发明名称 Hall effect thruster with anode having magnetic field barrier
摘要 An efficiency enhancing anode-magnetic structure of a Hall effect thruster produces a radially directed magnetic field between inner and outer poles at the exit portion of a gas distribution channel. The field-shaping structure includes magnetic material extending alongside the channel with an associated secondary flux-generating component to create an axially directed magnetic field in the area between the anode of the thruster and the exit portion of the gas distribution channel.
申请公布号 US7164227(B2) 申请公布日期 2007.01.16
申请号 US20050233401 申请日期 2005.09.21
申请人 AEROJET-GENERAL CORPORATION 发明人 DE GRYS KRISTI H.
分类号 H05H5/03 主分类号 H05H5/03
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