...
首页> 外文期刊>Acta astronautica >RF Helicon-based Inductive Plasma Thruster (IPT) Design for an Atmosphere-Breathing Electric Propulsion system (ABEP)
【24h】

RF Helicon-based Inductive Plasma Thruster (IPT) Design for an Atmosphere-Breathing Electric Propulsion system (ABEP)

机译:基于RF直升光的电感等离子体推进器(IPT)设计用于气氛呼吸电动推进系统(ABEP)

获取原文
获取原文并翻译 | 示例
   

获取外文期刊封面封底 >>

       

摘要

Challenging space missions include those at very low altitudes, where the atmosphere is source of aerodynamic drag on the spacecraft. To extend such missions lifetime, an efficient propulsion system is required. One solution is Atmosphere-Breathing Electric Propulsion (ABEP). It collects atmospheric particles to be used as propellant for an electric thruster. The system would minimize the requirement of limited propellant availability and can also be applied to any planet with atmosphere, enabling new mission at low altitude ranges for longer times. Challenging is also the presence of reactive chemical species, such as atomic oxygen in Earth orbit. Such species cause erosion of (not only) propulsion system components, i.e. acceleration grids, electrodes, and discharge channels of conventional EP systems. IRS is developing within the DISCOVERER project, an intake and a thruster for an ABEP system. The paper describes the design and implementation of the RF helicon-based inductive plasma thruster (IPT). This paper deals in particular with the design and implementation of a novel antenna called the birdcage antenna, a device well known in magnetic resonance imaging (MRI), and also lately employed for helicon-wave based plasma sources in fusion research. This is aided by the numerical tool XFdtd (R). The IPT is based on RF electrodeless operation aided by an externally applied static magnetic field. The IPT is composed by an antenna, a discharge channel, a movable injector, and a solenoid. By changing the operational parameters along with the novel antenna design, the aim is to minimize losses in the RF circuit, and accelerate a quasi-neutral plasma plume. This is also to be aided by the formation of helicon waves within the plasma that are to improve the overall efficiency and achieve higher exhaust velocities. Finally, the designed IPT with a particular focus on the birdcage antenna design procedure is presented.
机译:具有挑战性的空间任务包括非常低的海拔地区的空间,大气是航天器上的空气动力学拖曳的来源。为了延长这样的任务寿命,需要一个有效的推进系统。一种解决方案是呼吸电动推进(ABEP)。它收集大气颗粒用作电推进器的推进剂。该系统将最大限度地减少有限推进剂可用性的要求,也可以应用于任何带有大气的行星,在低海拔地区实现新的任务,更长的时间。挑战性也是反应性化学物质的存在,如地球轨道中的原子氧。这些物种导致(不仅)推进系统组件的侵蚀,即传统EP系统的加速网格,电极和放电通道。美国国税局正在发现项目中开发,ABEP系统的摄入量,摄入和推进器。本文介绍了基于RF Helicon的电感等离子体推进器(IPT)的设计和实现。本文特别涉及一种名为鸟笼天线的新型天线的设计和实施,该装置在磁共振成像(MRI)中众所周知的装置,并且还可以用于融合研究中的Helicon-Waiv基等离子体源。这是由数值工具XFDTD(R)辅助的。 IPT基于由外部施加的静态磁场辅助的RF无电极操作。 IPT由天线,排出通道,可移动注射器和螺线管组成。通过改变操作参数以及新颖的天线设计,目的是最小化RF电路中的损耗,并加速准中性等离子体羽流。这也是通过在等离子体内形成Helicon波的形成,这是提高整体效率并实现更高的排气速度。最后,提出了设计的IPT,特别关注鸟笼天线设计程序。

著录项

  • 来源
    《Acta astronautica》 |2020年第11期|476-483|共8页
  • 作者单位

    Univ Stuttgart Inst Space Syst IRS D-70569 Stuttgart Germany;

    Univ Stuttgart Inst Space Syst IRS D-70569 Stuttgart Germany;

    Univ Stuttgart Inst Space Syst IRS D-70569 Stuttgart Germany;

    Univ Stuttgart Inst Space Syst IRS D-70569 Stuttgart Germany;

    Univ Stuttgart Inst Space Syst IRS D-70569 Stuttgart Germany;

    Univ Manchester George Begg Bldg Sackville St Manchester M13 9PL Lancs England;

    Univ Manchester George Begg Bldg Sackville St Manchester M13 9PL Lancs England;

    Univ Manchester George Begg Bldg Sackville St Manchester M13 9PL Lancs England;

    Univ Manchester George Begg Bldg Sackville St Manchester M13 9PL Lancs England;

    Univ Manchester George Begg Bldg Sackville St Manchester M13 9PL Lancs England;

    Univ Manchester George Begg Bldg Sackville St Manchester M13 9PL Lancs England;

    Univ Manchester George Begg Bldg Sackville St Manchester M13 9PL Lancs England;

    Univ Manchester George Begg Bldg Sackville St Manchester M13 9PL Lancs England;

    Univ Manchester George Begg Bldg Sackville St Manchester M13 9PL Lancs England;

    Univ Manchester George Begg Bldg Sackville St Manchester M13 9PL Lancs England;

    Univ Manchester George Begg Bldg Sackville St Manchester M13 9PL Lancs England;

    Elecnor Deimos Satellite Syst C Francia 9 Puertollano 13500 Spain;

    Elecnor Deimos Satellite Syst C Francia 9 Puertollano 13500 Spain;

    Elecnor Deimos Satellite Syst C Francia 9 Puertollano 13500 Spain;

    Elecnor Deimos Satellite Syst C Francia 9 Puertollano 13500 Spain;

    Elecnor Deimos Satellite Syst C Francia 9 Puertollano 13500 Spain;

    GomSpace AS Langagervej 6 DK-9220 Aalborg Denmark;

    GomSpace AS Langagervej 6 DK-9220 Aalborg Denmark;

    GomSpace AS Langagervej 6 DK-9220 Aalborg Denmark;

    GomSpace AS Langagervej 6 DK-9220 Aalborg Denmark;

    UPC BarcelonaTECH Colom 11 TR5 Terrassa 08222 Spain;

    UPC BarcelonaTECH Colom 11 TR5 Terrassa 08222 Spain;

    UPC BarcelonaTECH Colom 11 TR5 Terrassa 08222 Spain;

    Univ Coll London Holnibury St Mary Mullard Space Sci Lab Dorking RH5 6NT Surrey England;

    Christopher Newport Univ Newport News VA 23606 USA;

    Euroconsult 86 Blvd Sebastopol Paris France;

    Euroconsult 86 Blvd Sebastopol Paris France;

    Euroconsult 86 Blvd Sebastopol Paris France;

    Euroconsult 86 Blvd Sebastopol Paris France;

    Concentris Res Management Gmbh Ludwigstr 4 D-82256 Furstenfeldbruck Germany;

    Concentris Res Management Gmbh Ludwigstr 4 D-82256 Furstenfeldbruck Germany;

  • 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

    ABEP; IPT; VLEO; Helicon; Birdcage;

    机译:abep;ipt;vleo;helicon;鸟笼;

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号