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

An edition of Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure (1996)

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

By Robert S. Jankovsky

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Publish Date

1996

Publisher

National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program,National Technical Information Service, distributor

Language

eng

Pages

Description:

subjects: Thrust chamber pressure, Exhaust velocity, Divergent nozzles, Specific impulse, Nozzle geometry, Nozzle thrust coefficients, Nozzle efficiency, Rocket nozzles