Experimentally Determined Neutral Density and Plasma Parameters in a 30 CM Ion Engine-Reference-Cited by-同舟云学术

Experimentally Determined Neutral Density and Plasma Parameters in a 30 CM Ion Engine

Published:2004-06-21 Issue: Volume: Page:
ISSN:
Container-title:40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
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Author:

Sengupta Anita¹,Goebel Dan¹,Tynan George²,Doerner Russ²,Fitzgerald D.¹,Owens A.³

Affiliation:

1. Jet Propulsion Laboratory

2. University of California San Diego

3. California Institute of Technology

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2004-3613

Reference17 articles.

1. Williams, G. J., The Use of Laser-Induced Fluorescence to Characterize Discharge Cathode Erosion in a 30 cm Ring-CuspIonThruster,Ph.D.Dissertation,UniversityofMI,2000.

2. Williams, G. J.,et al. "Characterization of FMT-2Discharge CathodePlume," IEPC-99-104, Oct.1999.

3. Herman, D., et al. "Comparison of Discharge Plasma Parameters in a 30-cm NSTAR Type Ion Engine with and without BeamExtraction", AIAA-03-5162,July,2003.

4. Polk, J. E., et al. "An Overview of the Results from an 8200 Hour Wear Test of the NSTAR Ion Thruster," AIAA-99-2446,June1999.

5. Sengupta, A., et al, "Status of the Extended Life Test of the Deep Space 1 Flight Spare Ion Engine After 30,352 HoursofOperation,"AIAA-2003-4558,July2003.

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