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Aerodynamic results of a separation effects test (IA87) on a 0.01-scale model (52-OTS) of the integrated SSV in the AEDC/VKF 40-by-40 inch supersonic wind tunnel A, volume 2Data tables, model figures, and tabulated source data are given for aerodynamic investigations of separation effects in the integrated space shuttle vehicle. For Volume 1, see N75-28101.
Document ID
19750022161
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Campbell, J. H., II (Rockwell Intern. Corp. Downey, Calif., United States)
Date Acquired
September 3, 2013
Publication Date
June 1, 1975
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
DMS-DR-2192-VOL-2
NASA-CR-141542
Report Number: DMS-DR-2192-VOL-2
Report Number: NASA-CR-141542
Accession Number
75N30234
Funding Number(s)
CONTRACT_GRANT: NAS9-13247
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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