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    • 13. 发明申请
    • MICRO-CATHODE THRUSTER AND A METHOD OF INCREASING THRUST OUTPUT FOR A MICRO-CATHODE THRUSTER
    • 微控制器THRUSTER和增加微控制器THRUS输出的方法
    • US20110258981A1
    • 2011-10-27
    • US13081106
    • 2011-04-06
    • Michael KEIDARAlexey SHASHURINTaisen ZHUANG
    • Michael KEIDARAlexey SHASHURINTaisen ZHUANG
    • B64G1/40
    • B64G1/405F03H1/0081F03H1/0087H05H1/50
    • A magnetically enhanced micro-cathode thruster assembly for providing long-lasting thrust is provided. The micro-cathode thruster assembly includes a tubular housing, a tubular cathode, an insulator, an anode and a magnetic field. The tubular housing includes an open distal end. The tubular cathode is housed within the housing and includes a distal end positioned proximate the open distal end of the housing. The insulator is in contact with the cathode forming an external cathode-insulator interface. The anode is housed within the housing, proximate the open distal end of the housing. The magnetic field is positioned at or about the external cathode-insulator interface and has magnetic field lines with an incidence angle of about 0 to about 90 degrees and preferably about 4 to about 30 degrees relative to the external cathode-insulator interface.
    • 提供了一种用于提供持久推力的磁力增强型微阴极推进器组件。 微阴极推进器组件包括管状壳体,管状阴极,绝缘体,阳极和磁场。 管状壳体包括敞开的远端。 管状阴极容纳在壳体内并且包括靠近壳体的敞开的远端定位的远端。 绝缘体与阴极接触形成外部阴极 - 绝缘体界面。 阳极容纳在壳体内,靠近壳体的敞开的远端。 磁场定位在外部阴极 - 绝缘体界面处或周围,并且具有相对于外部阴极 - 绝缘体界面具有约0至约90度,优选约4至约30度的入射角的磁场线。