Cover Image

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
Description
Item Description:Title from title screen (viewed July 19, 2016).
"June 1996"--Report documentation page.
"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.
"AIAA-96-2584."
Physical Description:1 online resource (10 pages) : illustrations.
Bibliography:Includes bibliographical references (page 10).