发明名称 Multichannel Hall effect thruster
摘要 A Hall effect thruster for propelling spacecraft and satellites includes at least two acceleration channels, each of the channels has a closed end and an open end, and a plurality of flux guides adjacent each of the channels. The plurality of flux guides includes an innermost flux guide, an outermost flux guide, and at least one intermediate flux guide. Each intermediate flux guide helps provide a magnetic field to each of two adjacent acceleration channels.
申请公布号 US2005116652(A1) 申请公布日期 2005.06.02
申请号 US20030726398 申请日期 2003.12.02
申请人 MCVEY JOHN B.;PERRUCCI ANDREW S.;BRITT EDWARD J. 发明人 MCVEY JOHN B.;PERRUCCI ANDREW S.;BRITT EDWARD J.
分类号 F03H1/00;H01J7/24;(IPC1-7):H01J7/24 主分类号 F03H1/00
代理机构 代理人
主权项
地址