发明名称 A CLOSED ELECTRON DRIFT PLASMA THRUSTER ADAPTED TO HIGH THERMAL LOADS
摘要 The closed electron drift plasma thruster uses a magnetic circuit to create a magnetic field in a main annular channel (124) for ionization and acceleration, said magnetic circuit comprises: an essentially radial first outer pole piece (134); a conical second outer pole piece (311); an essentially radial first inner pole piece (135); a conical second inner pole piece (351); a plurality of outer magnetic cores (137) surrounded by outer coils (131) to interconnect the first and second outer pole pieces (134, 311); an axial magnetic core (138) surrounded by a first inner coil (133) and connected to the first inner pole piece (135); and a second inner coil (132) placed upstream from the outer coils (131). The thruster also comprises a plurality of radial arms (352, 136) included in the magnetic circuit, and a structural base (175) which is separate from the magnetic circuit and which serves, amongst other things, to cool the coils (131, 132, 133).
申请公布号 CA2280479(A1) 申请公布日期 2000.02.25
申请号 CA19992280479 申请日期 1999.08.18
申请人 SOCIETE NATIONALE D-ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION - S.N .E.C.M.A. 发明人 BUGEAT, JEAN-PIERRE;VALENTIAN, DOMINIQUE;KLINGER, ERIC
分类号 F03H1/00;H05H1/54;(IPC1-7):F03H1/00 主分类号 F03H1/00
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