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首页> 外文期刊>Plasma Sources Science & Technology >Performance characterization of a low-power magnetically shielded Hall thruster with an internally-mounted hollow cathode
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Performance characterization of a low-power magnetically shielded Hall thruster with an internally-mounted hollow cathode

机译:具有内部安装空心阴极的低功耗磁屏蔽霍尔推进器的性能表征

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摘要

Magnetically shielded miniature (MaSMi) is a low power (?1 kW) long life (>100 kg Xe throughput) magnetically shielded Hall thruster that features an internally mounted hollow cathode. The development model MaSMi Hall thruster was designed, fabricated, and tested in preparation for advancement into an engineering model design. The MaSMi-DM uses an ultracompact internally-mounted heaterless hollow cathode, which has previously demonstrated stable operation over a discharge current range of 0.5–4 A. More than 100 heaterless ignitions were performed during this test campaign, revealing consistent and predictable start-up behavior. Component testing of a novel anode manifold used in the MaSMi-DM demonstrated peak-topeak azimuthal propellant flow distribution variations of less than 3.2% across three flow rates and two anodes. Current–voltage-magnetic field testing of the MaSMi-DM was completed over a discharge voltage range of 200–600 V, a discharge current range of 0.5–4.0 A, and a discharge power range of 150–1000 W. The MaSMi-DM demonstrated the highest total efficiency and highest total specific impulse of any sub-kW Hall thruster to date. Performance highlights include a peak thrust of 68.6 mN, a peak total specific impulse of 1940 s at 1000W with >1500 s available above 500 W, and a peak total efficiency of 54.2% at 1000W with >40% available above 300 W. Visual observations of the plasma discharge, carbon-coated discharge channel walls post-operation, and the results from plasma simulations provided strong evidence of magnetic shielding and the projected >100 kg Xe throughput capability of the thruster.
机译:磁屏蔽的微型(MASMI)是低功率(?1 kW)长寿命(> 100千克XE吞吐量)磁屏蔽霍尔推进器,其具有内部安装的空心阴极。设计,制造和测试了开发模型MASMI Hall推进器,以准备进入工程模型设计。 MASMI-DM使用超自联内部安装的可加工中空阴极,前面已经在0.5-4 A的放电电流范围内显示出稳定的操作。在此测试活动期间进行了超过100个可用点火,揭示一致和可预测的启动行为。在MASMI-DM中使用的新型阳极歧管的组件测试在三个流速和两个阳极上显示出峰值顶辐射的推进剂流量分布变化小于3.2%。 MASMI-DM的电流电压 - 磁场测试在200-600 V的放电电压范围内完成,放电电流范围为0.5-4.0a,放电功率范围为150-1000W .MASMI-DM迄今为止展示了任何子千瓦霍尔推进器的最高总效率和最高特定脉冲。性能亮点包括68.6mn的峰值推力,1940秒的峰值总特定脉冲在1000w以上的1000w,高于500W的峰值,峰值总效率为1000W,> 40%以上可用300 W.视觉观测在等离子体放电,碳涂覆的排出通道壁后操作,并且等离子体模拟的结果提供了强大的磁屏蔽证据和推进器的投影> 100kg XE吞吐量能力。

著录项

  • 来源
    《Plasma Sources Science & Technology》 |2019年第10期|共14页
  • 作者单位

    Electric Propulsion Group Jet Propulsion Laboratory California Institute of Technology Pasadena CA 91109 United States of America;

    Electric Propulsion Group Jet Propulsion Laboratory California Institute of Technology Pasadena CA 91109 United States of America;

    Electric Propulsion Group Jet Propulsion Laboratory California Institute of Technology Pasadena CA 91109 United States of America;

    Electric Propulsion Group Jet Propulsion Laboratory California Institute of Technology Pasadena CA 91109 United States of America;

    Electric Propulsion Group Jet Propulsion Laboratory California Institute of Technology Pasadena CA 91109 United States of America;

    Electric Propulsion Group Jet Propulsion Laboratory California Institute of Technology Pasadena CA 91109 United States of America;

  • 收录信息
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 等离子体物理学;
  • 关键词

    Hall thruster; low power; magnetic shielding;

    机译:霍尔推进器;低功率;磁屏蔽;

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