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    A hall effect plasma accelerator
    2.
    发明公开
    A hall effect plasma accelerator 失效
    霍尔效应等离子体加速器

    公开(公告)号：EP0800196A1

    公开(公告)日：1997-10-08

    申请号：EP96308748.1

    申请日：1996-12-03

    申请人： MATRA MARCONI SPACE FRANCE S.A. ,  Keldysh Research Center

    发明人： Yashnov, Yuri Michaylovich ,  Petrosov, Valery Alexandrovich ,  Baranov, Vladimir Ivanovich ,  Vasin, Anatoly Ivanovich

    IPC分类号： H01J27/08 ,  F03H1/00 ,  H01J37/08

    CPC分类号： F03H1/0075 ,  B64G1/405

    摘要： A Hall effect plasma accelerator comprises an annular accelerating channel. A radial magnetic field is applied across the channel between magnetic poles of opposite polarity. Instead of these magnetic poles being linked by magnetic material extending around the closed end of the channel so as to form a single magnet, the invention proposes that the magnetic poles be defined on bodies of material which are magnetically separate. This allows the designer to have greater freedom in selecting the dimensions of the thruster in general and of the magnetic system in particular, thereby giving an opportunity to improve thruster efficiency and to manufacture thrusters having a wide variety of different shapes depending on available space.

    摘要翻译： 霍尔效应等离子体加速器包括环形加速通道。 在相反极性的磁极之间的通道上施加径向磁场。 代替这些磁极通过围绕通道封闭端延伸的磁性材料连接以形成单个磁体，本发明提出磁极被限定在磁性分离的材料体上。 这使得设计者在选择推力器的大小和特别是磁系统的尺寸时具有更大的自由度，由此提供了提高推进器效率的机会并且根据可用空间制造具有各种不同形状的推进器。

    Steerable hall effect thruster
    4.
    发明公开
    Steerable hall effect thruster 失效
    Steuerbarer Hall-Effekt-Antrieb

    公开(公告)号：EP0778415A1

    公开(公告)日：1997-06-11

    申请号：EP96308749.9

    申请日：1996-12-03

    申请人： MATRA MARCONI SPACE FRANCE S.A. ,  Keldysh Research Center

    发明人： Yashnov, Yuri Michaylovich ,  Petrosov, Valery Alexandrovich ,  Baranov, Vladimir Ivanovich ,  Vasin, Anatoly Ivanovich ,  Koroteev, Anatoly Sazonovich ,  Poussin, Jean Francios ,  Stephan, Jean Marc ,  Balaam, Philip Andrew ,  Britt, Edward Joseph, Dr. ,  Koester, John, Dr.

    IPC分类号： F03H1/00

    CPC分类号： F03H1/0075 ,  B64G1/405

    摘要： In a Hall effect thruster, especially for use in manoeuvring satellites, a stream or plume of ions, used to produce the thrust is deflected, by appropriate adjustment of a magnetic field, so as to steer the satellite or other vehicle. The channel (20), along which the ions are accelerated, is preferably flared outwardly at its open end (22A) so as to avoid erosion which would otherwise be caused by the deflection. The adjustment of the magnetic field is preferably achieved by dividing an outer magnetic pole, surrounding the channel, into separate sectors (38A, 38B, 38C, 38D) and winding individual electric coils (18, 18', 19, 19') around the sectors. Control of the current through these individual coils is used to make the appropriate adjustments of magnetic field.

    摘要翻译： 在霍尔效应推进器中，特别是用于操纵卫星时，用于产生推力的用于产生推力的流或羽流通过适当地调整磁场而被偏转，以便引导卫星或其他车辆。 离子被加速沿着的通道（20）优选地在其开口端（22A）处向外扩张，以避免否则由偏转引起的侵蚀。 优选地，通过将​​围绕通道的外部磁极分成单独的扇区（38A，38B，38C，38D）并且围绕着各个电线圈（18,18'，19,19'）卷绕来实现磁场的调节。 部门。 通过这些单个线圈的电流的控制用于对磁场进行适当的调整。