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

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

McRonald, A.
URI: http://hdl.handle.net/2014/13753
Date: 2000-01-23
Citation: AAS/AIAA Space Flight Mechanics Meeting
Clearwater, Florida, USA

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.

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