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Development and test of a permanent magnet helicon thruster.

机译:永磁螺旋推进器的开发和测试。

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摘要

This thesis describes the development of a test facility equipped with Langmuir probe and Retarding Potential Analyzer diagnostics for helicon thruster research. A helicon thruster using permanent magnets was also designed and tested. The helicon has several advantages, but the main disadvantage is the use of electromagnets to generate the required magnetic field, requiring a high power draw. The choice of using permanent magnets is to reduce the size, cost and power required to generate high specific impulse thrust. A prototype has been designed, analyzed and tested using Argon with demonstrated specific impulse of 1400 seconds. Analysis of the variation of beam power and ion temperature in the exhaust plume with variation of input power and vacuum pressure are presented. Preliminary tests were conducted using water as a propellant. Measurement of the ion energy distribution function shows a number of peaks indicating the presence of dissociation products.
机译:本文介绍了配备用于直升机推进器研究的配备Langmuir探针和减速电位分析器诊断程序的测试设备的开发。还设计并测试了使用永磁体的螺旋推进器。螺线管有几个优点,但主要缺点是使用电磁体产生所需的磁场,需要大功率消耗。选择使用永磁体是为了减小产生高比冲推力所需的尺寸,成本和功率。已经使用Argon设计,分析和测试了原型,并证明了1400秒的特定脉冲。提出了随着输入功率和真空压力的变化分析束流功率和废气羽流中离子温度的变化。使用水作为推进剂进行了初步测试。离子能量分布函数的测量显示出许多峰,表明存在离解产物。

著录项

  • 作者

    DeMaio, Michael Frank, Jr.;

  • 作者单位

    University of Maryland, College Park.;

  • 授予单位 University of Maryland, College Park.;
  • 学科 Engineering Aerospace.
  • 学位 M.S.
  • 年度 2010
  • 页码 118 p.
  • 总页数 118
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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