Effect of Exhaust Magnetic Field in a Helicon Double-Layer Thruster Operating in Xenon

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Charles, Christine
Boswell, Roderick

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Institute of Electrical and Electronics Engineers (IEEE Inc)

Abstract

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

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IEEE Transactions on Plasma Science

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