Design of high efficiency and high thrust grid system for ion thruster-Reference-Cited by-同舟云学术

Design of high efficiency and high thrust grid system for ion thruster

Published:2017-08-09 Issue:17 Volume:31 Page:1816-1825
ISSN:0920-5071
Container-title:Journal of Electromagnetic Waves and Applications
language:en
Short-container-title:Journal of Electromagnetic Waves and Applications

Author:

Rahaman S. E.¹,Barik R. K.²³,Singh A. K.²³,Shukla S. K.²³,Min S.-H.⁴⁵⁶,Park G.-S.⁴⁷

Affiliation:

1. Department of Physics, The University of Burdwan, Burdwan, India

2. Academy of Scientific & Innovative Research (AcSIR), New Delhi, India

3. CSIR-Central Electronics Engineering Research Institute, Pilani, India

4. Department of Physics and Astronomy, Seoul National University, Seoul, South Korea

5. Department of Electrical Engineering and Computer Sciences, Seoul National University, Seoul, South Korea

6. Division of Heavy-Ion Clinical Researches, Korea Heavy Ion Medical Accelerator Project, Korea Institute of Radiological and Medical Science, Seoul, South Korea

7. Seoul-Teracom, Inc., Seoul, South Korea

Publisher

Informa UK Limited

Subject

Electrical and Electronic Engineering,General Physics and Astronomy,Electronic, Optical and Magnetic Materials

Link

https://www.tandfonline.com/doi/pdf/10.1080/09205071.2017.1349002

Reference13 articles.

1. Experimental Investigation of Discharge Plasma Magnetic Confinement in the NSTAR Ion Thruster

2. Prototype design and manufacturing method of an 8 cm diameter RF ion thruster

3. Wang J, Polk J, Brinza D. Ion thruster modeling: particle simulations and experimental validations” Blacksburg (VA); Pasadena (CA): Virginia Polytechnic Institute and State University; USA Jet Propulsion Laboratory; 2003.

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