Electrical Prototype Power Processor for the 30-cm Mercury electric propulsion engine-Reference-Cited by-同舟云学术

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Electrical Prototype Power Processor for the 30-cm Mercury electric propulsion engine

Published:1978-04-25 Issue: Volume: Page:
ISSN:
Container-title:13th International Electric Propulsion Conference
language:
Short-container-title:

Author:

BIESS J.¹,FRYE R.²

Affiliation:

1. TRW Defense and Space Systems Group, Redondo Beach, Calif.

2. NASA, Lewis Research Center, Cleveland, Ohio

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1978-684

Reference6 articles.

1. Design," NASA TMX 73502, Nov. 1976. [41 Yu, Y. and Biess, J.J. "Some Design Aspects

2. 75-380, March 1975, AIAA, New York, N.Y. [61 Biess, J.J. e t a l , "Thyristor Power Processor

3. f o r the 30cm Mercury E l e c t r i c Propulsion Engine," Paper No. 75-433, March 1975, AIAA,

Cited by 8 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Development status of the NSTAR ion propulsion system power processor;31st Joint Propulsion Conference and Exhibit;1995-07-10

2. A detailed model of ion propulsion systems;25th Joint Propulsion Conference;1989-07-12

3. Simplified Power Supplies for Ion Thrusters;Journal of Spacecraft and Rockets;1982-09

4. Ion Propulsion Cost Effectivity;Electric Propulsion and Its Applications to Space Missions;1981-01-01

5. Reduced Power Processor Requirements for the 30-cm Diam Mercury Ion Thruster;Electric Propulsion and Its Applications to Space Missions;1981-01-01

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