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US 4,102,953 AGranted
Method for making extruded, solventless, composite-modified double base propellant
AssigneeThe United States of America as represented by the Secretary of the Navy
InventorsCraig E. Johnson, Paul F. Dendor, Elmer R. Csanady
Life of this patent
Estimating the term…
Abstract
Solids loaded, extrudable, solventless, double-base propellants are formued by combining liquid plasticizers, solid binders, a high percentage of solid oxidizers, and fillers to yield propellants having high densities and capable of delivering high specific impulse.
Claims19
A method for formulating an extrudable composite-modified double-base propellant having an appreciable quantity of ballistic solids, which comprise the steps of:
- preparing a first solution comprising a liquid aliphatic hydrocarbon solvent selected from the group consisting of heptane, hexane, and octane, a first portion of active plasticizers selected from the group consisting of nitroglycerin, metroil trinitrate, triethylene glycol dinitrate, pentaerythritol trinitrate and mixtures thereof, a first portion of relatively non-active plasticizers selected from the group consisting of dinormal propyl adipate, dibutyl phthalate, dimethyl phthalate, diethyl phthalate, dioctyl phthalate, diisobutyl azelate, dimethyl sebacate, dibutyl sebacate, and mixtures thereof, and a first portion of filler ingredients selected from the group consisting of ethyl centralite, resorcinol, candelilla wax, 2-nitro diphenyl amine, aluminum lead oxide, lead stamate, lead salicylate, copper salicylate, lead .beta. resorcylate, copper .beta. resorcylate, and mixtures thereof;
- mixing a solid binder ingredient selected from the group consisting of from 12 to 14.14% nitrogen nitrocellulose, into said first solution so as to form a first slurry;
- agitating said first slurry for from about 30 to about 60 minutes at a rate from about 3500 to about 5000 revolutions per minute, so as to deagglomerate and bruise the surface of the selected solid binder ingredient;
- mixing into said first slurry a second portion of the selected relatively non-active plasticizers so as to coat said deagglomerated solid binder ingredient;
- separating and saving said first liquid aliphatic hydrocarbon solution from said coated solid binder;
- drying said coated solid binder to remove any remaining liquid aliphatic hydrocarbon and any traces of water;
- determining the amount of the selected liquid aliphatic hydrocarbon lost in separating and drying;
- forming a second slurry by re-slurrying said dry coated solid binder in a second solution comprising a mixture of said saved solution and enough of the selected liquid aliphatic hydrocarbon to replace that lost in separating and drying;
- mixing a solid oxidizer selected from group consisting of nitroquanidine, ammonium perchlorate, ammonium nitrate, cyclotetramethylenetetranitramine, and cyclotrimethylenetrinitramine into said second slurry to obtain a uniform dispersion of said solid oxidizer and said coated solid binder;
- forming a solid composition by mixing into said dispersion a second portion of the selected active plasticizer ingredients and the selected fillers, and a third portion of the selected relatively non-active plastizers, so as to evenly coat said solid oxidizer and begin to penetrate said coated solid binder;
- separating and saving the resulting liquid aliphatic hydrocarbon solution from said solid composition;
- drying and curing said solid composition until it is fully plasticized;
- and
- extruding the dried cured composite-modified double-base propellant composition.
11 more elements
Dependencies are inferred from the claim text.