Dynamic characteristics of a resonant gas-dynamic system for ignition of a fuel mixture

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 pressu...

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Veröffentlicht in:Combustion, explosion, and shock waves explosion, and shock waves, 2013-11, Vol.49 (6), p.657-661
Hauptverfasser: Aref’ev, K. Yu, Voronetskii, A. V., Il’chenko, M. A.
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Sprache:eng
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Zusammenfassung: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.
ISSN:0010-5082
1573-8345
DOI:10.1134/S0010508213060038