Composite Solid Propellant Ignition Mechanisms

This report describes the results of an experimental study of the thermal decomposition characteristics of composite solid propellant fuel components. Variations in heating rate, pressure, environmental gas, and polymer type were studied. Supplementary propellant ignition tests utilizing an arc- ima...

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Bibliographische Detailangaben
1. Verfasser:	Shannon, Larry J
Format:	Report
Sprache:	eng
Schlagworte:	Combustion and Ignition COMPOSITE PROPELLANTS DECOMPOSITION FLAMMABILITY IGNITION POLYMERS PYROLYSIS REACTION KINETICS SOLID ROCKET PROPELLANT BINDERS Solid Rocket Propellants THERMAL PROPERTIES THERMAL RADIATION
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Beschreibung
Zusammenfassung:	This report describes the results of an experimental study of the thermal decomposition characteristics of composite solid propellant fuel components. Variations in heating rate, pressure, environmental gas, and polymer type were studied. Supplementary propellant ignition tests utilizing an arc- imaging furnance and ionization gap techniques were conducted to obtain information relating time for onset of a gas-phase reaction to propellant ignition times via radiant heating.