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FEASIBILITY OF APPLYING FIELD-ION EMISSION TO ELECTROSTATIC ROCKET ENGINES

机译：应用场发射在静电火箭发动机上的可行性

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Application of field-ion emission to electrostatic rocket engines - ionization lifetimes of hydrogen, lithium, sodium, rubidium, cesium, and xenon

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作者
Stankiewicz, N.;
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年度 1963
页码 1-22
总页数 22
原文格式 PDF
正文语种 eng
中图分类工业技术 ;
关键词
CESIUM; ELECTROSTATIC PROPULSION; EMISSION; GAS IONIZATION; HIGH VOLTAGES; HYDROGEN; ION ENGINES; LITHIUM; ROCKET ENGINES; RUBIDIUM; SODIUM; WENTZEL-KRAMER-BRILLOUIN METHOD; XENON; CESIUM; ELECTROSTATIC PROPULSION; EMISSION; HYDROGEN; IONIZATION; LITHIUM; RUBIDIUM; SODIUM; XENON;

机译：铯;静电推进;发射;气体电离;高电压;氢;离子发动机;锂;火箭发动机;铷;钠; WENTZEL-KRamER-BRILLOUIN方法;氙;铯;静电推进;发射;氢;电离;锂;铷;钠;氙;

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4. A Feasibility study on using inkjet technology, micropumps, and MEMs as fuel injectors for bipropellany rocket engines [C] . P. Glynne, C. Bramanti AIAA/ASME/SAE/ASEE Joint Propulsion Conference Exhibit . 2008

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FEASIBILITY OF APPLYING FIELD-ION EMISSION TO ELECTROSTATIC ROCKET ENGINES

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