Electrolytic igniter for rocket engines using liquid propellants

摘要: The electrolytic ignitor comprises an injector ( 2 ) constituting a first electrode and including fuel device 26 ), oxidizer 27 electrolyte 1 second 5 electrically insulated from the by insulator 4 extending downstream beyond tank 12 solenoid valve 11 interposed between distribution channel 3 suitable for delivering in form of free jets through constituted at least one injection hole situated vicinity electrical power supply circuit adapted to raise potential lying range 50 V 1000 relative electrode. injected is capable causing ignition gaseous mixture formed outlet combustion chamber torch incorporating main rocket engine.