Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)
Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)
Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)
Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)
Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)
Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)
Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA)
出版者
宇宙航空研究開発機構(JAXA)
出版者（英）
Japan Aerospace Exploration Agency (JAXA)
雑誌名
宇宙航空研究開発機構特別資料: 第7回スペースデブリワークショップ講演資料集
雑誌名(英)
JAXA Special Publication: Proceedings of the 7th Space Debris Workshop
Low cost development of active debris removal (ADR) systems is required to realize the sustainable debris remediation strategy. An electrodynamic tether (EDT) is a promising candidate for the deorbit propulsion device of the ADR systems because of its advantages such as the absence of consumables, the absence of thrust vectoring, and the easy attachment to debris. In this presentation, the pros and cons of the EDT, its development scenario and technological issues for the ADR application are to be described.
内容記述
形態: カラー図版あり
内容記述（英）
Physical characteristics: Original contains color illustrations
Toward the application of electrodynamic tether systems to orbital debris deorbit
AA1630052023.pdf
(3.34MB)
