publication . Conference object . 2005

High Power Helicon Thruster

Timothy Ziemba; John Carscadden; James Prager; John Slough; Robert Winglee;
  • Published: 10 Jul 2005
  • Publisher: American Institute of Aeronautics and Astronautics
The High Power Helicon (HPH) plasma thruster under development at MSNW and the University of Washington is an emerging electrode-less in-space thruster that is potentially capable of high thrust level (1-2 Newtons) at moderate power levels of 20 to 50 kW. Unlike previous lower power (2 to 5 kW) helicon thruster schemes, which have been shown to produce moderate temperature of 5 to 10 eV thermal plasmas, the HPH axial and radial plasma characteristics show that the plasma is created in the helicon coil and is then accelerated in the axial direction downstream away from the HPH. The bulk acceleration of the plasma is believed to be due to a directional coupling of...
free text keywords: Electric field, Xenon, chemistry.chemical_element, chemistry, Argon, Plasma, Ambipolar diffusion, Propellant, Helicon, Materials science, Ion, Atomic physics
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