发明名称 |
Ion thruster having a hollow cathode assembly with an encapsulated heater, and its fabrication |
摘要 |
An ion thruster (20) has a hollow cathode assembly (50) including a heater (72) with an inner ceramic sleeve (52) and an outer ceramic sleeve (58). The outer ceramic sleeve (58) overlies the inner ceramic sleeve (52) with a filament volume (64) between the two sleeves (52, 58). A wound filament (66) has windings disposed within the filament volume (64), and a mass of ceramic powder (68) fills the remaining portion of the filament volume (64) between the windings of the filament (66). A cathode (76) is disposed within the inner ceramic sleeve (52) of the heater (72). The heater (72) is assembled by preparing the filament (66) and forming it into a wound cylinder, and then encapsulating it and the powder between the inner and the outer ceramic sleeves (58). The hollow cathode assembly (50) may serve as a portion of a plasma source (24) or as a portion of a charge neutralizer (40) (Fig. 3). <IMAGE> |
申请公布号 |
EP1122427(A3) |
申请公布日期 |
2003.12.03 |
申请号 |
EP20010101313 |
申请日期 |
2001.01.20 |
申请人 |
THE BOEING COMPANY |
发明人 |
FALCE, LOUIS RAYMOND;BEATTIE, JOHN R. |
分类号 |
B64G1/40;C04B35/00;F03H1/00 |
主分类号 |
B64G1/40 |
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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