Optimization of Performance and Efficiency of a Coaxial Pulsed Plasma Thruster-Reference-Cited by-同舟云学术

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Optimization of Performance and Efficiency of a Coaxial Pulsed Plasma Thruster

Published:2002-07-07 Issue: Volume: Page:
ISSN:
Container-title:38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Jaeger Stephen,Burton Rodney,Laystrom Julia,Benavides Gabriel

Publisher

American Institute of Aeronautics and Astronautics

Reference7 articles.

1. Advanced pulsed plasma thruster electrical components

2. Wilson, M.J., Bushman, S.S., and Burton, R.L. "A Compact Thrust Stand for Pulsed Plasma Thrusters." 25thInternational Electric Propulsion Conference, IEPCPaper 97-122, Cleveland, OH, Aug. 1997.

3. Rysanek, F., Burton, R. L. "Performance and Heat Loss of a Coaxial Teflon Pulsed Plasma Thruster" 37th International Electric Propulsion Conference, IEPC Paper Number 01-151, Pasadena, CA, Oct. 2001.

4. AIAA Progress Series;Burton R. L.,2000

Cited by 2 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. Study on the influence of ignitor position on a coaxial pulsed plasma thruster;Vacuum;2023-12

2. Geometric Optimization of a Coaxial Pulsed Plasma Thruster;39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;2003-06-26

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