Preliminary Development and Testing of a Self-Injecting Gallium MPD Thruster-Reference-Cited by-同舟云学术

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Preliminary Development and Testing of a Self-Injecting Gallium MPD Thruster

Published:2008-07-21 Issue: Volume: Page:
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Container-title:44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Thomas Robert,Burton Rodney,Polzin Kurt

Publisher

American Institute of Aeronautics and Astronautics

Reference17 articles.

1. 1Markusic, T.E., Thio, Y.C.F., and Cassibry, J.T. "Design of a high-energy, two stage pulse plasma thruster," 38th AIAA/ASME/SAE/ASEEJoint Propulsion Conference, July 7-10,2002, AIAAPaper 2002-4125.

2. 3Thomas, R.E., Burton, R.L., Glumac, N.G., and Polzin, K.A. "Preliminary Spectroscopic Measurements for a Gallium Electromagnetic (GEM) Thruster," 43rdAIAA/ASME/SAE/ASEE Joint Propulsion Conference, July8-11,2007,AIAAPaper2007-5257.

Cited by 3 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. Performance Characteristics of an Ablative Gallium Electromagnetic Accelerator;Journal of Propulsion and Power;2013-07

2. Pulsed Plasma Thrusters;Encyclopedia of Aerospace Engineering;2010-12-15

3. Investigation of a Gallium MPD Thruster with an Ablating Cathode;46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2010-07-25

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