Abstract
Conclusions An ignition system based on resonance igniter was designed and tested, which 1) can operate independently of engine propellant lines only at the cost of the energyof stored compressedoxygen;2) contains reduced number of components and can be designed as a modular unit, for a wide range of mass ow rate and mixture ratio; and 3) allows up to eight ignitions with an oxygen tank of 2.4 L under 170 bar, for 2 s of torch duration and 33 ¢ 10 3 kg/s of torch ow rate.
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