Electrostatic acceleration of helicon plasma using a cusped magnetic field-Reference-Cited by-同舟云学术

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Electrostatic acceleration of helicon plasma using a cusped magnetic field

Published:2014-11-10 Issue:19 Volume:105 Page:194101
ISSN:0003-6951
Container-title:Applied Physics Letters
language:en
Short-container-title:Appl. Phys. Lett.

Author:

Harada S.¹²,Baba T.¹,Uchigashima A.¹,Yokota S.¹³,Iwakawa A.¹,Sasoh A.¹,Yamazaki T.²,Shimizu H.²

Affiliation:

1. Department of Aerospace Engineering, Nagoya University, Nagoya, Aichi 464-8603, Japan

2. Mitsubishi Heavy Industry ltd., 16-5 Konan 2-chome, Minato-ku, Tokyo 108-8215, Japan

3. Department of Engineering Mechanics and Energy, University of Tsukuba, 1-1-1 Tennodai Tsukuba, Ibaraki 305-8573, Japan

Funder

Japan Society for Promotion of Science

Publisher

AIP Publishing

Subject

Physics and Astronomy (miscellaneous)

Link

http://aip.scitation.org/doi/pdf/10.1063/1.4900423

Reference30 articles.

1. Plasmas for spacecraft propulsion

2. Ambipolar ion acceleration in an expanding magnetic nozzle

3. VX-200 Magnetoplasma Thruster Performance Results Exceeding Fifty-Percent Thruster Efficiency

4. Improved Efficiency and Throttling Range of the VX-200 Magnetoplasma Thruster

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3. Helicon plasma in a magnetic shuttle;AIP Advances;2020-10-01

4. Central and External Cathode Operations in a Diverging-Magnetic-Field Electrostatic Thruster;Journal of Propulsion and Power;2020-01

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