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J-GLOBAL ID:201802291398633233   Reference number:18A0416455

Hall Thruster Development for Japanese Space Propulsion Programs

日本の宇宙推進プログラムのためのHallスラスタ開発
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Volume: 60  Issue:Page: 320-326(J-STAGE)  Publication year: 2017 
JST Material Number: U0630A  ISSN: 2189-4205  Document type: Article
Article type: 原著論文  Country of issue: Japan (JPN)  Language: ENGLISH (EN)
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Rocket engines 
Reference (46):
  • 1) Juno/NASA, http://www.nasa.gov/mission_pages/juno/main/index.html (accessed 7 June 2016).
  • 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) 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) 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) 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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