Combustor performance with various hydrogen-oxygen injection methods in a 200-pound-thrust rocket engine

Author:	Heidmann, M. F.
Year:	1958
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-E58E21
Link:	https://digital.library.unt.edu/ark:/67531/metadc64263/