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Theoretical performance of liquid hydrogen and liquid fluorine as a rocket propellant for a chamber pressure of 600 pounds per square inch absolute
Author:
Fortini, Anthony
Year:
1957
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-E56L10a
Link:
https://digital.library.unt.edu/ark:/67531/metadc63260/
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