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/

< New search