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 |
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Hauptverfasser: | , , |
Format: | Artikel |
Sprache: | eng |
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Online-Zugang: | Volltext |
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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. |
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ISSN: | 0010-5082 1573-8345 |
DOI: | 10.1134/S0010508213060038 |