1AE6450 Rocket PropulsionInjector-Combustion Chamber Figures 1RegenerativelyCooled TCAFrom SuttonAE6450 Rocket PropulsionInjector-Combustion Chamber Figures 2Hydrazine Thruster InjectionFrom Sutton2AE6450 Rocket PropulsionInjector-Combustion Chamber Figures 3Combustion Chamber: ZonesFrom SuttonAE6450 Rocket PropulsionInjector-Combustion Chamber Figures 4Combustion Chamber Cooling ApproachesFrom Humble3AE6450 Rocket PropulsionInjector-Combustion Chamber Figures 5Small Thruster: Radiation CooledFrom SuttonAE6450 Rocket PropulsionInjector-Combustion Chamber Figures 6Characteristic Combustion Chamber LengthsFrom HumbletccAVL =*comb. chamber vol.nozzle throat area4AE6450 Rocket PropulsionInjector-Combustion Chamber Figures 7Injector HeadFromSuttonAE6450 Rocket PropulsionInjector-Combustion Chamber Figures 8Injector TypesFrom SuttonInjector elements:holes in injector facefastened into injector face5AE6450 Rocket PropulsionInjector-Combustion Chamber Figures 9Bonded Plate AssemblyFrom SuttonAE6450 Rocket PropulsionInjector-Combustion Chamber Figures 10Injector ConfigurationsFrom Humble6AE6450 Rocket PropulsionInjector-Combustion Chamber Figures 11Injector ConfigurationsAE6450 Rocket PropulsionInjector-Combustion Chamber Figures 12Discharge CoefficientsFrom SuttonρρpACQmDΔ==2&7AE6450 Rocket PropulsionInjector-Combustion Chamber Figures 13From HumbleInjectorsAE6450 Rocket PropulsionInjector-Combustion Chamber Figures 14Impingement Injectors: AnglesFrom