Magnetic field design in miniature microwave discharge ion engines

Naoji Yamamoto, Takayuki Chikaoka, Shinya Kondo, Hirokazu Masui, Hideki Nakashima, Takao Yoshiyuki

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

The effect of magnetic field configuration on thrust performance in a 30 W class miniature microwave discharge ion engine was investigated with the objective of improving its thrust performance. The ion beam current with various magnitude of magnetic field was measured, since magnetic confinement and microwave - plasma coupling could be affected by the magnetic field configuration. The ion beam current is increased with the increase in the number of magnets and there is an optimum magnitude of magnetic field. The thrust performance of the miniature microwave discharge ion engine, propellant utilization, and ion beam production cost were 0.67 and 660 W/A, respectively at mass flow rate =0.02 mg/s, and incident microwave power= 8 W.

元の言語英語
ホスト出版物のタイトルCollection of Technical Papers - AIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference
ページ8172-8178
ページ数7
出版物ステータス出版済み - 12 1 2006
イベントAIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference - Sacramento, CA, 米国
継続期間: 7 9 20067 12 2006

出版物シリーズ

名前Collection of Technical Papers - AIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference
10

その他

その他AIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference
米国
Sacramento, CA
期間7/9/067/12/06

    フィンガープリント

All Science Journal Classification (ASJC) codes

  • Space and Planetary Science
  • Energy(all)
  • Aerospace Engineering
  • Control and Systems Engineering
  • Electrical and Electronic Engineering
  • Mechanical Engineering

これを引用

Yamamoto, N., Chikaoka, T., Kondo, S., Masui, H., Nakashima, H., & Yoshiyuki, T. (2006). Magnetic field design in miniature microwave discharge ion engines. : Collection of Technical Papers - AIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference (pp. 8172-8178). (Collection of Technical Papers - AIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference; 巻数 10).