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Comparison of experimental and kinetically limited theoretical performance of the hydrogen-fluorine propellant systemTheoretical calculations of hydrogen-fluorine rocket engine performance
Document ID
19660025362
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Bittker, D. A. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1966
Subject Category
Propellants
Report/Patent Number
NASA-TN-D-3607
Report Number: NASA-TN-D-3607
Accession Number
66N34652
Funding Number(s)
CONTRACT_GRANT: 129-01-02-01-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ROCKET ENGINE
FLUORINE
HYDROGEN FUEL

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