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Studies of airframe propulsion system integration for Mach 6 cruise vehiclesAirframe-propulsion system integration for hypersonic aircraft
Document ID
19670029519
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Cubbage, J. M., Jr. (NASA Langley Research Center Hampton, VA, United States)
Kirkham, F. S. (NASA Langley Research Center Hampton, VA, United States)
Small, W. J. (NASA Langley Research Center Hampton, VA, United States)
Vahl, W. A. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1967
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-4128
Report Number: NASA-TN-D-4128
Accession Number
67N38848
Funding Number(s)
CONTRACT_GRANT: 126-13-03-31-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
PROPULSION CONFIGURATION
RAMJET ENGINE
HYPERSONIC AIRCRAFT
INTEGRATION
AIRFRAME

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