Experimental and theoretical investigations of the Giessen neutralizer system
Author:
Affiliation:
1. Giessen, Universitaet, Giessen, West Germany
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1978-706
Reference12 articles.
1. Brunet, A., Hollow Cathode Discharges: Arc Regime with Interior Positive Column in a Flow of Argon, ONERA Note Technique, No. 1975-3
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1. Thermographic investigation of 3.2 mm diameter orificed hollow cathodes;34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit;1998-07-13
2. A review of the manufacturing and characterization activities at PROEL of a plasma bridge neutralizer for the RIT 10 ion thruster;21st International Electric Propulsion Conference;1990-07-18
3. Performance data comparison of the inert gas RIT 10;Journal of Spacecraft and Rockets;1984-07
4. RIT 35-Design and Application of the Giessen Primary Propulsion Engine;Electric Propulsion and Its Applications to Space Missions;1981-01-01
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