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Results of a Pressure Loads Investigation on a 0.030-scale Model (47-OTS) of the Integrated Space Shuttle Vehicle Configuration 5 in the NASA Ames Research Center 11 x 11 Foot Leg of the Unitary Plan Wind Tunnel (IA81A), Volume 7Tabulated pressure data are presented on the external tank and miscellaneous orifices of the integrated space shuttle vehicle configuration. For Vol. 1, see N76-15246.
Document ID
19760008164
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Chee, E. (Rockwell Intern. Corp. Downey, Calif., United States)
Date Acquired
September 3, 2013
Publication Date
November 1, 1975
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-CR-141842
DMS-DR-2169-VOL-7
Report Number: NASA-CR-141842
Report Number: DMS-DR-2169-VOL-7
Accession Number
76N15252
Funding Number(s)
CONTRACT_GRANT: NAS9-13247
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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