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Thermodynamic Extrapolation of Rocket Performance ParametersThermodynamically defined rocket performance parameters
Document ID
19620006858
Document Type
Reprint (Version printed in journal)
Authors
Gordon, S. (NASA Lewis Research Center Cleveland, OH, United States)
Zeleznik, F. J. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 1, 2013
Publication Date
August 1, 1962
Publication Information
Publication: American Rocket Society Journal
Volume: 32
Issue: 8
Subject Category
Nuclear Engineering
Accession Number
62N16858
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
ROCKET
THERMODYNAMICS
PROPELLANT

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