Plume impingement during separation of a two stage space shuttle vehicle
Optimum separation trajectory analysis for two stage space shuttle configuration considering plume impingement effect
Fossler, I.↗
Engineering topics
Publications and source records attributed to Prozan, R..
Optimum separation trajectory analysis for two stage space shuttle configuration considering plume impingement effect
Liquid rocket propellant engine exhaust plume flow field, discussing mathematical models for combustion chamber, throat region and nozzle
Liquid rocket propellant engine exhaust plume flow field, discussing mathematical models for combustion chamber, throat region and nozzle