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A Light-Weight Inflatable Hypersonic Drag Device for Venus Entry
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A Light-Weight Inflatable Hypersonic Drag Device for Venus Entry
McRonald, A.
URI:
http://hdl.handle.net/2014/17926
Date:
1999-09-16
Citation:
AAS/AIAA, Astrodynamics Conference
Girdwood, Alaska, USA
Abstract:
The author has studied inflatable drag devices for deceleration in the atmosphere of Venus, for both direct aerocapture and for entry from circular orbit.
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JPL TRS 1992+
JPL TRS 1992+
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