1975
DOI: 10.1016/s0065-2539(08)61121-x
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Technology of Electron-Bombardment Ion Thrusters

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Cited by 115 publications
(52 citation statements)
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“…Higher cathode temperatures, expected at higher values of emission current, can probably be reduced with modest increases in the cathode orifice diameter as suggested in Ref. 16. Thruster Performance Table 3 shows the performance, obtained in this study, for thrusters operated with three grid optics.…”
Section: Discharge Chambermentioning
confidence: 55%
“…Higher cathode temperatures, expected at higher values of emission current, can probably be reduced with modest increases in the cathode orifice diameter as suggested in Ref. 16. Thruster Performance Table 3 shows the performance, obtained in this study, for thrusters operated with three grid optics.…”
Section: Discharge Chambermentioning
confidence: 55%
“…More complete descriptions of the discharge chamber plasma are [3][4] available~but a short description is included here for convenience.…”
Section: Discharge Chambermentioning
confidence: 99%
“…Cathode erosion raves may be adequately correlated with discharge current level and cathode orifice diameter. (10,12) It was desired to obtain a cathode that exhibited the following: case of starting, low thermal loading due to die.. charge self heating, stability during a high voltage 4ecycle and an acceptable V-I characteristic for discharge currents from 10 to 25 A. Figure 8 illustrates the variation of discharge voltage with discharge chamber magnetic field strength for cathodes with orifice diameters' of 0.75 and 1.52 mm.…”
Section: Discharge Chamber Cathode Performancementioning
confidence: 99%
“…Further gains in ion beam uniformity might be made by magnetic circuit optimization along wrath Yon optics correctives grid misalinement. (7,10) Conclusions Ion optics, cathodes and neutralizers for a 30 cm diameter argon ion source were evaluated. Significant tent results are as follows:…”
Section: Ion Source Beam Characteristicsmentioning
confidence: 99%