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

Description
Item Description:	Title from title screen (viewed April 20, 2016). "Prepared for the 32nd Joint Propulsion Conference cosponsored by AIAA, ASME, SAE, and ASEE, Lake Buena Vista, Florida, July 1-3, 1996." "Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.
Physical Description:	1 online resource (11 pages) : illustrations.
Bibliography:	Includes bibliographical references (pages 4-5).