Combustion performance and heat transfer characterization of lox/hydrocarbon type propellants : final report, volume II.

Bibliographic Details

Corporate Author:	Aerojet-General Corporation. Liquid Rocket Plant
Format:	Government Document eBook
Language:	English
Published:	Houston, Texas : National Aeronautics and Space Administration, Lyndon B. Johnson Space Center, September 1983.
Series:	NASA contractor report ; NASA CR-171714.
Subjects:	Heat transfer. Performance prediction. Thermal stability. Pressure gradients. Injectors.
Online Access:	https://purl.fdlp.gov/GPO/gpo106664