Development of orbital debris environment model in the Low Earth Orbit

Kengo Uramoto, Toshiya Hanada

研究成果: ジャーナルへの寄稿Conference article

抄録

LEODEEM (Kyushu University Low Earth Orbit orbital debris environment evolution model) is being based on "particle in a box" concept. This indicates mathematics model predicting the characteristic of LEO debris environment. LEODEEM provide a mathematical description of distribution of objects in the LEO, understanding of the space debris accumulation mechanism in LEO, analysis of the effectiveness of debris mitigation measures. This paper will report the current status of LEODEEM development.

元の言語英語
ページ(範囲)927-938
ページ数12
ジャーナルAdvances in the Astronautical Sciences
117
出版物ステータス出版済み - 12 1 2004
イベント10th International Conference of Pacific Basin Societies, ISCOPS - Tokyo, 日本
継続期間: 12 10 200312 12 2003

Fingerprint

Debris
Orbits
Earth (planet)
space debris
Space debris
mathematics

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Space and Planetary Science

これを引用

Development of orbital debris environment model in the Low Earth Orbit. / Uramoto, Kengo; Hanada, Toshiya.

:: Advances in the Astronautical Sciences, 巻 117, 01.12.2004, p. 927-938.

研究成果: ジャーナルへの寄稿Conference article

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