NASA NTRS · 19660022898
Design and cooling performance of a dump- cooled rocket engine
Abstract
Design and evaluation of liquid hydrogen cooled rocket engine for determining minimum satisfactory coolant flow
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Curley, J. K., Masters, P. A., Pavli, A. J., Schwartz, R. M.. 1966-08-01. Design and cooling performance of a dump- cooled rocket engine. https://ntrs.nasa.gov/citations/19660022898
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