Laboratory Model Development of Lissajous Acceleration for Electrodeless Helicon Plasma Thruster-Reference-Cited by-同舟云学术

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Laboratory Model Development of Lissajous Acceleration for Electrodeless Helicon Plasma Thruster

Published:2012-07-30 Issue: Volume: Page:
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Container-title:48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Matsuoka Takeshi,Funaki Ikkoh,Satoh Syuhei,Fujino Takayasu,Iwabuchi Shota,Nakamura Takahiro,Nishida Hiroyuki,Shinohara Shunjiro,Tanikawa Takao,Hada Tohru,Shamrai Konstantin

Publisher

American Institute of Aeronautics and Astronautics

Reference22 articles.

1. Current-free double-layer formation in a high-density helicon discharge

2. 4West, M. D., Charles, C., and Boswell, R. W. "SpaceSimulation TestingoftheHelicon Double Layer ThrusterPrototype," 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference &Exhibit, AIAA2010-7016, July25 -28,Nashville, TN, 2010.

3. Direct thrust measurement of a permanent magnet helicon double layer thruster

4. 6Williams, L. T., Walker, M. L. R. "Thrust Measurements of a Helicon Plasma Source," 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference &Exhibit, AIAA2011-5893,Jul.31-Aug. 3,San Diego,2011.

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1. Laboratory Model Development of Lissajous Acceleration for Electrodeless Helicon Plasma Thruster;48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2012-07-30

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