Browsing Space Systems Design Lab (SSDL) by Subject "Hypersonic flight"
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Static Aeroelastic Analysis of a Thin-Film Clamped Ballute for Titan Aerocapture
(Georgia Institute of Technology, 2006-05)Many authors have shown the potential mass savings that a ballute can offer for both aerocapture and entry. This mass savings could enhance or even enable many scientific and human exploration missions. Prior to flight ...