A series of chemical equilibrium, chemical nonequilibrium and thermal nonequilibrium calculations are performed for various chemical processes related to a Single Stage To Orbit Hydrogen Fueled Airbreathing Hypersonic Vehicle (SSTOHFAHV). The processes include air dissociation downstream of a normal shock, 60 and 30 degree oblique shocks and H2-air combustion. The calculations are applied to two typical SSTOHFAHV trajectories.
Chemistry associated with hypersonic vehicles
Chemie in Zusammenhang mit Ueberschallflugzeugen
AIAA-Papers ; Jun ; 1-30
1987
30 Seiten, 31 Bilder, 5 Tabellen, 24 Quellen
Conference paper
English
Chemistry associated with hypersonic vehicles
AIAA | 1987
|Chemistry associated with hypersonic vehicles
AIAA | 1989
|