Effect of Exhaust Magnetic Field in a Helicon Double-Layer Thruster Operating in Xenon
A xenon ion beam is spatially characterized by using a retarding-field energy analyzer positioned 7 cm downstream of a helicon double-layer thruster (HDLT) operating at 500-W radio-frequency power, 0.07-mtorr (9.33 × 10-3Pa) gas pressure, and with an exh
|Collections||ANU Research Publications|
|Source:||IEEE Transactions on Plasma Science|
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