NON-ASBESTOS INSULATION FOR ROCKET MOTOR CASING

An insulation material for a rocket motor is described, which is composed of a glass fabric, a resin binder, and a fire retardant. The resin binder preferably is composed of a phenolic resin and a Buna-N rubber, and the fire retardant is preferably alumina trihydrate. A method of manufacturing the i...

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Bibliographic Details
Main Authors DAVIDSON, THOMAS F, PENNINGTON, WILLIAM L, SKOLNIK, EDWARD G
Format Patent
LanguageEnglish
French
Published 02.12.1999
Edition7
Subjects
AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F,C08G
BLASTING
CHEMISTRY
COMBUSTION ENGINES
COMPOSITIONS BASED THEREON
COMPOSITIONS OF MACROMOLECULAR COMPOUNDS
GENERAL PROCESSES OF COMPOUNDING
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
JET-PROPULSION PLANTS
LIGHTING
MECHANICAL ENGINEERING
METALLURGY
ORGANIC MACROMOLECULAR COMPOUNDS
THEIR PREPARATION OR CHEMICAL WORKING-UP
WEAPONS
WORKING-UP
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Summary:An insulation material for a rocket motor is described, which is composed of a glass fabric, a resin binder, and a fire retardant. The resin binder preferably is composed of a phenolic resin and a Buna-N rubber, and the fire retardant is preferably alumina trihydrate. A method of manufacturing the insulation material is also described. An insulation material for a rocket motor is described, which is composed of a glass fabric, a resin binder, and a fire retardant. The resin binder preferably is composed of a phenolic resin and a Buna-N rubber, and the fire retardant is preferably alumina trihydrate. A method of manufacturing the insulation material is also described.
Bibliography:Application Number: CA19992328083