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Hypersonic aerodynamic characteristics of NR-ATP orbiter, orbiter with external tank, and ascent configurationA scale model of the North American Rockwell ATP Orbiter with and without the external tank has been tested in a 22-inch helium tunnel at Mach 20 and a Reynolds number based on model length, of 2.14 times one million. Longitudinal and lateral-directional data were determined for the orbiter alone while only longitudinal characteristics and elevon roll effectiveness were investigated for the orbiter/tank combination. Oil flow and electron beam flow visualization studies were conducted for the orbiter alone, orbiter with external tank and the ascent configuration.
Document ID
19730013111
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Ashby, G. C., Jr.
(NASA Langley Res. Center)
Date Acquired
September 2, 2013
Publication Date
March 1, 1973
Subject Category
Space Vehicles
Report/Patent Number
DMS-DR-2003
NASA-CR-128754
Report Number: DMS-DR-2003
Report Number: NASA-CR-128754
Accession Number
73N21838
Funding Number(s)
CONTRACT_GRANT: NAS9-13247
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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