HYPERGOLIC IGNITION AT REDUCED PRESSURES. PART 2

A mathematical model of hypergolic ignition in reaction control systems was developed based on physical kinetics of droplet evaporation and chemical kinetics of ignition reactions. Reasonable agreement between theoretical and experimental ignition delays were obtained. The dominant ignition reaction...

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Bibliographische Detailangaben
Hauptverfasser:	Corbett, Albert D, Dawson, Bruce E, Seamans, Thomas F, Vanpee, Marcel M
Format:	Report
Sprache:	eng
Schlagworte:	ALCOHOLS CHLORINE COMPOUNDS CHLORINE PENTAFLUORIDE CHLORINE TRIFLUORIDE COMBUSTION CHAMBERS CONDENSATION FLUID FLOW FLUORIDES FUEL ADDITIVES FUEL INJECTION FUEL INJECTORS FURANS HYDRAZINE DERIVATIVES HYDRAZINES HYPERGOLIC IGNITION HYPERGOLIC ROCKET PROPELLANTS IGNITION LAG Liquid Propellant Rocket Engines LIQUID ROCKET FUELS LIQUID ROCKET OXIDIZERS Liquid Rocket Propellants MATHEMATICAL MODELS METHYL HYDRAZINES MHF-5 MMH NITROGEN COMPOUNDS NITROGEN OXIDE(N2O4) NITROGEN OXIDE(NO2) REACTION KINETICS ROCKET NOZZLES SPACE PROPULSION TETROXIDES VAPORS
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