Discharge Chamber Plasma Structure of a 40-cm NEXT-type Ion Engine-Reference-Cited by-同舟云学术

Discharge Chamber Plasma Structure of a 40-cm NEXT-type Ion Engine

Published:2005-07-10 Issue: Volume: Page:
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Container-title:41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Herman Daniel,Gallimore Alec

Publisher

American Institute of Aeronautics and Astronautics

Reference52 articles.

1. A Critical History of Electric Propulsion: The First 50 Years (1906-1956)

2. 2Polk,J.E.,Kakuda,R.Y.,Anderson,J.R.,Brophy,J.R.,Rawlin,V.K.,Patterson,M.J.,Sovey,J.S.andHamley,J. "Performance oftheNSTAR IonPropulsion Systemon the DeepSpace OneMission,"AIAA-2001-0965,39thAIAA Aerospace Sciences Meeting and ExhibitJointPropulsion Conference, Reno, NV, January8-11,2001.

3. 4Patterson,M.J.,Rawlin,V.K.,Sovey,J.S.,Kussmaul,M.andParkes,J."2.3kWIonThrusterWearTest,"AIAA-1995-2516, 31stAIAA /ASME / SAE /ASEEJointPropulsion Conference, San Diego,CA, July 10-12.

4. 5Polk,J.E.,Patterson,M.J.,Brophy,J.R.,Rawlin,V.K.,Sovey,J.S.,Myers,R.M.,Blandino,J.J.,Goodfellow,K.D.and Garner, C. E. "A 1000 Hour WearTest ofthe NASA NSTAR Ion Thruster,"AIAA-1996-2784,32nd AIAA/ ASME / SAE / ASEE JointPropulsion Conference,LakeBuenaVista,FL, July 1-3.

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2. Ion Engine Discharge Chamber Plasma Modeling Using a 2-D PIC Simulation;42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2006-07-09

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