年次大会講演論文集
Online ISSN : 2433-1325
セッションID: S1904-2-2
会議情報
S1904-2-2 はやぶさカプセルの再突入飛行と回収オペレーション(大気突入・減速技術(2),社会変革を技術で廻す機械工学)
山田 哲哉山田 和彦國中 均川口 淳一郎
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会議録・要旨集 認証あり

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Hayabusa Sample Return Capsule (SRC) has accomplished reentry flight directly from the interplanetary-transfer orbit with velocity of about 12 km/s and successfully recovered on June 14, 2010. The SRC is considered to deploy parachute at the altitude of 5 km as planned, while the chute-trigger timer has been carefully set to cover contingency cases due to malfunctions of triggering devises taking account of dispersions of orbital and atmospheric density and errors in the aerodynamic coefficients. All the components separated at the chute-deployment were searched-out based on the landing position of the instrument module.

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