Orbital Debris Modeling at Kyushu University

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概要

• 論文の詳細を見る

• Orbital debris modeling at Kyushu University was initiated with satellite impact testing, aiming to investigate low-velocity impact phenomena possible in the geosynchronous Earth orbit. Testing results were incorporated in an orbital debris evolutionary model for the geosynchronous Earth orbit region, named GEODEEM. Kyushu University also has developed an orbital debris evolutionary model for the low Earth orbit, named LEODEEM. The orbital debris evolutionary models are an essential tool to predict the future orbital debris environment and to discuss on what and how to do for orbital debris mitigation. This paper will briefly introduce orbital debris modeling being conducted at Kyushu University.

• 特定非営利活動法人　日本ロケット協会の論文

著者

• HANADA Toshiya

  Kyushu Univ.

• MURAKAMI Junko

  Kyushu University

• ARIYOSHI Yuya

  Kyushu University

• MIYAZAKI Kazuki

  Kyushu University

• MANIWA Kazuaki

  Kyushu University

• KAWAMOTO Satomi

  Japan Aerospace Exploration Agency

関連論文

• A FLIGHT EXPERIMENT OF ELECTRODYNAMIC TETHER USING A SMALL SATELLITE : AS THE FIRST STEP FOR DEBRIS REMOVAL
• Orbital Debris Modeling at Kyushu University
• A Flight Experiment of Electrodynamic Tether using a Small Satellite: as the First Step for Debris Removal

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