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Space Shuttle wind tunnel testing programA major phase of the Space Shuttle Vehicle (SSV) Development Program was the acquisition of data through the space shuttle wind tunnel testing program. It became obvious that the large number of configuration/environment combinations would necessitate an extremely large wind tunnel testing program. To make the most efficient use of available test facilities and to assist the prime contractor for orbiter design and space shuttle vehicle integration, a unique management plan was devised for the design and development phase. The space shuttle program is reviewed together with the evolutional development of the shuttle configuration. The wind tunnel testing rationale and the associated test program management plan and its overall results is reviewed. Information is given for the various facilities and models used within this program. A unique posttest documentation procedure and a summary of the types of test per disciplines, per facility, and per model are presented with detailed listing of the posttest documentation.
Document ID
19850002819
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Reference Publication (RP)
Authors
Whitnah, A. M.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Hillje, E. R.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Date Acquired
September 5, 2013
Publication Date
November 1, 1984
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NAS 1.61:1125
S-535
NASA-RP-1125
Report Number: NAS 1.61:1125
Report Number: S-535
Report Number: NASA-RP-1125
Accession Number
85N11127
Funding Number(s)
PROJECT: RTOP 953-36-00
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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