Abstract:A resonance ignition system is attractive for rocket engines because of the igniter's simplicity and the possibility of multiple ignitions without additional mechanical complexities. In this work a resonance igniter to produce a torch from burning of gaseous oxygen and liquid kerosene was designed and tested. The oxygen is heated for 0, 1 s in the acoustic resonator cavity, and the ignition occurs instantaneously on kerosene injection. The preliminary tests under ambient conditions demonstrated the igniter's a… Show more
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