Helicon hall thruster

Electric lamp and discharge devices: systems – Discharge device load with fluent material supply to the... – Plasma generating

Reexamination Certificate

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C315S111610, C315S111810

Reexamination Certificate

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07436122

ABSTRACT:
Atoms of a propellant gas are ionized in a helicon plasma source, preferably in an annular area between inner and outer cylinders. The annular ionization area is aligned with an annular acceleration stage similar to the electrical-magnetic acceleration stage of a Hall effect thruster.

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patent: 2003/0111963 (2003-06-01), Tolmachev et al.
patent: 2006/0168936 (2006-08-01), Rooney
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Yun, S., et al., “Density Enhancement Near Lower Hybrid Resonance Layer in m=0 Helicon Wave Plasmas,” Physics of Plasmas 8(1):358-363, 2001.

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