Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure
By: Robert S. Jankovsky and John M. Kazaroff, Albert J. Pavli.
Contributors: Kazaroff, John M.; Pavli, Albert J.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Program.
Series: NASA technical paper -- 3576.
Publisher: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program; National Technical Information Service, distributor
Published: 1996
Place of publication: [Washington, D.C.]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Rocket nozzles.; Exhaust velocity.; Specific impulse.; Nozzle thrust coefficients.; Nozzle geometry.; Thrust chamber pressure.; Nozzle efficiency.; Divergent nozzles.
Other titles: Experimental performance of a high area ratio rocket nozzle at high combustion chamber pressure.
Notes: Shipping list no.: 98-0733-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.