Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure

Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure

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Bibliographic Details
Main Author:	Jankovsky, Robert S
Corporate Author:	United States National Aeronautics and Space Administration. Scientific and Technical Information Program
Other Authors:	Kazaroff, John M, Pavli, Albert J
Format:	Government Document Book
Language:	English
Published:	[Washington, D.C.] : [Springfield, Va. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; National Technical Information Service, distributor, 1996]
Series:	NASA technical paper 3576
Subjects:	Rockets (Aeronautics) > Nozzles Divergent nozzles Exhaust velocity Nozzle efficiency Nozzle geometry Nozzle thrust coefficients Rocket nozzles Specific impulse Thrust chamber pressure
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Stanford University

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Call Number:	ISIL:US-CST NAS 1.60:3576