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A Light-Weight Inflatable Hypersonic Drag Device for Venus Entry

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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