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Description and operating parameters of a Mach 2 nozzle system for the Langley 11-inch ceramic-heated tunnelDescription and operating parameters of Mach 2 nozzle system for 11-inch ceramic heated wind tunnel
Document ID
19680023718
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Sutton, K.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
September 1, 1968
Subject Category
Facilities, Research, And Support
Report/Patent Number
NASA-TN-D-4750
Accession Number
68N33190
Funding Number(s)
CONTRACT_GRANT: 129-03-02-03-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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