LEO debris environment modeling in Japan

Tomohiro Narumi, Toshiya Hanada, Satomi Kawamoto, Seishiro Kibe

研究成果: Chapter in Book/Report/Conference proceedingConference contribution

抄録

This paper introduces the current status of an orbital debris evolutionary model for low Earth orbit, named LEODEEM and being developed under collaboration of Japan Aerospace Exploration Agency. The objective of low Earth orbit modeling is to discuss on effective mitigation measures to conserve orbital environment since study and long term prediction of orbital debris environment are urgent needs for secure human space development and exploration. In this model, an object with a perigee altitude less than 2,000 km is considered as a low Earth orbit object. The model calculates long-term evolution of artificial objects greater than 1 cm in low Earth orbit with future space operations, including collisions and explosions. The details of the model and results will be presented in this paper.

本文言語英語
ホスト出版物のタイトルAIAA 57th International Astronautical Congress, IAC 2006
出版社American Institute of Aeronautics and Astronautics Inc.
ページ3777-3782
ページ数6
ISBN(印刷版)9781605600390
DOI
出版ステータス出版済み - 1 1 2006
イベントAIAA 57th International Astronautical Congress, IAC 2006 - Valencia, スペイン
継続期間: 10 2 200610 6 2006

出版物シリーズ

名前AIAA 57th International Astronautical Congress, IAC 2006
6

その他

その他AIAA 57th International Astronautical Congress, IAC 2006
Countryスペイン
CityValencia
Period10/2/0610/6/06

All Science Journal Classification (ASJC) codes

  • Space and Planetary Science
  • Aerospace Engineering

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