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/ |