SOLID COMBUSTIBLE PROPELLANT COMPOSITION

A solid combustible propellant composition is disclosed comprising a solid oxidizer composition comprising ammonium nitrate and at least one other solid oxidizer having a decomposition or melting temperature of at least 500° C., a fuel, and a polymer binder that decomposes by chain scission to under...

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Bibliographische Detailangaben
1. Verfasser:	MANGUM MICHAEL GEORGE
Format:	Patent
Sprache:	eng
Schlagworte:	BLASTING CHEMISTRY COMBUSTION ENGINES EXPLOSIVES EXPLOSIVES OR THERMIC COMPOSITIONS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MANUFACTURE THEREOF MATCHES MECHANICAL ENGINEERING METALLURGY USE OF SINGLE SUBSTANCES AS EXPLOSIVES WEAPONS
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Beschreibung
Zusammenfassung:	A solid combustible propellant composition is disclosed comprising a solid oxidizer composition comprising ammonium nitrate and at least one other solid oxidizer having a decomposition or melting temperature of at least 500° C., a fuel, and a polymer binder that decomposes by chain scission to undergo liquefaction during combustion of the propellant composition.