Continuing life test of a xenon hollow cathode for a space plasma contactor-Reference-Cited by-同舟云学术

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Continuing life test of a xenon hollow cathode for a space plasma contactor

Published:1994-06-27 Issue: Volume: Page:
ISSN:
Container-title:30th Joint Propulsion Conference and Exhibit
language:
Short-container-title:

Author:

Sarver-Verhey Timothy¹

Affiliation:

1. NYMA, Inc., Brook Park, OH

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1994-3312

Reference30 articles.

1. "ohl, W.H., Handbook of Materials and Techniques for Vacuum Devices, Reinhold, New York, 1967,pp.491-496.

2. Development and flight history of the SERT II spacecraft

3. SAnon. "8-cm Mercury Ion Thruster System Technology,"NASA TMX-71611, Oct. 1974.

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1. Analysis of Effect of Ground Experiment Environment on Plasma Contactor Performance;AIAA Journal;2023-03

2. Operating Characteristics of Hall Thruster with Radio Frequency Plasma Cathode;JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES;2016

3. Experimental Investigation of Inductively Coupled Plasma Cathode for the Application to Ion Thrusters;47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2011-07-31

4. Ongoing Wear Test of a XIPS 25-cm Thruster Discharge Cathode;44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit;2008-07-21

5. Near-field investigation of ions emitted from a hollow cathode assembly operating at low-power;34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;1998-07-13

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