Propellant vaporization as a criterion for rocket engine design : relation between percentage of propellant vaporized and engine performance

Author:	Heidmann, Marcus F
Year:	1958
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-4219
Link:	https://digital.library.unt.edu/ark:/67531/metadc57168/