发明名称 |
STARTER CIRCUIT FOR AN ION ENGINE |
摘要 |
A starter circuit particularly suitable for a plasma of an ion engine for a spacecraft includes a power supply having an output inductor with a tap. A switch is coupled to the tap. The switch has a control input. A pulse control logic circuit is coupled to said control input, said pulse control logic circuit controlling said switch to an off state to generate a high voltage discharge.
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申请公布号 |
US2002047623(A1) |
申请公布日期 |
2002.04.25 |
申请号 |
US20010935189 |
申请日期 |
2001.08.22 |
申请人 |
HUGHES ELECTRONICS CORPORATION |
发明人 |
CARDWELL GILBERT I.;PHELPS THOMAS K. |
分类号 |
F03H1/00;(IPC1-7):H05B31/26 |
主分类号 |
F03H1/00 |
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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