AI Chat Paper
Note: Please note that the following content is generated by AMiner AI. SciOpen does not take any responsibility related to this content.
{{lang === 'zh_CN' ? '文章概述' : 'Summary'}}
{{lang === 'en_US' ? '中' : 'Eng'}}
Chat more with AI
PDF (5.8 MB)
Collect
Submit Manuscript AI Chat Paper
Show Outline
Outline
Show full outline
Hide outline
Outline
Show full outline
Hide outline
Publishing Language: Chinese

Research status and prospect of high-power wave-heating magnetoplasma thruster

Xiong YANG1Xiaokang LI1Dawei GUO1Mousen CHENG1( )Fan ZHANG2Bixuan CHE1Qingyun LEI1
College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China
Beijing Institute of Tracking and Telecommunications Technology, Beijing 100094, China
Show Author Information

Abstract

The wave-heating magnetoplasma thruster possesses many advantages such as its suitability for high power propulsion (about 100 kWe-1 MWe), high thrust density (about 4×105 N/m2), variable high thrust (about 1-100 N), and adjustable specific impulse (about 3 000-10 000 s). These advantages make the wave-heating magnetoplasma thruster well suited for a diverse range of future space missions with high-performance. Based on previous studies of the wave-heating magnetoplasma thruster both home and abroad, this work summarizes the technical status of the wave-heating magnetoplasma thruster in recent years, and analyzes the theoretical issues the present research faced in the development of the wave-heating magnetoplasma thruster, such as the so called single-pass ion cyclotron resonance heating, the plasma detachment controlling, the high-power density plasma diagnosing in strong magnetic fields, as well as many engineering difficulties, including the efficient thermal management and high-power RF power supplies. Finally, application directions of the wave-heating magnetoplasma thruster are prospected according to its performance characteristics.

CLC number: V439 Document code: A

References

【1】
【1】
 
 
Acta Aeronautica et Astronautica Sinica
Article number: 028761

{{item.num}}

Comments on this article

Go to comment

< Back to all reports

Review Status: {{reviewData.commendedNum}} Commended , {{reviewData.revisionRequiredNum}} Revision Required , {{reviewData.notCommendedNum}} Not Commended Under Peer Review

Review Comment

Close
Close
Cite this article:
YANG X, LI X, GUO D, et al. Research status and prospect of high-power wave-heating magnetoplasma thruster. Acta Aeronautica et Astronautica Sinica, 2024, 45(7): 028761. https://doi.org/10.7527/S1000-6893.2023.28761

739

Views

15

Downloads

0

Crossref

2

Scopus

2

CSCD

Received: 29 March 2023
Revised: 17 April 2023
Accepted: 07 May 2023
Published: 28 February 2024
© 2024 The Journal of Acta Aeronautica et Astronautica Sinica