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Performance characteristics of the lifting body vehicleDesigners have relied heavily upon aerodynamic theory and wind-tunnel testing of large and small models to obtain accurate estimates of the performance characteristics for a new configuration and to provide a realistic simulation of the vehicle’s flying characteristics before its first flight, However, the highly unusual shapes of the lifting body vehicles have raised some questions of how accurately their lift and drag characteristics could be defined with these prediction techniques. Thus it is pertinent to com- pare the lift and drag data obtained in flight for three lifting body vehicles (ref. 1 and unpublished results) with wind-tunnel measurements obtained on the actual flight vehicles (refs. 2 and 3 and unpublished results) and on small-scale models of the flight vehicles (ref. 4 and unpublished results). These comparisons, together with discussions of separated flow problems and the effects of ablated surfaces, should be useful to the designers of space shuttlecraft.
Document ID
19710000631
Acquisition Source
Headquarters
Document Type
Conference Paper
Authors
Jon S Pyle
(Flight Research Center Rosamond, California, United States)
Lawrence G Ash
(Flight Research Center Rosamond, California, United States)
Date Acquired
August 6, 2013
Publication Date
October 1, 1970
Publication Information
Publication: Flight Test Results Pertaining to the Space Shuttlecraft
Publisher: National Aeronautics and Space Administration
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: NASA Symposium on Flight Test Results Pertaining to the Space Shuttlecraft
Location: Edwards, CA
Country: US
Start Date: June 30, 1970
Sponsors: Flight Research Center
Accession Number
71N10105
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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