Helicon Double Layer Thrusters-Reference-Cited by-同舟云学术

Helicon Double Layer Thrusters

Published:2006-07-09 Issue: Volume: Page:
ISSN:
Container-title:42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
language:
Short-container-title:

Author:

Charles Christine,Boswell Rod,Alexander P.,Costa C.,Sutherland Orson,Pfitzner Leigh,Franzen R.,Kingwell Jeff,Parfitt A.,Frigot Pierre-Etienne,Gonzalez del Amo J.,Gengembre E.,Saccoccia G.,Walker R.

Publisher

American Institute of Aeronautics and Astronautics

Reference19 articles.

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

2. Ion acceleration in plasmas emerging from a helicon-heated magnetic-mirror device

3. Parallel velocity and temperature of argon ions in an expanding, helicon source driven plasma

4. Experimental evidence of parametric decay processes in the variable specific impulse magnetoplasma rocket (VASIMR) helicon plasma source

5. The Current-Free Electric Double Layer in a Coronal Magnetic Funnel

Cited by 10 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Simulation of a helicon plasma source in a magnetoplasma rocket engine;Plasma Science and Technology;2022-06-08

2. RF Helicon-based Inductive Plasma Thruster (IPT) Design for an Atmosphere-Breathing Electric Propulsion system (ABEP);Acta Astronautica;2020-11

3. Plasma Fluid Simulation of RF Discharge in Non-Uniform Magnetic Field for RF Plasma Thruster;AIAA Propulsion and Energy 2020 Forum;2020-08-17

4. Numerical Simulation of Non-Uniform Magnetic Field Type RF Plasma Thruster Using Fluid Model;TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN;2020

5. Combined Chemical–Electric Propulsion for a Stand-Alone Mars CubeSat;Journal of Spacecraft and Rockets;2019-11