A rational design method for the Nagoya type-III antenna

TL;DR

This paper develops a rational, practical design method for the Nagoya type-III helicon antenna, enabling quick and effective dimensioning for plasma thruster applications based on simplified models and full-wave simulations.

Contribution

It introduces a simplified, rational approach for designing the antenna length of Nagoya type-III helicon antennas, validated against full-wave 3D simulations.

Findings

Derived a practical formula for antenna length based on plasma and tube dimensions.

Validated simplified models against full-wave simulations with good agreement.

Provided a rapid prototyping method for helicon antenna design.

Abstract

The current study, as part of a PhD project on the design of a helicon thruster, aims to provide a rational methodology for the design of the helicon thruster's main component, i.e., the helicon antenna. A helicon thruster is an innovative electrodeless plasma thruster that works by exciting helicon waves in a magnetized plasma, and its antenna is capable of producing a uniform, low-temperature, high-density plasma. A magnetic nozzle is used to accelerate the exhaust plasma in order to generate a propulsive thrust. In this paper, we consider a simple helicon antenna, specifically the Nagoya type-III antenna. We consider a common experimental setup consisting of a quartz tube with finite length containing a uniform magnetized plasma and a Nagoya type-III antenna placed at the tube centre. Considering previous studies on helicon waves theory, we compare three different design methods, each based on simplifying different modelling assumptions, and evaluate the predictions of these models with results from full-wave 3D simulations. In particular, we concentrate on deriving a rational design method for the helicon antenna length, given the dimension of the quartz tube and the desired target plasma parameters. This work aims to provide a practical and fast method for dimensioning the antenna length, useful for initializing more accurate but computationally heavier full-wave simulations in 3D geometry or simply for a rapid prototyping of the helicon antenna. These results can be useful for the development of a helicon thruster but also for the design of a high-density radiofrequency plasma source.