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Convergent neutral gas injection using supersonic gas puffing (SSGP) method for propellant feeding system in RF electric propulsion.

作者信息

Furukawa Takeru, Ishigami Yuichi, Kuwahara Daisuke, Miyazawa Jyunichi, Shinohara Shunjiro

机构信息

Kobe University, Hyogo 657-8501, Japan.

Tokyo University of Agriculture and Technology, Tokyo 184-8588, Japan.

出版信息

Rev Sci Instrum. 2022 Aug 1;93(8):083501. doi: 10.1063/5.0082821.

DOI:10.1063/5.0082821
PMID:36050084
Abstract

A convergent gas feeding method is proposed to alleviate neutral gas depletion near the central plasma region in typical electrodeless radio-frequency (RF)/helicon plasma thrusters. To achieve further performance improvement, the SuperSonic Gas Puffing (SSGP) system is one of the methods that is expected to overcome the above-mentioned depletion and the density limit. This study discovered that the spatiotemporal profiles of the neutral pressure and the estimated gas diffusion angle vary depending on the SSGP gas feeding condition, i.e., the nozzle size, filling pressure, and the valve opening time. Convergent gas feeding is successfully conducted using the SSGP method in a vacuum. As a preliminary study, high-density plasma is also obtained in the vicinity of the gas injection region using the developed SSGP system. The effects of the gas feeding position and an external divergent magnetic field on the plasma density are investigated. A suitable gas feeding position/region exists for plasma generation using the RF/helicon plasma thruster.

摘要

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