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公开(公告)号:EP1123642B1
公开(公告)日:2006-09-13
申请号:EP99938169.2
申请日:1999-06-11
IPC分类号: H05H1/54
CPC分类号: H05H1/54 , B64G1/405 , F03H1/0068
摘要: The invention relates to a plasma accelerator arrangement, especially for use as an ion thruster in a spacecraft. According to the invention, the arrangement is structured in such a way that an accelerated electron beam is introduced into an ionisation chamber with propellant gas and guided through the ionisation chamber as a concentrated beam, towards an electric deceleration field which also acts as an acceleration field for the propellant ions produced by ionisation. The arrangement produces a focussed beam of an essentially neutral plasma with a high degree of efficiency. Examples of configurations for electric and magnetic fields for guiding and focussing the beams are also given.