ＭＵＳＥＳ‐Ｃ搭載高電圧太陽電池のプラズマ干渉

• 趙 孟佑

  九州工業大学

• 白石 康

  九州工業大学

• 匹田 政幸

  九州工業大学

• 國中 均

  宇宙科学研究所

書誌事項

タイトル別名

• Plasma Interaction of High Voltage Solar Arrays for MUSES-C.
• MUSES-C搭載高電圧太陽電池のプラズマ干渉
• MUSES C トウサイ コウデンアツ タイヨウ デンチ ノ プラズマ カンショウ

抄録

MUSES-C is an interplanetary spacecraft which will be launched in 2002 with the mission for the sample return from an asteroid. MUSES-C has high voltage solar arrays operating at 120 V and Xe ion thruster system as the main propulsion system. Plasma interaction between the backflow plasma from the ion thruster plume and the solar array is investigated by computer simulation and laboratory experiments. The plasma density near the solar arrays is expected to be 10¹¹ m^-3∼10¹³ m^-3. Due to the operation of ion thruster neutralizer, the solar array has a positive potential with respect to the plasma. The increase of electron current to the solar array, however, may drop the array potential. Once the array potential becomes negative, arcing is observed to occur even at the voltage of −120 V. Several methods to suppress the plasma interaction are proposed.

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 49 (571), 268-277, 2001

  一般社団法人 日本航空宇宙学会

キーワード

• Energy
• Solar Array
• High Voltage
• Arcnig
• Ion Thruster
• Plasma Interaction

詳細情報

• CRID: 1390001204470096896
• NII論文ID: 10006467839
• NII書誌ID: AA11307372
• DOI: 10.2322/jjsass.49.268
• ISSN: 24323691
• ISSN: 13446460
• NDL書誌ID: 5884157
• Web Site: https://ndlsearch.ndl.go.jp/books/R000000004-I5884157
• Web Site: https://www.jstage.jst.go.jp/article/jjsass/49/571/49_571_268/_pdf
• 本文言語コード: ja
• データソース種別:
  • JaLC
  • NDL
  • Crossref
  • CiNii Articles
• 抄録ライセンスフラグ: 使用不可