Thruster injector faceplate testing in support of the aerojet rocket-based combined cycle (RBCC) concept /

Bibliographic Details

Main Author:	Fazah, M. M. (Author)
Format:	Government Document eBook
Language:	English
Published:	Huntsville, Alabama : National Aeronautics and Space Administration, Marshall Space Flight Center, May 1998.
Series:	NASA technical memorandum ; 1998-208194.
Subjects:	Injectors. Gas-gas interactions. Rocket engines. Firing (igniting) Engine tests. Test firing. Rocket firing. Fuel combustion. Propellant combustion. Hydrogen fuels.
Online Access:	https://purl.fdlp.gov/GPO/gpo83111