Olin Corporation

Primex Technologies, Inc.

General Dynamics Ordnance and Tactical Systems, Inc.

William L O'Meara

Terry A Murray

Antonio F Gonzalez

Jonathon M Howard

John J Williamson

The present invention is directed to a propellant composition made from a lacquer, the lacquer comprising: (a) from about 15 to about 70 wt % of an organic solvent; (b) from about 0.1 to about 2.5 wt % of a stabilizer; (c) optionally, from about 0% to about 40 wt % of an energetic plasticizer; (d) optionally, from about 0 to about 10 wt % of a nonenergetic plasticizer; (e) optionally, from about 0 to about 10 wt % water; (f) optionally, from about 0 to about 15 wt % of additional additives; and balance being nitrocellulose; all weight percents based on the total weight of the composition, and wherein the lacquer has a viscosity of less than 10 million centipoise when processed. The present invention is also directed to an efficient and safe method of making perforated propellant grains using the above lacquer composition, as well as propellant grains having ellipsoidal cross sections or outwardly extending ridges.

Perforated propellant and method of manufacturing same

There is disclosed a propellent having a deterred burn rate. The propellent is a particulate containing an energetic binder base and a thermoplastic burn deterrent. The energetic binder has in impetus (energy) in excess of 200,000 foot pounds per pound (mass) and the thermoplastic burn deterrent is both a solid at room temperature and soluble in an organic solvent. The burn deterrent is gradationally dispersed within the particulate with the greatest concentration of burn deterrent at the particulate periphery.

Propellant containing a thermoplatic burn rate modifer

There is disclosed a propellent having a deterred burn rate. The propellent is a particulate containing a nitrocellulose base and a cellulosic thermoplastic deterrent, preferably cellulose acetate butyrate or cellulose acetate propionate. The deterrent is gradationally dispersed within the particulate with the greatest concentration of deterrent at the particulate periphery.

Nitrocellulose propellant containing a cellulosic burn rate modifier

Method of producing a nitrocellulose propellant containing a cellulosic

An energetic combustible cartridge case comprises a tubular body of a plastic nonfelted sheet propellant and an outer coating portion of a thermoset polymeric resin such as a polyurethane. The sheet propellant is a colloidal nitrocellulose composition which preferably contains a large portion of nitroglycerine and diethylene glycol dinitrate.

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Tallahassee, FL, United States of America

William L O'Meara