Insert Temperature Measurements of a 180A Hollow Cathode for the HiPER Project-Reference-Cited by-同舟云学术

Insert Temperature Measurements of a 180A Hollow Cathode for the HiPER Project

Published:2012-07-30 Issue: Volume: Page:
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Container-title:48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Author:

Coletti Michele,Gabriel Stephen

Publisher

American Institute of Aeronautics and Astronautics

Reference7 articles.

1. C.Casaregola, G.Cesaretti, and M.Andrenucci. HiPER: a Roadmap for Future Space Exploration with innovative Electric Propulsion Technologies. 31st International Electric Propulsion Conference,University of Michigan, Ann Arbor, Michigan, USA, September 20 -24. 2009

2. M.Coletti, R.Intini Marques, and S.B.Gabriel. Discharge hollow cathode design for a dual-stage gridded ion engine. Proc.IMechEPart J, J.AerospaceEngineering,Vol226, 272-280.2011

3. I.M.Ahmed Rudwan, N.C.Wallace, and M.Kelly. Dispenser Temperature Profile Measurements and Discharge Current Division in the T5&T6 Kaufman-type Ion Thruster. 30th International Electric Propulsion Conference, Florence, ItalySeptember 17-20.2007

4. D.M.Goebel, I.Katz, Y.Mikellides, and J.Polk. Extending Hollow Cathode Life for Deep Space Missions. AIAA Space2004 Conference, San Diego, California,September. 2004

5. Experimental study of impregnated-cathode behavior, emission, and life

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