Operating a magnetic nozzle helicon thruster with strong magnetic field

A pulsed axial magnetic field up to ∼2.8 kG is applied to a 26-mm-inner-diameter helicon plasma thruster immersed in a vacuum chamber, and the thrust is measured using a pendulum target. The pendulum is located 30-cm-downstream of the thruster, and the thruster rf power and argon flow rate are fixed...

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Veröffentlicht in:	Physics of plasmas 2016-03, Vol.23 (3)
Hauptverfasser:	Takahashi, Kazunori, Komuro, Atsushi, Ando, Akira
Format:	Artikel
Sprache:	eng
Schlagworte:	70 PLASMA PHYSICS AND FUSION TECHNOLOGY ARGON CLASSICAL AND QUANTUM MECHANICS, GENERAL PHYSICS COMPARATIVE EVALUATIONS FLOW RATE Flow velocity GAS FLOW LOSSES MAGNETIC FIELDS Magnetic nozzles Magnetism MECHANICAL VIBRATIONS NOZZLES One dimensional models ONE-DIMENSIONAL CALCULATIONS OSCILLATIONS PLASMA DENSITY Plasma loss Plasma physics Thrust THRUSTERS TIME MEASUREMENT Vacuum chambers
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