4016 小型成層圏気球を利用したインフレータブル型柔構造飛翔体の飛行実験計画(S67-2 大気突入・減速技術(2),21世紀地球環境革命の機械工学:人・マイクロナノ・エネルギー・環境)

概要

論文の詳細を見る
A low ballistic coefficient vehicle can drastically reduce peak aerodynamic heating during atmospheric entry. We are developing the new atmospheric entry system using an inflatable flexible aeroshell. A fight test of the system, which is aiming to verify the design method of the inflatable flexible aeroshell, is planned for late August, FY2008. The flight test is performed by stratospheric balloon-drop from altitude of about 30 km. In this paper, the system configuration and the operation sequence of this experiment system are overviewed.
社団法人日本機械学会の論文
2008-08-02