A performance comparison of two small rocket nozzles /

Bibliographic Details

Main Authors:	Arrington, Lynn A. (Author), Reed, Brian D. (Author), Rivera, Angel (Author)
Corporate Author:	United States. National Aeronautics and Space Administration (sponsoring body.)
Format:	Government Document eBook
Language:	English
Published:	Cleveland, Ohio : National Aeronautics and Space Administration, Lewis Research Center, August 1996.
Series:	NASA technical memorandum ; 107285.
Subjects:	Conical nozzles. Rocket thrust. Rocket nozzles. Nozzle design. Reynolds number. Thrust chamber pressure. Film cooling.
Online Access:	https://purl.fdlp.gov/GPO/gpo67112