Combustion performance and heat transfer characterization of LOX/hydrocarbon type propellants : final report, volume 1 /

Bibliographic Details

Main Author:	Michel, R. W.
Corporate Author:	United States. National Aeronautics and Space Administration
Format:	Government Document Book
Language:	English
Published:	Sacramento, Calif. : Aerojet Liquid Rocket Company, [1983]
Series:	NASA contractor report ; NASA CR-171713.
Subjects:	Cryogenic rocket propellants. Liquid oxygen. Oxygen-hydrocarbon rocket engines. Space shuttles.