Method of preparing a non-feathering nitramine propellant
AssigneeMorton Thiokol, Inc.
InventorsClifford E. Kristofferson, Donald G. Fisher, Frank H. Bell
Life of this patent
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Abstract
A low vulnerability ammunition (LOVA) propellant is prepared with a polyurethane binder and a mixture of nitramines consisting essentially of RDX and at least 7.5 wt. % HMX (based on combined oxidizer binder matrix weight). Dilution of RDX with HMX enhances precure extrudability of the propellant grain. Polymerization and extrudability is provided without slumping prior to total cure given a NCO:DIOL:TRIOL equivalent ratio of from about 110:15:85.
Claims6
A method of producing a solid extruded propellant grain characterized by a smooth surface and predictable burn characteristics, the method comprising:
- a. solventlessly formulating an uncured propellant composition consisting essentially of from 20% to 60% based upon total oxidizer-binder weight of a plasticized or non-plasticized polyurethane binder matrix formed from (A) an isocyanante of functionality of at least 2, (B) a diol prepolymer which is a hydroxyl-terminated block copolymer of ethylene and propylene oxides and (C) a crosslinker, the matrix having an NCO:DIOL:crosslinker equivalent ratio of about 110:15:85, with about an 8% permissible variation in this ratio, and from 40% to 80% based upon total oxidizer-binder weight of a mixture of nitramine oxidizers consisting essentially of from 7.5 wt. % to 50 wt. % HMX based upon total oxidizer weight, balance essentially RDX, the amount of HMX being sufficient whereby feathering is avoided;
- and
- b. at a temperature whereat said prepolymer, said isocyanate and said crosslinker are in a liquid phase, extruding said uncured propellant composition to form a propellant grain.
Dependencies are inferred from the claim text.