Flight performance test of MPD thruster system
Author:
Affiliation:
1. Tokyo, University, Tokyo, Japan
2. Ishikawajima-Harima Heavy Industries Co., Ltd., Yokohama, Japan
3. National Space Development Agency of Japan, Tokyo, Japan
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1981-664
Reference13 articles.
1. K u r i k i , K. and S u z u k i , H." Q u a s i s t e a d y MPD A r c j e t w i t h Anode Gas I n j e c t i o n , ' AIM paper 79-2058, 1979.
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1. 10 kW class pulsed MPD thruster design for SEOTV applications;30th Joint Propulsion Conference and Exhibit;1994-06-27
2. Development of MPD thruster EM for a space test;21st International Electric Propulsion Conference;1990-07-18
3. Performance and lifetime assessment of MPD arc thruster technology;24th Joint Propulsion Conference;1988-07-11
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