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A Light-Weight Hypersonic Inflatable Drag Device for a Neptune OrbiterThe 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.
Document ID
20210002294
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other
External Source(s)
hdl:2014/13753
Authors
McRonald, A.
Date Acquired
January 23, 2000
Publication Date
January 23, 2000
Publication Information
Publisher: UNKNOWN
Distribution Limits
Public
Copyright
Other
Technical Review
Keywords
inflatable
hypersonic
Drag
aerocapture
Neptune
Orbiter
ballutes

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