4010 柔軟構造エアロシェルによる低弾道係数型大気突入システムに関する研究(S67-1 大気突入・減速技術(1),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

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A Low-ballistic-coefficient atmospheric-entry technology using a flexible aeroshell is promising for a space transportation system in next generation because it can reduce the maximum aerodynamic heating during a re-entry and the terminal velocity dramatically. Its technology will lead to realize a safer, cheaper and more universal space transportation system. Our group has researched various important subjects in order to apply the flexible aeroshell to actual atmospheric-entry missions. In this paper, the innovative re-entry system from LEO which was defined as the nominal mission by our group is introduced and our current research and development are reported.
社団法人日本機械学会の論文
2008-08-02