ホールスラスタの地上試験におけるチャンバ背圧影響に関する数値感度解析

• 張 科寅

  連絡先著者（Corresponding author） ：[e-mail] 宇宙航空研究開発機構

• 渡邊 裕樹

  首都大学東京

• 窪田 健一

  宇宙航空研究開発機構

• 船木 一幸

  宇宙航空研究開発機構

書誌事項

タイトル別名

• Numerical Sensitivity Analysis of Chamber Backpressure Effect in Hall Thruster Experiment
• ホールスラスタ ノ チジョウ シケン ニ オケル チャンバ ハイアツ エイキョウ ニ カンスル スウチ カンド カイセキ

抄録

Facility backpressure effect remains to be an important unsolved problem for Hall thruster development making it difficult to predict the thruster on-orbit operation precisely. Measurements in previous research shows the backpressure effects can cause unexpectedly-high thrust and discharge current increment in comparison with the theory. In this study, backpressure effects were investigated by sensitivity analysis using Particle-In-Cell plasma simulation. Not only static pressure but also dynamic pressure, or the velocity of background gas flow, were parameterized. The results show that if dynamic pressure exists, > 10% increment of thrust and current can be observed even if the recommended pressure criteria for Hall thruster measurement is satisfied. It is thus suggested that the dynamic pressure of background gas could be one of the main reason of the backpressure-effect issue. The primary cause of the thrust/current increment is identified to be the flux of ingested background gas. It is also observed in the simulation that the channel wall volume erosion rate also increases linearly with the ingested flux.

収録刊行物

• 日本航空宇宙学会論文集

  日本航空宇宙学会論文集 66 (3), 61-68, 2018

  一般社団法人 日本航空宇宙学会

キーワード

• Hall Thruster
• Facility Pressure Effect
• Numerical Simulation
• Particle-In-Cell

詳細情報

• CRID: 1390282763013157248
• NII論文ID: 130007384385
• NII書誌ID: AA11307372
• DOI: 10.2322/jjsass.66.61
• ISSN: 24323691
• ISSN: 13446460
• NDL書誌ID: 029103380
• Web Site: https://ndlsearch.ndl.go.jp/books/R000000004-I029103380
• Web Site: https://www.jstage.jst.go.jp/article/jjsass/66/3/66_66_61/_pdf
• 本文言語コード: ja
• データソース種別:
  • JaLC
  • NDL
  • Crossref
  • CiNii Articles
  • KAKEN
• 抄録ライセンスフラグ: 使用不可