Microsatellite impact tests to investigate the outcome of satellite fragmentations

Junko Murakami, Toshiya Hanada, J. C. Liou

研究成果: Contribution to journalArticle査読

3 被引用数 (Scopus)

抄録

To predict the future orbital environments, it is necessary to know outcome of the satellite fragmentation. The NASA standard breakup model is designed to describe the outcome of typical satellite fragmentation. This model is an empirical model and the major data sources are the 1980s on-orbit satellite breakup events and the ground-based Satellite Orbit Debris Characterization Impact Test series conducted in early 1990s. The target cubic satellites ranged from 15 to 20 cm in size and about 1000 g in mass. Results from all seven impact tests carried out in 2008 are shown in this paper and compared with the NASA standard breakup model to demonstrate potential improvements of the model in the future.

本文言語英語
ページ(範囲)208-212
ページ数5
ジャーナルJournal of Spacecraft and Rockets
48
1
DOI
出版ステータス出版済み - 2011

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering
  • Space and Planetary Science

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