发明名称 A HALL EFFECT PLASMA ACCELERATOR
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.
申请公布号 WO9737517(A3) 申请公布日期 1997.12.04
申请号 WO1997US05254 申请日期 1997.03.31
申请人 INTERNATIONAL SCIENTIFIC PRODUCTS 发明人 YASHNOV, Y. M.;PETROSOV, V. A.;BARANOV, V. I.;VASIN, A. I.
分类号 H05H1/54;B64G1/40;F03H1/00 主分类号 H05H1/54
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