Influence Mechanism of Magnetic Field and Wave Modes on Helicon Plasma Thruster

Author:

Sun Bin1,Zhang Yue2ORCID,Zhou Cheng3,Xia Guangqing1,Lu Chang1,Han Daoman3

Affiliation:

1. Dalian University of Technology, 116024 Dalian, People’s Republic of China

2. Beijing Institute of Mechanical Equipment, 100854 Beijing, People’s Republic of China

3. Beijing Institute of Control and Engineering, 100190 Beijing, People’s Republic of China

Abstract

The mechanism of energy deposition on a helicon plasma thruster under a focused magnetic field is different with a uniform magnetic field, and energy coupling efficiency has greatly improved. This paper studies the spatial distribution of power deposition under different magnetic field configurations. The results show that the magnetic field configuration can change the spatial distribution of energy deposition. A focused magnetic field configuration can couple more energy on the antenna downstream and reduce energy loss during plasma transport, which leads to improved propellant utilization efficiency and enhanced thruster performance. Then this paper studies the energy coupling efficiency and energy distribution characteristics for ionization and acceleration under different W modes, including W1 and W2. The results show that, in the W1 mode, the energy is mainly focused on ion acceleration, resulting in higher ion beam energy. In contrast, the W2 mode is focused on propellant ionization, resulting in greater efficiency of propellant utilization. The W2 mode demonstrates a higher energy coupling efficiency and has superior thruster performance compared to the W1 mode, with a thrust increase of about 1.6 times. The paper proposes several suggestions to improve the thrust-to-weight ratio and specific impulse of a helicon plasma thruster, which provides theoretical support for engineering applications.

Funder

Fundamental Research Funds for the Central Universities of China

National Key RD Program of China

ST Program of Hebei

Advanced Space Propulsion Laboratory of BICE and Beijing Engineering Research Center of Efficient and Green Aerospace Propulsion Technology

National Natural Science Foundation of China

ST Innovation Program of Hebei

ST Program of Langfang

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

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