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Aerodynamic Characteristics of a Proposed Personnel Launch System (PLS) Lifting-Body Configuration at Mach Numbers from 0.05 to 20.3. SupplementA wind-tunnel investigation was performed to determine the aerodynamic characteristics of a proposed lifting-body personnel launch system (PLS) configuration over a Mach range of 0.05 to 20.3. The test configuration had a low-aspect-ratio body with a flat undersurface and three fins on the upper aft body. Data are presented with a minimum of analysis. All of the experimental data were placed in a structured data base using the R:BASE system. This is the CD-ROM that is available for this report.
Document ID
20090005242
Acquisition Source
Langley Research Center
Document Type
Other - Numeric Database
Authors
Cruz, Christopher I.
(NASA Langley Research Center Hampton, VA, United States)
Ware, George M.
(NASA Langley Research Center Hampton, VA, United States)
Grafton, Sue B.
(NASA Langley Research Center Hampton, VA, United States)
Woods, William C.
(NASA Langley Research Center Hampton, VA, United States)
Young, James C.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 24, 2013
Publication Date
November 1, 1989
Subject Category
Space Transportation And Safety
Report/Patent Number
NASA-TM-101651
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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