年次大会講演論文集
Online ISSN : 2433-1325
セッションID: 1031
会議情報
1031 月探査機の着陸時における接触力学実験解析(S90 高速飛翔体発生装置とその応用,S90 高速飛翔体発生装置とその応用)
能見 公博原田 勇宮原 啓
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会議録・要旨集 フリー

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抄録
This frictional force is horizontal power to receive from sand. It is not drag received from the sand done by moon soft landing design of experiment [1]. In the beginning the power that lunar lander receives from sand in the surface of the moon and the amount of the cave-in to sand are confirmed with an experimental apparatus, and the influence received from sand is understood in the beginning. The analysis of the behavior when the lunar lander lands on the moon uses the mechanical analysis software named ADAMS. The coefficient of friction used at that time refers to the numerical value obtained from the experiment.
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© 2006 一般社団法人日本機械学会
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