Regenerative-cooling studies in a 5000-pound-thrust liquid-oxygen - JP-4 rocket engine operated at 6000-pounds-per-square-inch combustion-chamber pressure

Author:	Tischler, Adelbert O.
Year:	1956
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-E56B02
Link:	https://digital.library.unt.edu/ark:/67531/metadc62477/