Arguments are presented for the retention of vibrational equilibrium of species in the nozzle of the Space Shuttle Main Engine which are especially applicable to water and the hydroxyl radical. It is shown that the reaction OH + HH yields HOH + H maintains equilibrium as well. This is used to relate OH to H, the temperature, and the oxidizer-to-fuel ratio.
Equilibrium Retention in the Nozzle of Oxygen Hydrogen Propulsion Systems
1987
26 pages
Report
No indication
English
Engineering Index Backfile | 1934
Hydrogen-oxygen for rocket propulsion.
NTRS | 1964
|Hydrogen/Oxygen Auxiliary Propulsion Technology
NTIS | 1991
|Hydrogen/oxygen auxiliary propulsion technology
AIAA | 1991
|