On-Orbit Demonstration of a Pulsed Self-Field Magnetoplasmadynamic Thruster System-Reference-Cited by-同舟云学术

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On-Orbit Demonstration of a Pulsed Self-Field Magnetoplasmadynamic Thruster System

Published:2000-09 Issue:5 Volume:16 Page:880-886
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Toki K.¹,Shimizu Y.¹,Kuriki K.¹

Affiliation:

1. Institute of Space and Astronautical Science, Kanagawa 229-8510, Japan

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/2.5655

Reference32 articles.

1. Application of MPD thruster systems to interplanetary missions

2. Performance and lifetime assessment of magnetoplasmadynamic arc thruster technology

3. Mass savings domain of plasma propulsion for LEO to GEO transfer

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1. Effect of pulse frequency on discharge characteristics of Hall thruster under pulsating operation;Vacuum;2024-06

2. The technological and commercial expansion of electric propulsion;Acta Astronautica;2019-06

3. Numerical investigations of a repetitively pulsed MPD thruster;IEEJ Transactions on Electrical and Electronic Engineering;2012-03-20

4. A porous flow control element for pulsed plasma thrusters;CEAS Space Journal;2011-10-08

5. Numerical Study of Plasma Behavior in a Magnetoplasmadynamic Thruster Around Critical Current;Journal of Propulsion and Power;2009-03

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