Development of orbital debris environment model in the Low Earth Orbit

Kengo Uramoto, Toshiya Hanada

Research output: Contribution to journalConference article

Abstract

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.

Original languageEnglish
Pages (from-to)927-938
Number of pages12
JournalAdvances in the Astronautical Sciences
Volume117
Publication statusPublished - Dec 1 2004
Event10th International Conference of Pacific Basin Societies, ISCOPS - Tokyo, Japan
Duration: Dec 10 2003Dec 12 2003

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Space and Planetary Science

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