Experimental Study on Operating Range Extension of Hall Thrusters under Pulsating Mode-Reference-Cited by-同舟云学术

Experimental Study on Operating Range Extension of Hall Thrusters under Pulsating Mode

Published:2023-07 Issue:4 Volume:36 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Ma Haochen¹,Wei Liqiu²^ORCID,Cai Haikuo³,Wang Shangmin⁴,Han Liang⁵,He Yongfeng⁶,Li Hong⁷,Ding Yongjie⁸

Affiliation:

1. Doctoral Candidate, School of Energy Science and Engineering, Harbin Institute of Technology, Harbin, Heilongjiang 150001, People’s Republic of China.

2. Professor, Key Laboratory of Aerospace Plasma Propulsion, Ministry of Industry and Information Technology, Harbin, Heilongjiang 150001, People’s Republic of China (corresponding author). ORCID: .

3. Assistant Engineer, Knock Engine Technology Research Center, Beijing Institute of Power Machinery, Beijing 100074, People’s Republic of China.

4. Senior Engineer, Science and Technology on Vacuum Technology and Physics Laboratory, Lanzhou Institute of Physics, Lanzhou 730000, People’s Republic of China.

5. Senior Engineer, Propulsion Systems Dept., Beijing Institute of Power Machinery, Beijing 100074, People’s Republic of China.

6. Senior Engineer, Key Laboratory of Aerospace Plasma Propulsion, Ministry of Industry and Information Technology, Harbin, Heilongjiang 150001, People’s Republic of China.

7. Associate Professor, Key Laboratory of Aerospace Plasma Propulsion, Ministry of Industry and Information Technology, Harbin, Heilongjiang 150001, People’s Republic of China.

8. Professor, Key Laboratory of Aerospace Plasma Propulsion, Ministry of Industry and Information Technology, Harbin, Heilongjiang 150001, People’s Republic of China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

https://ascelibrary.org/doi/pdf/10.1061/JAEEEZ.ASENG-4949

Reference26 articles.

1. Tutorial: Physics and modeling of Hall thrusters

2. Bugrova A. A. Lipatov S. Baranov A. Morozov and Y. Daren. 2005. “SPT operation in ‘machine-gun’ mode.” In Proc. 29th Int. Electric Propulsion Conf. Cleveland: Electric Rocket Propulsion Society.

3. Investigating a two-stage electric space propulsion system: Simulation of plasma dynamics

4. Effect of azimuthal diversion rail location on the performance of Hall thrusters

5. Focia R. J. and C. A. Frost. 2009. “A compact low jitter fast rise time gas-switched pulse generator system with high pulse repetition rate capability.” In Proc. 2009 IEEE Pulsed Power Conf. 1227–1232. Washington DC: IEEE.

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