Hall Thruster Development for Japanese Space Propulsion Programs-Reference-Cited by-同舟云学术

Hall Thruster Development for Japanese Space Propulsion Programs

Published:2017 Issue:5 Volume:60 Page:320-326
ISSN:0549-3811
Container-title:TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
language:en
Short-container-title:Trans. Japan Soc. Aero. S Sci.

Author:

HAMADA Yushi¹,BAK Junhwi¹,KAWASHIMA Rei¹,KOIZUMI Hiroyuki¹,KOMURASAKI Kimiya¹,YAMAMOTO Naoji²,EGAWA Yusuke²,FUNAKI Ikkoh³,IIHARA Shigeyasu⁴,CHO Shinatora⁵,KUBOTA Kenichi⁵,WATANABE Hiroki⁶,FUCHIGAMI Kenji⁷,TASHIRO Yosuke⁴,TAKAHATA Yuya⁸,KAKUMA Tetsuo⁸,FURUKUBO Yusuke⁸,TAHARA Hirokazu⁸

Affiliation:

1. Department of Aeronautics and Astronautics, The University of Tokyo

2. Department of Advanced Energy Engineering Science, Kyushu University

3. Institute of Space and Astronautical Science, JAXA

4. IHI Aerospace Co., Ltd.

5. Research and Development Directorate, JAXA

6. Department of Aerospace Engineering, Tokyo Metropolitan University

7. IHI Corporation

8. Department of Aeronautics and Astronautics, Osaka Institute of Technology

Publisher

Japan Society for Aeronautical and Space Sciences

Subject

Space and Planetary Science,Aerospace Engineering

Link

https://www.jstage.jst.go.jp/article/tjsass/60/5/60_T-16-49/_pdf

Reference46 articles.

1. 1) Juno/NASA, http://www.nasa.gov/mission_pages/juno/main/index.html (accessed 7 June 2016).

2. 2) Boeing: World's First All-Electric Propulsion Satellite Begins Operations, http://boeing.mediaroom.com/2015-09-10-Boeing-World-s-First-All-Electric-Propulsion-Satellite-Begins-Operations (accessed 7 June 2016).

3. 3) Florenz, R. E.: The X3 100-kW Class Nested-Channel Hall Thruster: Motivation, Implementation, and Initial Performance, Ph.D. Thesis, University of Michigan, 2013.

4. 4) Soulas, G., Haag, T., Herman, D., Huang, W., Kamhawi, H., and Shastry, R.: Performance Test Results of the NASA-457M v2 Hall Thruster, AIAA 2012-3940, 2012.

5. 5) Semenkin, A. V., Zakharenkov, L. E., and Soldukhin, A. E.: Feasibility of High Power Multi-Mode EPS Development Based on the Thruster with Anode Layer, IEPC 2011-064, 2011.

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