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Cooldown characteristics of regenerative nozzle used in full-scale, cold-flow, nuclear rocket test facilityTransient pressure drop and heat transfer characteristics of regeneratively cooled nozzle assembly used in full scale, cold flow nuclear rocket test facility
Document ID
19670015289
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Cox, E. (NASA Lewis Research Center Cleveland, OH, United States)
Turney, G. E. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
May 1, 1967
Subject Category
Facilities, Research, And Support
Report/Patent Number
NASA-TN-D-3931
Accession Number
67N24618
Funding Number(s)
CONTRACT_GRANT: 122-29-01-07-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
REGENERATIVE COOLING
NUCLEAR ROCKET
PRESSURE DROP
ROCKET NOZZLE
HEAT TRANSFER

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