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Development of hall thruster propulsion system for STSAT-3 application

机译:STSAT-3应用的霍尔推进器推进系统的开发

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摘要

Science and technology satellite-3 (STSAT-3) is being developed and is scheduled for launch in 2011. One of the primary objectives of its mission is to verify the performance of a hall thruster propulsion system (HPS) that uses xenon gas. According to its major functions, the HPS can be divided into several sub-modules. This paper presents the development and qualification of the hall effect thruster propulsion subsystem that includes a xenon feed system (XFS). The xenon feed system regulates the pressure down from the xenon propellant tank and supplies the xenon flows to the anode and cathode. The technology and xenon feed system developed for the STSAT-3 spacecraft will also be applicable to a variety of future electronic propulsion systems and micro-satellites. Details related to the overall development and performance results of the HPS are presented in this paper.
机译:正在研发3号科技卫星(STSAT-3),计划于2011年发射。其任务的主要目标之一是验证使用氙气的霍尔推进器推进系统(HPS)的性能。根据其主要功能,HPS可以分为几个子模块。本文介绍了包括氙气供料系统(XFS)的霍尔效应推进器推进子系统的开发和鉴定。氙气进料系统可调节来自氙气推进剂罐的压力,并将氙气流提供给阳极和阴极。为STSAT-3航天器开发的技术和氙气馈送系统也将适用于各种未来的电子推进系统和微卫星。本文介绍了有关HPS总体开发和性能结果的详细信息。

著录项

  • 来源
    《Acta astronautica》 |2012年第maraaapra期|p.90-97|共8页
  • 作者

    H.K. Cho; J. Rhee;

  • 作者单位

    Andong National University, 1375 Cyeongdong-ro, Andong-si, Gyeongsangbuk-do 760-749, Republic of Korea;

    Korea Aerospace Research Institute, 115 Gwahakro, Yuseong-gu, Daejeon 305-333, Republic of Korea;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    xenon feed system; hall thruster; satellite;

    机译:氙气进料系统;霍尔推力器卫星;
  • 入库时间 2022-08-18 02:34:16

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