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FEASIBILITY OF OPTIMIZING NOZZLE PERFORMANCE FOR ORBITALLAUNCH NUCLEAR ROCKETSFeasibility of optimizing nozzle performance for orbital-launch nuclear rockets
Document ID
19630004375
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Jack, J. R.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1963
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-1578
Report Number: NASA-TN-D-1578
Accession Number
63N14251
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ROCKET NOZZLE
NUCLEAR ROCKET
ORBITAL LAUNCH
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