MODELLING THE PLASMA FLOW IN A HALL THRUSTER

机译：模拟霍尔通道中的等离子流

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A recently completed 1-D, macroscopic model of the plasma flow in a Hall thruster is here used to stand out that the solutions inside the thruster channel and in the external plume are always coupled and conditions at the channel exit can change significantly with thruster parameters and external conditions. In addition, preliminary results on a modified model which includes heat conduction are presented.

机译：霍尔推力器中等离子流的最新完成的一维宏观模型在这里用来表明，推力器通道内部和外部羽流中的溶液始终是耦合的，并且通道出口处的条件会随着推力器参数的变化而显着变化。和外部条件。此外，还提出了包含热传导的改进模型的初步结果。

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《7th Spacecraft Charging Technology Conference 2001: a Spacecraft Charging Odyssey, Apr 23-27, 2001, Noordwijk, the Netherlands》|2001年|p.539-544|共6页
会议地点 Noordwijk(NL)
作者
E. Ahedo; P. Martinez Cerezo; J.M. Gallardo; M. Martinez-Sanchez;
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作者单位

E. T.S.I. Aeronauticos, Univ. Politecnica, 28040 Madrid, Spain;

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会议组织
原文格式 PDF
正文语种 eng
中图分类航天（宇宙航行）;
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专利

1. Comment on "One-dimensional model of the plasma flow in a Hall thruster" [Phys. Plasmas 8, 3058 (2001)] [J] . Kundu M., Srinivasan R., Deshpande SP. Physics of plasmas . 2003,第4期

机译：评论“霍尔推力器中等离子体流的一维模型” Plasmas 8，3058（2001）]
2. Response to "Comment on 'One-dimensional model of the plasma flow in a Hall thruster' " [Phys. Plasmas 10, 1172 (2003)] [J] . Ahedo E., Martinez-Sanchez M. Physics of plasmas . 2003,第4期

机译：对“关于“霍尔推进器中等离子体流的一维模型”的评论”的回应Plasmas 10，1172（2003）]
3. One-dimensional model of the plasma flow in a Hall thruster [J] . Ahedo E., Martinez-Sanchez M., Martinez-Cerezo P. Physics of plasmas . 2001,第6期

机译：霍尔推力器中等离子体流的一维模型
4. MODELLING THE PLASMA FLOW IN A HALL THRUSTER [C] . E. Ahedo, P. Martinez Cerezo, J.M. Gallardo, Spacecraft charging technology conference . 2001

机译：在大厅推进器中建模等离子体流动
5. Enhancing Micro-Cathode Arc Thruster (muCAT) Plasma Generation to Analyze Magnetic Field Angle Effects on Sheath Formation in Hall Thrusters. [D] . Lukas, Joseph Nicholas. 2016

机译：增强微型阴极电弧推力器（muCAT）等离子体的产生，以分析磁场角度对霍尔推力器鞘层形成的影响。
6. Demonstrating a new technology for space debris removal using a bi-directional plasma thruster [O] . Kazunori Takahashi, Christine Charles, Rod W. Boswell, -1

机译：演示使用双向等离子推进器清除空间碎片的新技术
7. Plasma flow and plasma–wall transition in Hall thruster channel [O] . M. Keidar, I. D. Boyd, I. I. Beilis 2001

机译：霍尔推进器通道中的等离子体流动和等离子壁过渡
8. Performance Potential of Plasma Thrusters: Arcjet and Hall Thruster Modeling. [R] . Martinez-Sanchez, M. 1993

机译：等离子推进器的性能潜力：arcjet和Hall推进器建模。

MODELLING THE PLASMA FLOW IN A HALL THRUSTER

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