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.
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申请公布号 |
US2006076872(A1) |
申请公布日期 |
2006.04.13 |
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 |
H01J27/02;F03H1/00;H01J7/24;H05B31/26 |
主分类号 |
H01J27/02 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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