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Aircraft Configured for Flight in an Atmosphere Having Low DensityAn aircraft is configured for flight in an atmosphere having a low density. The aircraft includes a fuselage, a pair of wings, and a rear stabilizer. The pair of wings extends from the fuselage in opposition to one another. The rear stabilizer extends from the fuselage in spaced relationship to the pair of wings. The fuselage, the wings, and the rear stabilizer each present an upper surface opposing a lower surface. The upper and lower surfaces have X, Y, and Z coordinates that are configured for flight in an atmosphere having low density.
Document ID
20120010544
Acquisition Source
Headquarters
Document Type
Other - Patent
Authors
Croom, Mark A.
Smith, Stephen C.
Gelhausen, Paul A.
Guynn, Mark D.
Hunter, Craig A.
Paddock, David A.
Riddick, Steven E.
Teter, Jr., John E.
Date Acquired
August 26, 2013
Publication Date
June 12, 2012
Subject Category
Aircraft Design, Testing And Performance
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-8,196,858|NASA-Case- LAR-17514-1
Patent Application
US-Patent-Appl-SN-12/721,833

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