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Publication numberUS3706278 A
Publication typeGrant
Publication dateDec 19, 1972
Filing dateFeb 25, 1971
Priority dateFeb 25, 1971
Publication numberUS 3706278 A, US 3706278A, US-A-3706278, US3706278 A, US3706278A
InventorsKowalick James F, Silverstein Martin S, Stiefel Ludwig
Original AssigneeUs Army
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Distributed propulsion for guns
US 3706278 A
Abstract
Propellant charges for weapons, especially for the small caliber type, made of grains consisting of two layers, an outer slow burning composition and an inner or core composition for the control of interior ballistics. The charges consist of a plurality of increments of such type grains which differ in the thickness and composition of the outer layer and the thickness and composition of the core resulting in better control of interior ballistics, such, for example, as the obtention of higher velocities at lower peak pressure.
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United States Patent 1151 3,706,278

Stiefel et al. 1451 Dec. 19, 1972 [54] DISTRIBUTED PROPULSION FOR [56] References Cited GUNS UNITED STATES PATENTS [72] Inventors: Ludwig Stieiel, Philadelphia, Pa.;

Martin S. silverstein, Mest Mount, 2,072,671 3/1937 Foulke ..102/4O NJ .JamesF Kowalick southam 3,092,525 6/1963 Cook ..102/104 p 3,421,931 1/1969 Reverandu... ..1(l2/l()4 2,289,318 7/1942 Pratt ..102/104 [73] Assigneez The United States of America as 2,575,871 11/1951 Gordon etal. ..l(l2/l()4 23: 3 by the Secretary of the Primary Examiner-Robert F. Stahl Att0rney-Harry M. Saragovitz et al.

[22] Filed:" Feb. 25, 1971 [21] Appl. No.: 118,739 [57] ABSTRACT Propellant charges for weapons, especially for the Related Appllcatlon Data small caliber type, made of grains consisting of two [63] Continuation-impart of Ser. No. 818,140, April 21, l an outer Pummg Composmon 1969 abandoned inner or core composition for the control of interior ballistics. The charges consist of a plurality of incre- [52] Us Cl 102/38 102/103 102/104 ments of such type grains which differ in the thickness 149/3 and composition of the outer layer and the thickness [51] Int Cl F42) 5/16 and composition of the core resulting in better control [58] i 49/3 of interior ballistics, such, for example, as the obten 0 149/ 1 tion of higher velocities at lower peak pressure.

5 Claims, 1 Drawing Figure P AfTEIN TEH m 19 I972 \NVENTOR5 LUDW\6 STiEF'EL. MART\N E5. $\L,\/ERSTE\N JAMES F. KOWALICK AT TURN EY5.

DlSTlRlBUTED PROPULSION FOR GUNS This application is a continuation-in-part of our application Ser. No. 818,140, filed 21 Apr. 1969, for Distributed Propulsion for Guns", now abandoned, and relates to incremental propellant charges in the control of interior ballistics for small arms weapons wherein the propellant grains in a given increment will consist of two layers, a slower burning outer layer and a faster burning inner layer.

The invention described herein may be manufactured, used, and licensed by or for the Government for governmental purposes without the payment to us of any royalty thereon.

At present, the gas generation rate of small arms propellants may be modified through propellant composition, grain geometry, or deterrent coatings, any of which are capable of changing the pressure-time curve produced by the ammunition.

These current small arms ammunition charges are generally comprised of one type and size of propellant grain. Our invention contemplates propellant charges which comprise a plurality of increments, wherein propellant grains of different sizes, shapes and com position may be used therein, i.e., the grains may be solid cylinders, perforated cylinders, spheres, platelets or discs. Because of the very small sizes of the grains used in small arms ammunition, only grains of limited geometries heretofore could be economically manufactured. Consequently, the number of variables that could be manipulated to achieve a given specified performance was severely limited. Our invention, however, will permit the manipulation of a large number of variables to obtain desired controls. Furthermore, the charges can now be loaded in conventional loading machinery, there being no barriers or separate packages or capsules involved.

As aforediscussed, prior art small arms propellants are treated with a deterrent composition which is not a film or layer on the external surface of the grains, but a material which is absorbed into the outer portions of the grain matrix and thus serving to reduce the burning rate of outer portions of the grains.

In contrast therewith, our invention allows the gas generation schedule to be controlled by permitting the programmed burning of the increments without the use of any separately assembled barriers, capsules and the like. With regard to these smaller caliber cartridges, such barriers or capsules cannot readily be loaded into the narrow case necks, and furthermore, the very short ballistic time results in incomplete combustion of the barriers or capsules, to thereby cause deposition of unburned debris in the weapon, or the ejection of partially burned material from the gun. Our invention therefore, involves polymeric films, or layers, or coatings applied to the outer surfaces of the individual grains in such a way that the entire charge, including the scheduling coating is totally consumed by the time the bullet exits from the gun or weapon.

Briefly then, our invention lends versatility to propellant charges, especially small arms propellant charges, such that their gas generation schedule may be regulated by manipulating the thickness and burning rate of the outer layer and inner core respectively, as well as the number and size of the increments.

It is therefore the principal object of this invention to provide improved means for controlling the interior ballistics of weapons.

Other and further objects of the invention will be apparent to those skilled in the art upon study of this disclosure and wherein the single FIGURE illustrates a sectional view of an embodiment of our small arms cartridge.

Referring now to the drawing, a standard small arms cartridge 10 includes a projectile l2, casing 14 and primer 16. While three increments only are shown, mixed uniformly, any reasonable number may be employed. One of the increments comprises a ball propellant or inner core composition 20, although single and double base extreded propellants may be used advantageously. The uncoated propellant is herein designated the inner core or faster burning composition. Another increment 22 is comprised of grains having an inner core composition with an outer layer of a suitable resin or polymeric coating, which may suitably comprise n-butyl methacrylate resin; methyl cellulose; or polyvinyl acetate; and others.

These scheduling coating materials should be soluble or dispersable in a solvent that does not react adversely with the inner core composition propellant. Upon evaporation of the solvent, a polymerization or crosslinking reaction should desirably occur to insolubilize the deposited film or coating with respect to the solvent to prevent softening of the previous layer when subsequent layers are applied. The coating solution will consist of about 5 to 15 percent solids by weight in the solvent, the exact concentration of coating solids in the solution being dependent only on the requirements of the specific coating process, for example, the types of spray devices being used. The actual proportions of solvent to solids is of little concern and within the skill of the art since the solvent will have evaporated leaving the deposited film, or layer, or coating on the desired surfaces.

Processes for coating our materials are many and varied. For example, the tablet coating process, fluidized bed process, airless spray process, microencapsulation techniques, vacuum deposition, phase separation from aqueous as well as organic-solvent solutions, interfacial polymerization and melt techniques, and the like, may be employed advantageously and successfully in carrying out our invention, while providing means for preventing the small grains from adhering to each other while the film is drying.

A third increment 24 which may comprise the same materials as 22 is also incorporated into the charge. Regardless of the composition of the outer material, it will be slower burning than the outer layer used for increment 22, by virtue of its composition or thickness. The propellant contained within the coating may be identical with inner core 20 or that used for increment 22, or may even be faster burning than either of these. Any air space remaining between projectile l2 and the propellant may be packed with cotton 26.

The abovedescribed concept of charges consisting of increments of different types of overall propellant grains, where each coated grain consists of an outer slower burning composition and a faster core composi tion to yield controlled interior ballistics by means of the burning rates and thicknesses of the outer composition and burning rate and thickness of the inner composition for each type used and by quantities of each type used in the complete charge is referred to as distributed propulsion.

The products and processes of our invention are illustrated by the non-limiting example hereinunder set forth, all percentages being by weight:

A 5.56mm cartridge, including a projectile weighing 56 grains, was loaded with 27.8 grains of a standard double base rolled ball propellant having a cut of 0.027 inch/.016 inch (grain passed through a screen having 0.027 inch openings but was retained on a screen having 0.016 inch openings) rolled to a uniform web of 0.015 inch, and a composition as follows:

Composition:

Nitrocellulose (13.15% N) 81.59% Nitroglycerine 10.52 Dibutylphthalate 5.68 Diphenylamine 0.98 Total Volatiles 1.23

The peak chamber pressure obtained was 49.0 kpsi (thousand pounds per square inch) and the projectile velocity, measured at 15 feet from the muzzle, was 3100 fps. Measurement of the velocity at a distance of 15 feet from the muzzle is accomplished by the standard 2-screen method whereby an average velocity at 15 feet from the muzzle is obtained using a 10 foot base line.

EXAMPLE I 75/25 polyvinylbutyral/melamine formaldehyde resin Solvent: 50/50 V/V l-leptaneethanol Coating Solution: 10% solids in the solution 3rd Increment:

Weight: 5.6 grains Propellant: Identical with second increment Coating:

(a) Level:5% by weight of propellant (b) Data:

Solids: 75/25 polyvinylbutyral/melamine formaldehyde resin Solvent: 50/50 V/V Heptaneethanol Coating Solution: solids in the solution These increments were mixed and loaded into the 5.56mm cartridge case. The 25 grains so mixed yielded a peak pressure of 48.9 kpsi and a velocity at feet of 3160 fps. Although the peak pressures and velocities are substantially the same for our inventive distributed propulsion cartridge and the standard, our cartridge required only 25.0 grains to equal the performance of 27.8 rains f standar doubl b se ball ellant. Furthgr, the Tower loadi ng density 3f our ch ig of extruded propellant makes it even more difficult to achieve the values of the standard.

We wish it to be understood that we do not desire to be limited to the exact details of construction shown and described, for obvious modifications will occur to a person skilled in the art.

We claim: 1. In combination with a cartridge having a primer, projectile and case, the improvement therewith for providing good control of interior ballistics in a weapon system using said cartridge, said improvement comprismg a propellant charge disposed within said case and comprising 7 4 a substantially uniform mixture of the propellant grains of a plurality of increments of propellant grains, each grain of at least one of said increments comprising two layers, said layers comprising an outer slower burning composition and an inner faster burning core composition, and each grain of at least one of said increments comprising at least one layer, said one layer being a core composition whose composition may be the same as or different from said first mentioned core composition and which is faster burning than any of said outer slower burning compositions, whereby upon ignition of said propellant charge, better control of interior ballistics is provided.

2. The cartridge of claim 1 wherein said cartridge is of 5.56mm size.

3. The cartridge of Claim 1 wherein said charge comprises a first increment of double base extruded propellant devoid of perforations therethrough, a second increment of single base extruded propellant grain, and a third increment of single base extruded propellant grain having a single perforation therethrough, said double base, extruded propellant comprising, by weight, 87.9 percent nitrocellulose having 13.15 percent nitrogen, 9.8 percent nitroglycerine, 1.0 percent diphenylamine, and 1.3 percent volatiles, and said single base extruded propellant grain comprising, by weight, 97.7 percent nitrocellulose having 13.15 percent nitrogen, 1.0 percent diphenylamine, and 1.3 percent volatiles.

The cartridge of claim 3 wherein said first increment comprises 6.3 grains, each of said grains having a 0.025 inch outside diameter and a 0.025 inch length, said second increment has a single perforation therethrough and comprises 13.1 grains, each of said second increment grains having an outer diameter of 0.030 inch, a length of 0.42 inch, and a perforation diameter of 0.007 inch with a 4 percent coating, by weight, therearound of /25 polyvinylbutyral/melamine formaldehyde, and said third increment comprises 5.6 grains, each of said third increment grains having dimensions equal to said second increment grains and having a 5 percent coating, by weight, therearound of 75/25 polyvinylbutyral/melamine formaldehyde.

5. The cartridge of claim 4 wherein said cartridge yields a peak pressure of 48.9 kpsi and a projectile velocity at 15 feet of 3160 fps.

Patent Citations
Cited PatentFiling datePublication dateApplicantTitle
US2072671 *Oct 30, 1934Mar 2, 1937Hercules Powder Co LtdAmmunition and propellant charge therefor
US2289318 *Dec 14, 1932Jul 7, 1942Atlas Powder CoPropellent fuel cartridge
US2575871 *Sep 24, 1947Nov 20, 1951Ici LtdGranular smokeless propellant powders
US3092525 *Sep 30, 1960Jun 4, 1963Olin MathiesonMethod of producing unitary nitrocellulose grains capable of fragmentation under primer blast to original granules
US3421931 *Aug 2, 1965Jan 14, 1969RhodiacetaCoating of pulverulent materials
Referenced by
Citing PatentFiling datePublication dateApplicantTitle
US3897733 *Mar 19, 1973Aug 5, 1975Us ArmyHigh bulk density extruded propellant for small arms cartridges
US3938440 *Mar 14, 1974Feb 17, 1976Olin CorporationMixed propellant charge
US4455942 *Jul 16, 1981Jun 26, 1984The Secretary Of State For Defence In Her Britannic Majesty's Government Of The United Kingdom Of Great Britain And Northern IrelandTraining ammunition
US4590860 *Jan 11, 1984May 27, 1986United Technologies CorporationConstant pressure end burning gas generator
US5712445 *Apr 10, 1996Jan 27, 1998Alliant Techsystems Inc.Propellant system
US5892172 *Apr 22, 1997Apr 6, 1999Alliant Techsystems Inc.Propellant system
US6508177 *Sep 11, 2000Jan 21, 2003The Ensign-Bickford CompanyMatrices comprising pentaerythritol tetranitrate, pentolite or trinitrotoluene having geometric shaped pellets and high sensitivity contactor surfaces for detonation
US8276519 *Sep 17, 2010Oct 2, 2012Polywad, Inc.Wad-less cartridges and method of manufacturing the same
US20110017090 *Sep 17, 2010Jan 27, 2011Menefee Iii James YWad-less cartridges and method of manufacturing the same
USRE30002 *Jul 28, 1977May 22, 1979Olin CorporationCompacts of nitrocellulose dispersed in granular nitrocellulose
EP0005112A1 *Apr 12, 1979Oct 31, 1979ETAT-FRANCAIS représenté par le DELEGUE GENERAL POUR L'ARMEMENTPropulsive charge for ammunition and process for charging cartridges
EP0499244A2 *Feb 13, 1992Aug 19, 1992Dynamit Nobel AktiengesellschaftModular propellant charge
EP0580017A1 *Jul 7, 1993Jan 26, 1994DIEHL GMBH & CO.Igniter for propulsive charges
WO2001053771A2 *Jan 5, 2001Jul 26, 2001Beal Harold FRound of rifle ammunition and method for making same
Classifications
U.S. Classification102/430, 149/3, 102/288
International ClassificationF42B5/16, F42B5/00
Cooperative ClassificationF42B5/16
European ClassificationF42B5/16