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A Light-Weight Hypersonic Inflatable Drag Device for a Neptune Orbiter

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dc.contributor.author McRonald, A. en_US
dc.date.accessioned 2004-09-23T17:22:00Z
dc.date.available 2004-09-23T17:22:00Z
dc.date.issued 2000-01-23 en_US
dc.identifier.citation AAS/AIAA Space Flight Mechanics Meeting en_US
dc.identifier.citation Clearwater, Florida, USA en_US
dc.identifier.clearanceno 00-0123 en_US
dc.identifier.uri http://hdl.handle.net/2014/13753
dc.description.abstract The author will discuss presently available ballute materials and a development program of aerodynamic tests and materials that would be requried for ballutes to achieve their full potential. en_US
dc.format.extent 890371 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other inflatable hypersonic Drag aerocapture Neptune Orbiter ballutes en_US
dc.title A Light-Weight Hypersonic Inflatable Drag Device for a Neptune Orbiter en_US


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