Abstract
Results of an experimental study of specific features of operation of a resonant gasdynamic ignition system, as applied to initiation of liquid-propellant thrusters, are reported. Dynamic characteristics of the initiation process are determined. The behavior of the spectral characteristics of pressure oscillations in the combustor of a testbench model of a liquid-propellant thruster with ignition of the fuel mixture by the gas-dynamic system is considered.
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Original Russian Text © K.Yu. Aref’ev, A.V. Voronetskii, M.A. Il’chenko.
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Translated from Fizika Goreniya i Vzryva, Vol. 49, No. 6, pp. 41–46, November–December, 2013.
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Aref’ev, K.Y., Voronetskii, A.V. & Il’chenko, M.A. Dynamic characteristics of a resonant gas-dynamic system for ignition of a fuel mixture. Combust Explos Shock Waves 49, 657–661 (2013). https://doi.org/10.1134/S0010508213060038
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DOI: https://doi.org/10.1134/S0010508213060038