Demonstration of wide throttling range ion engines

Naoji Yamamoto, Taichi Morita, Masakatsu Nakano, Yasushi Ohkawa, Ikkoh Funaki

研究成果: 著書/レポートタイプへの貢献会議での発言

1 引用 (Scopus)

抜粋

For demonstration of a wide range throttling ion engine by changing the ion beam extraction duty cycle, time history of ion beam current and neutralizer current were measured using 100 N class miniature ion engine. The ion beam current synchronized with the accel. grid voltage, with repetition frequency of 1 kHz, duty cycle of 0.5. The time integrated emission current from field emission cathode and the time integrated ion beam current are balanced; the neutralization of a wide throttling range ion engine system was successfully demonstrated.

元の言語英語
ホスト出版物のタイトル2018 Joint Propulsion Conference
出版者American Institute of Aeronautics and Astronautics Inc, AIAA
ISBN(印刷物)9781624105708
DOI
出版物ステータス出版済み - 1 1 2018
イベント54th AIAA/SAE/ASEE Joint Propulsion Conference, 2018 - Cincinnati, 米国
継続期間: 7 9 20187 11 2018

出版物シリーズ

名前2018 Joint Propulsion Conference

会議

会議54th AIAA/SAE/ASEE Joint Propulsion Conference, 2018
米国
Cincinnati
期間7/9/187/11/18

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Control and Systems Engineering

フィンガープリント Demonstration of wide throttling range ion engines' の研究トピックを掘り下げます。これらはともに一意のフィンガープリントを構成します。

  • これを引用

    Yamamoto, N., Morita, T., Nakano, M., Ohkawa, Y., & Funaki, I. (2018). Demonstration of wide throttling range ion engines. : 2018 Joint Propulsion Conference [AIAA 2018-4815] (2018 Joint Propulsion Conference). American Institute of Aeronautics and Astronautics Inc, AIAA. https://doi.org/10.2514/6.2018-4815