H_2, a radical of NH with a radially wide distribution was considered to contribute to the better nitriding as a chemically active and non heating process.
进行了光谱和静电探针测量,以检查有或没有钛板的血浆特性,用于10 kW级的直流电流推进器。还通过镍弹和热电偶排列评估了从血浆中进入板的热通量。氮和氢的氨和混合物用作工作气体。喷嘴中的NH_3和N \ 2+2+3H_2等离子体在没有底物板的情况下以热力学非平衡状态处。结果,尽管NH分子 - 旋转激发温度没有显示出轴向降低,但在喷嘴中的H原子电子激发温度和N_2分子激发温度强烈降低。除了NH_3工作气体的NH旋转温度外,每个温度都保持在没有基板板的羽流中。另一方面,随着接近钛板的接近,热力学非平衡等离子体成为温度平衡的血浆,因为血浆流量倾向于停滞在板前。电子温度在板附近的径向变化很小。电子数密度和热通量都在径向向外降低,而H_2摩尔分数的增加使它们在恒定的径向位置上升高。在使用NH_3和N_2+3H_2的情况下,具有径向宽分布的NH的自由基被认为有助于更好的硝化作用作为化学活性和非加热过程。

项目成果

期刊论文数量(54)
专著数量(0)
科研奖励数量(0)
会议论文数量(0)
专利数量(0)
Hirokazu Tahara et al.: "Exhaust Plume Characteristics of Quasi-Steady MPD Thrusters"27th Int. Electric Propulsion Conf.. 1-9 (1999)
Hirokazu Tahara 等人:“准稳态 MPD 推进器的排气羽流特性”27th Int.
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Hirokazu Tahara et al.: "Near Substrate Plasma Characteristics of a Supersonic Ammonia and Nitrogen/Hydrogen-Mixture DC Plasma Jet for Nitriding under a Low Pressure Environment"Proc. 15th Int. Symp. Plasma Chemistry. 1. 205-210 (2001)
Hirokazu Tahara 等人:“低压环境下用于氮化的超音速氨和氮/氢混合直流等离子体射流的近基底等离子体特性”Proc。
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Hirokazu Tahara et al.: "Material Spraying Using Electromagnetically Accelerated Plasma"Jpn. J. Appl. Phys.. in press. (2002)
Hirokazu Tahara 等人:“使用电磁加速等离子体的材料喷涂”Jpn。
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Hirokazu Tahara et al.: "Plasma and Heat Flux Characteristics of a Supersonic Ammonia or Nitrogen/Hydrogen-Mixture DC Plasma Jet"IEEE Trans. Plasma Science. 4(印刷中). (2003)
Hirokazu Tahara 等人:“超音速氨或氮/氢混合直流等离子体射流的等离子体和热通量特性”IEEE Trans 4(出版中)。
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    0
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Hirokazu Tahara et al.: "Material Spraying Llsiing Electromagnetically Accelerated Plasma"Japanese Journal of Appl.Phys.. 4(印刷中). (2003)
Hirokazu Tahara 等人:“电磁加速等离子体材料喷射”,日本应用物理学杂志 4(印刷中)。
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TAHARA Hirokazu其他文献

TAHARA Hirokazu的其他文献

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{{ truncateString('TAHARA Hirokazu', 18)}}的其他基金

Development of High-Performance, Long-Lifetime and High-Power Magneto-Plasma-Dynamic Thrusters for In-Space Exploration
开发用于太空探索的高性能、长寿命和高功率磁等离子体动力推进器
  • 批准号:
    17H03484
  • 财政年份:
    2017
  • 资助金额:
    $ 8.45万
  • 项目类别:
    Grant-in-Aid for Scientific Research (B)
Research on Low-Temperature Material Processings Using Supersonic Plasma Jets
超音速等离子射流低温材料加工研究
  • 批准号:
    23656543
  • 财政年份:
    2011
  • 资助金额:
    $ 8.45万
  • 项目类别:
    Grant-in-Aid for Challenging Exploratory Research
RESEARCH AND DEVELOPMENT OF HIGH-SPECIFIC-IMPULSE AND LONG-LIFETIME HALL THRUSTERS
高比冲长寿命霍尔推进器的研发
  • 批准号:
    22360360
  • 财政年份:
    2010
  • 资助金额:
    $ 8.45万
  • 项目类别:
    Grant-in-Aid for Scientific Research (B)
RESEARCH ON ENHANCEMENT OF IMPULSE FOR ELECTROTHERMAL PULSED PLASMA THRUSTERS ONBOARD SMALL SATELLITES
小卫星电热脉冲等离子体推进器脉冲增强研究
  • 批准号:
    19360382
  • 财政年份:
    2007
  • 资助金额:
    $ 8.45万
  • 项目类别:
    Grant-in-Aid for Scientific Research (B)
RESEARCH AND DEVELOPMENT OF LOW-POWER HALL THRUSTERS WITH CIRCULAR-CROSS-SECTIONAL DISCHARGE CHAMBER, AND ITS INNER PHYSICAL PROCESSES
圆形断面放电室小功率霍尔推进器及其内部物理过程的研制
  • 批准号:
    16360420
  • 财政年份:
    2004
  • 资助金额:
    $ 8.45万
  • 项目类别:
    Grant-in-Aid for Scientific Research (B)
Research and Development of Ground Simulation Methods for Spacecraft Environment, and Degradation Experiments of Spacecraft Materials
航天器环境地面模拟方法研究与进展及航天器材料降解实验
  • 批准号:
    09555301
  • 财政年份:
    1997
  • 资助金额:
    $ 8.45万
  • 项目类别:
    Grant-in-Aid for Scientific Research (B)
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
  • 财政年份:
    1995
  • 资助金额:
    $ 8.45万
  • 项目类别:
    Grant-in-Aid for Scientific Research (C)

相似国自然基金

太空化学激光推进中等离子体时空演化特性及能量转化机理研究
  • 批准号:
    11905223
  • 批准年份:
    2019
  • 资助金额:
    26.0 万元
  • 项目类别:
    青年科学基金项目

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SBIR Phase I: A Fully Electric Space Vehicle Propulsion Engine
SBIR 第一阶段:全电动航天器推进发动机
  • 批准号:
    2318600
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    2023
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Study on Space Propulsion with a Low Toxicity ADN-Based Monopropellant
低毒ADN基单组元推进剂空间推进研究
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    19K21074
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Research on Reaction Promotion of Green Propellant by Pulsed Electric Discharge for Space Propulsion
空间推进脉冲放电绿色推进剂反应促进研究
  • 批准号:
    17K14875
  • 财政年份:
    2017
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    $ 8.45万
  • 项目类别:
    Grant-in-Aid for Young Scientists (B)
RESEARCH AND DEVELOPMENT OF LOW-POWER HALL THRUSTERS WITH CIRCULAR-CROSS-SECTIONAL DISCHARGE CHAMBER, AND ITS INNER PHYSICAL PROCESSES
圆形断面放电室小功率霍尔推进器及其内部物理过程的研制
  • 批准号:
    16360420
  • 财政年份:
    2004
  • 资助金额:
    $ 8.45万
  • 项目类别:
    Grant-in-Aid for Scientific Research (B)
Ion heating in a fast-flowing plasma for applying an advanced space propulsion
快速流动等离子体中的离子加热用于应用先进的空间推进
  • 批准号:
    15340196
  • 财政年份:
    2003
  • 资助金额:
    $ 8.45万
  • 项目类别:
    Grant-in-Aid for Scientific Research (B)
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