Pulsed plasma thruster variations for improved mission capabilities-Reference-Cited by-同舟云学术

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Pulsed plasma thruster variations for improved mission capabilities

Published:2000-07-24 Issue: Volume: Page:
ISSN:
Container-title:36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
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Author:

Scharlemann C.¹,Mikellides I.¹,Mikellides P.¹,Turchi P.¹,Corey R.¹

Affiliation:

1. Ohio State Univ., Columbus

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2000-3260

Reference3 articles.

1. I.G.Mikellides, PJ. Turchi, Optimization of Pulsed Plasma Thruster in Retangular and Coaxial Geometries, IEPC 99-211

2. P.G.Mikellides, PJ. Turchi, Modelling Electric Propulsion and Cometary Resource of Late-Time Ablation in Pulsed Plasma Utilization,IEPC-99-189 Thrusters, AIAA96-2733,July 1996

Cited by 5 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. Plasma in Space Propulsion;Plasma Engineering;2018

2. Plasma in Space Propulsion;Plasma Engineering;2013

3. Numerical Simulation of a Water Propellant Pulsed Plasma Thruster;48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2012-07-30

4. Pulsed Plasma Thruster Using Water Propellant, Part I: Design and Investigation of Thrust Behavior;39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2003-06-26

5. Pulsed Plasma Thruster Using Water, Part II: Thruster Operation and Performance Evaluation;39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2003-06-26

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