花田 俊也
平山 寛
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【 研究概要 】
To deal with the orbital debris issues that threats safety in space, orbital debris evolutionary models have been built by incorporation of laws of astrodynamics and empirical assumptions. The assumptions have been augmented and verified by a series of laboratory satellite impact tests. This work not only deals the world-wide effort to predict orbital environment but it also provides a novel tool to identify effective procedures of orbital environment protection.
【 関連キーワード 】
Impact Fragmentation
| Orbital Debris
| Space Environment
| 宇宙環境
| 宇宙ゴミ
| 衝突破壊
【 関連URL 】
 http://ssdl.aero.kyushu-u.ac.jp/?SpaceDebris
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