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PERIGEE PROPULSION FOR ORBITAL LAUNCH OF NUCLEAR ROCKETSPerigee propulsion for orbital launch of nuclear rockets
Document ID
19630001905
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Report (TR)
Authors
Johnson, P. G. (NASA Lewis Research Center Cleveland, OH, United States)
Rom, F. E. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1962
Subject Category
Propellants
Report/Patent Number
NASA-TR-R-140
Report Number: NASA-TR-R-140
Accession Number
63N11781
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
NUCLEAR ROCKET
PROPULSION
PERIGEE
ORBITAL LAUNCH

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