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Exploratory study of performance of the Langley pilot model expansion tube with a hydrogen driverExpansion tube for simulating hypervelocity flow conditions for reentry vehicles
Document ID
19660015871
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Jones, J. J. (NASA Langley Research Center Hampton, VA, United States)
Moore, J. A. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1966
Subject Category
Facilities, Research, And Support
Report/Patent Number
NASA-TN-D-3421
Report Number: NASA-TN-D-3421
Accession Number
66N25160
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
HYPERSONIC FLOW
FLOW VELOCITY
REENTRY VEHICLE

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