Validation of high aspect ratio cooling in a 89 kN (20,000 lbf) thrust combustion chamber /

Bibliographic Details

Main Authors:	Wadel, Mary F. (Author), Meyer, Michael L. (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, June 1996.
Series:	NASA technical memorandum ; 107270.
Subjects:	Rocket engines. Combustion chambers. Thrust chambers. Mass flow. Liquid hydrogen. Cooling. High aspect ratio. Performance tests.
Online Access:	https://purl.fdlp.gov/GPO/gpo69478