Control of Low-Frequency Oscillation in a Hall Thruster
Author:
Affiliation:
1. Graduate School, Nagoya University
2. Department of Aerospace Engineering, Nagoya University
Publisher
Japan Society for Aeronautical and Space Sciences
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://www.jstage.jst.go.jp/article/tjsass/44/145/44_145_164/_pdf
Reference19 articles.
1. 1) 2Furukawa, T., Miyasaka, T., Sakurai, Y. and Fujiwara, T.: Measurement and Modeling of Low Frequency Oscillation in a Hall Thruster, ISTS-00-b-22 (2000).
2. 2) Boeuf, J. P. and Garritues, L.: Low Frequency Oscillation in a Stationary Plasma Thruster, J. Appl. Phys., 84 (1998), pp. 3541–3554.
3. 3) Komurasaki, K. and Arakawa, Y.: Two-Dimensional Numerical Model of Plasma Flow in a Hall Thruster, J. Propul. Power., 11 (1995), pp. 1317–1323.
4. 4) Jankovsky, R., Tverdokhlebov, S. and Manzella, D.: High Power Hall Thrusters, AIAA-99-315745 (1999).
5. 5) Hirakawa, M.: Plasma Particle Simulation in Electric Propulsion, Tokyo-Univ., Ph.D. Thesis, 1995.
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