US2072671A - Ammunition and propellant charge therefor - Google Patents
Ammunition and propellant charge therefor Download PDFInfo
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- US2072671A US2072671A US750623A US75062334A US2072671A US 2072671 A US2072671 A US 2072671A US 750623 A US750623 A US 750623A US 75062334 A US75062334 A US 75062334A US 2072671 A US2072671 A US 2072671A
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- powder
- charge
- mass
- explosive
- propellant
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B5/00—Cartridge ammunition, e.g. separately-loaded propellant charges
- F42B5/02—Cartridges, i.e. cases with charge and missile
- F42B5/16—Cartridges, i.e. cases with charge and missile characterised by composition or physical dimensions or form of propellant charge, with or without projectile, or powder
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S206/00—Special receptacle or package
- Y10S206/819—Material
Definitions
- This invention relates to an improvement in ammunition and propellant charge therefor. More particularly, this invention relates to fixed ammunition and propellant charge therefor, but will be found to be applicable to non-xed propellant charges for large calibre guns.
- propellant charges usually composed Iof black or smokeless powder; is that they burn progressively so that pressure will be developed gradually and maintained or increased behind the shot or projectile after it starts its travel through a gun barrel in order that maximum velocity may be imparted to the shot or projectile with the l5 maximum pressure developed after the shot or projectile lias progressed appreciably through the gun barrel, rather than having the maximum pressure attained when the slot cr projectile is at, or near., the breech of the gun.
- Various expedients have heretofore been used to such end.
- the powder grains comprising a propellant charge have been coated with a deterrent material which slows the initial burning rate of powder.
- charges have comprised a mixture of powder grains having a fast burning rate and grains having a slow burning rate, or composite powder grains having a core of fast burning nitrocellulose colloid surrounded by an outer skin of slow burning nitrocellulose colloid.
- a propellant charge which has the characteristic of maintaining or building up the diminishing pressure behindthe shot or a projectile, after it has progressed on its passage through a gun 40 barrel, with the result that heavier charges may be used when desired Without'development of excessive maximum pressures and greatly increased projectile velocities are obtained over those obtained heretofore with similar maximum pressures.
- propellant charges in accordance with this invention may 'comprise any desired or suitable propellant powder in any desired or suitable grain formlfor the type and size of gun in which they are to be used.
- the charges may be composed of but one type of powder or of different types and all or a portion of the total charge may be treated or coated with a deterrent.
- propellant chargesin ac- 55 cordance with this invention may be contained in a cartridge case or shot shell such as are usual in the case of so-called xed ammunition, or they may be contained in powder bags such as are used in making up charges for guns of large calibre.
- propellant charges in accordance with this invention will comprise a mass of propellant powder less than the amount of the ⁇ total charge and a container or capsule or a plurality of containers or capsules carrying pro-- pellant powder in amount to make up the total charge.
- the container or containers Will be associated with the mass of powder, preferably embedded within the mass, and will be independent of the' cartridge case, shot shell or powder bag in which the charge as a whole is contained.
- the mass of propellant powder will desirably be in the form of grains and the container or containers will ydesirably be, as it were, mixed with the grains forming the mass.
- the containers may variously be formed of any desired material and may have any desired shape and structure.
- the containers may be formed from celluloid, gelatin, tin, lead, magnesium, steel, alloy steel, etc.;and may be generally cylindrical, or of globular or ovoid or other shape.
- Diierent containers in a charge may be composed of the ⁇ same or different materials and may be of the same or different shape or structure.
- the walls of the containers may be of varying thickness depending upon the material of which they are composed and the time for which they are desired to hold or resist burning of the powder contained therein. Different containers in a charge may have the same or different wall thickness.
- the particular material or materials, shape, structure and wall thickness of the containers will depend upon conditions such as type and calibre of gun, nature of the propellant powder or powders used, number of containers in a charge, results to be attained, etc. and may be widely varied.
- Figure 1 is a view in elevation, partly in section and partly broken away, of a shot gun shell embodying this invention.
- Figure 2 is a sectional view of a rloppy cartridge embodying this invention.
- Figures 3, 4 and 5 are views, in elevation. of different forms of containers illustrating modications from the form of the containers shown in Figures 1 and 2.
- Figure 6 is a view partly in section of a detail of a modication of this invention.
- Figures 1 and 2 A and B indii Vcate respectively a shot gun shell and a rifle car- 5 tridge, each 'provided in its base with a percussion indicated materials and desirably are made in 5 two parts adapted to telescope together, as shown.
- the containers may have the generally cylindrical torni of the capsules shown in Figures 1 and 2, or they may be of the globular form of the capsule E', Figure 3, the ovoid form of the capsule Figure 4, Dromer, desired form.
- the containers may be of'th'e structure of the containerE shown in- Figure 5; or may comprise a capsule or container E within a capsule or container E as shown in Figure 6; Iii a structure shown in Figure 6 the capsules may be loaded with the same or different powder or explosive as rindicated by D and D. The capsulesare so constructed as to close tightly.
- the mass of powder D is in amount less than the desired total charge of powder for the shell A'and the cartridge B respectively.
- the powder necessary to supplement the mass D to make up the total desired charge is carried, as 'shown at D', in the tightly closed capsules E, which, depending upon conditions, type or types of powder, results desired, etc., may be greater or less in number ythan shown.
- the cartridge B is fitted with a bullet f, while the shell A is provided with wads g over the pow- 40, der, a charge of shot h and a shot wad z' on which the edge of the shell is crimped to retain it.
- powder D may be of any type, as black powder or smokeless powder, and may be of any form or grain size, untreated or treated with a deterrent.
- the powder D and the powder D in the capsules may be ofthe same type and form or the two may be diierent in type or form, either or both.
- the powderD may be, for example, a. smokeless powder treated with a deterrent tov slow the burning rate and the powder Dmay be the same, orit may be, for example, an untreated faster burning powder.
- a fast burning powder may comprise the loose charge D, and one or more capsules E may contain a slower burning powder. In certain types of arms, such loading I have found very advantageous.
- diierent types or grades of powder may be used in the capsules respectively.
- the capsules or some of them may contain a very rapid burning explosive as nitrolactose, tetranitropentaerythrite,v etc., which I contemplate as within the term powder as used herein.
- the mass of powder D will be ignited and will burn,l creating a moderate pressure and temperature in the breech of the gun which will act ,to start the shot h or the bullet f through the gun barrel at a moderate but increasing velocity.
- the capsules E or some of them may be made to break down respectively I at intervals, if desired, by constructing them or some of them, respectively, of different materials relatively differently resistant to heat or pressure.
- a propellant charge for guns comprising a mass of explosive comprising a portion of the total charge and a container formed from an incombustible material embedded in said mass and containing an explosive comprising another portion of the total charge.
- a propellant charge for guns comprising a mass of relatively slow burning smokeless powder comprising a portion of the total charge and a container loosely .embedded in said mass of explosive and containing a relatively fast burning smokeless powder comprising another portion of the total charge.
- a propellant charge for guns comprising .a mass of explosive comprising a portion of the total charge and a container loosely embedded in said mass of explosive and containing a smokeless powder comprising another portion of the total charge, the smokeless powder comprised in said mass and contained in said capsule having, re-
- a propellant charge for guns comprising a mass of explosive comprising a portion of the total charge, a container within said massof .explosive containing an explosive comprising another portion of the charge and a container within said rst mentioned container and containing n still another portion of said charge.
- a propellant charge for guns comprising a
- mass of explosive comprising 'a portion of the total charge and a metallic container loosely embedded in said mass of explosive and containing an explosive comprising another portion of the charge.
- a propellant charge for guns comprising a mass of explosive comprising a portion of the total charge and a container loosely vembedded in said mass of explosive and containing an explosive comprising another portion of the total charge and means for firing the said mass vof explosive, the said container being of a character such as to protect its contained charge from flame resultant from ignition of the said mass of explosive for a period after the ignition thereof by the igniting means therefor.
- a propellant charge for guns comprising a mass of explosive comprising a portion of the total charge and a container containing an explosive comprising another portion of the total charge and means for firing the said mass of explosive, the said container being of a character such as to protect its contained charge from flame resultant from ignition of the said mass of explosive for aperiod after the ignition thereof by the igniting means therefor and of such a character as to conduct heat developed on burning of the said mass of explosive to its -contained charge for the ignition thereof at a time subsequent to the ignition of the said mass of explosive.
- a propellant charge for guns comprising a mass of explosive comprising a portion of the total charge and a container formed from a combustible material embedded wholly in said mass of explosive and containing an explosive comprising another portion of the total charge.
- a propellant charge for guns comprising a mass of explosive comprising a portion of the total charge and a. container formed from a combustible material embedded and freely movable within said mass of explosive and containing an explosive compris/ing another portion of the total
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- General Engineering & Computer Science (AREA)
- Portable Nailing Machines And Staplers (AREA)
Description
March 2, 1937. w, B. FOULKE AMMUNITION AND PROPELLANT CHARGE THEREFOR Filed Oct. 30, 1934 Patented Mar. 2, 1937 UNITED STATES PATENT OFFICE AMMUNITION AND PROPELLANT CHARGE THEREFOR Application October 30, 1934, Serial No.- 750,623
11 Claims. (Cl. 102-13) This invention relates to an improvement in ammunition and propellant charge therefor. More particularly, this invention relates to fixed ammunition and propellant charge therefor, but will be found to be applicable to non-xed propellant charges for large calibre guns.
As is well known, a characteristic desired for propellant charges. usually composed Iof black or smokeless powder; is that they burn progressively so that pressure will be developed gradually and maintained or increased behind the shot or projectile after it starts its travel through a gun barrel in order that maximum velocity may be imparted to the shot or projectile with the l5 maximum pressure developed after the shot or projectile lias progressed appreciably through the gun barrel, rather than having the maximum pressure attained when the slot cr projectile is at, or near., the breech of the gun. Various expedients have heretofore been used to such end. Thus, for example, the powder grains comprising a propellant charge have been coated with a deterrent material which slows the initial burning rate of powder. Again, charges have comprised a mixture of powder grains having a fast burning rate and grains having a slow burning rate, or composite powder grains having a core of fast burning nitrocellulose colloid surrounded by an outer skin of slow burning nitrocellulose colloid.
Another means to the end desired has been to break up a given charge into a plurality of separate' charges by division of a cartridge case into separate compartments. None of such expedients have. however, given entire satisfaction.`
Now in accordance withthis invention, a propellant charge is provided which has the characteristic of maintaining or building up the diminishing pressure behindthe shot or a projectile, after it has progressed on its passage through a gun 40 barrel, with the result that heavier charges may be used when desired Without'development of excessive maximum pressures and greatly increased projectile velocities are obtained over those obtained heretofore with similar maximum pressures. v
In general, propellant charges in accordance with this invention may 'comprise any desired or suitable propellant powder in any desired or suitable grain formlfor the type and size of gun in which they are to be used. The charges may be composed of but one type of powder or of different types and all or a portion of the total charge may be treated or coated with a deterrent.
Generally speaking, propellant chargesin ac- 55 cordance with this invention may be contained in a cartridge case or shot shell such as are usual in the case of so-called xed ammunition, or they may be contained in powder bags such as are used in making up charges for guns of large calibre.
From the broad standpoint, propellant charges in accordance with this invention will comprise a mass of propellant powder less than the amount of the` total charge and a container or capsule or a plurality of containers or capsules carrying pro-- pellant powder in amount to make up the total charge. The container or containers Will be associated with the mass of powder, preferably embedded within the mass, and will be independent of the' cartridge case, shot shell or powder bag in which the charge as a whole is contained. The mass of propellant powder will desirably be in the form of grains and the container or containers will ydesirably be, as it were, mixed with the grains forming the mass.
'I'he container or containers may variously be formed of any desired material and may have any desired shape and structure. Thus, for example, the containers may be formed from celluloid, gelatin, tin, lead, magnesium, steel, alloy steel, etc.;and may be generally cylindrical, or of globular or ovoid or other shape. l, Diierent containers in a charge may be composed of the `same or different materials and may be of the same or different shape or structure. The walls of the containers may be of varying thickness depending upon the material of which they are composed and the time for which they are desired to hold or resist burning of the powder contained therein. Different containers in a charge may have the same or different wall thickness.
The particular material or materials, shape, structure and wall thickness of the containers will depend upon conditions such as type and calibre of gun, nature of the propellant powder or powders used, number of containers in a charge, results to be attained, etc. and may be widely varied.
Having now indicated in a general'way the nature and purpose of this invention I will proceed to a detailed description of a preierred embodiment thereof with reference to the accompanying drawing, in which:
Figure 1 is a view in elevation, partly in section and partly broken away, of a shot gun shell embodying this invention. v
Figure 2 is a sectional view of a riile cartridge embodying this invention.
Figures 3, 4 and 5 are views, in elevation. of different forms of containers illustrating modications from the form of the containers shown in Figures 1 and 2.
Figure 6 is a view partly in section of a detail of a modication of this invention.
In the drawing, Figures 1 and 2, A and B indii Vcate respectively a shot gun shell and a rifle car- 5 tridge, each 'provided in its base with a percussion indicated materials and desirably are made in 5 two parts adapted to telescope together, as shown. The containers may have the generally cylindrical torni of the capsules shown in Figures 1 and 2, or they may be of the globular form of the capsule E', Figure 3, the ovoid form of the capsule Figure 4, Dromer, desired form. Likewise the containers may be of'th'e structure of the containerE shown in-Figure 5; or may comprise a capsule or container E within a capsule or container E as shown in Figure 6; Iii a structure shown in Figure 6 the capsules may be loaded with the same or different powder or explosive as rindicated by D and D. The capsulesare so constructed as to close tightly.
The mass of powder D is in amount less than the desired total charge of powder for the shell A'and the cartridge B respectively. The powder necessary to supplement the mass D to make up the total desired charge is carried, as 'shown at D', in the tightly closed capsules E, which, depending upon conditions, type or types of powder, results desired, etc., may be greater or less in number ythan shown.
The cartridge B is fitted with a bullet f, while the shell A is provided with wads g over the pow- 40, der, a charge of shot h and a shot wad z' on which the edge of the shell is crimped to retain it.
'Ihe mass of powder D may be of any type, as black powder or smokeless powder, and may be of any form or grain size, untreated or treated with a deterrent. The powder D and the powder D in the capsules may be ofthe same type and form or the two may be diierent in type or form, either or both. Thus the powderD may be, for example, a. smokeless powder treated with a deterrent tov slow the burning rate and the powder Dmay be the same, orit may be, for example, an untreated faster burning powder. Again, a fast burning powder may comprise the loose charge D, and one or more capsules E may contain a slower burning powder. In certain types of arms, such loading I have found very advantageous. Obviously diierent types or grades of powder may be used in the capsules respectively. Again, if desired, the capsules or some of them may contain a very rapid burning explosive as nitrolactose, tetranitropentaerythrite,v etc., which I contemplate as within the term powder as used herein.
In practice when, for example, the shell A or the cartridge B is fired in a gun, the mass of powder D will be ignited and will burn,l creating a moderate pressure and temperature in the breech of the gun which will act ,to start the shot h or the bullet f through the gun barrel at a moderate but increasing velocity.
Some time after ignition of the powder D, depending upon pressure/temperature conditions, material and wall thickness of thel capsules, the walls of the capsules will be burned through,
vbroken Orbtherwise destroyed or heated to a sucient temperature and the powder D' therein will burn. 'I'he powder D' will burn after the shot or bullet has progressed a substantial distance through the gun b'arrel and Vwill boost or maintain the pressure created on burning of the powder D, with the result that the velocity of the shot or bullet will be greatly accelerated.
As will be obvious, the capsules E or some of them may be made to break down respectively I at intervals, if desired, by constructing them or some of them, respectively, of different materials relatively differently resistant to heat or pressure.
The use of various particular materials for forming the capsules Ewill be productive variously of particular advantage. Thus, where celluloid is used it will, on burning, supplement the charge, gelatin will act as a deterrent to slow up the speed of burningof the charge as a whole, while tin or tin alloys will act to prevent fouling of the gun barrel.
Practical adaptation of this invention has shown its advantage more particularly in obtaining higher velocities with a given pressure than heretofore with the same pressure.
Such is shown, forI example, by the fact that a standard 30 06 Springeld riile, Yring cartridges loaded with smokeless powder (Hivel No. 2), and itted with a 173 grain boat-tailed bullet, was found to give a muzzle velocity of 1638 feet per second and a breech pressure of 33,700 pounds per square inch, when containing a unit charge of 25.5 gra-ins of the said smokeless powder. In comparison, a cartridgeidentical with thel above, except for the fact that the powder charge, of the same quality of powder, comprised 21.2 grains of loose powder and. 11.3 grains in a sealed copper capsule having a wall thickness of approximately .009 inch, or a total powder charge of 32.5 grains (which could be expected to give a much higher breech pressure if an undivided, loose charge), gave a velocity of 1862 feet per second and abreech pressure of. only 32,100 pounds per square inch, i. e. a breech pressure even lower than the normal unit charge, but producing a substantially higher velocity than the normal unit charge.
As illustrative of practical adaptation of this invention to shot gun shells, for example, results from the standpoint of shot velocity and breech pressures using the same shell,`cap, powder and shot charge as shown in the following table in comparison between a standard loading and loadings in accordance with this invention.
Shot ve- Breecli Smokeless powder charge 10cm, pressure Ft. per Lbs.
sec.
Standard-22.5 grams 926 10, 600. Embodylng the `invention-30.5 grains (10.0
thereof being in gelatin capsules) 1, 011 10, 700 37.8 grains (13.32 thereof being in gelatin capsules) 1, 019 9, 200
details may be made from the specific description above Without departing from the scope of the invention.
What I claim and desire to protect by Letters Patent is:
1. A propellant charge for guns comprising a mass of explosive comprising a portion of the total charge and a container formed from an incombustible material embedded in said mass and containing an explosive comprising another portion of the total charge.
2. A propellant charge for guns comprising a mass of relatively slow burning smokeless powder comprising a portion of the total charge and a container loosely .embedded in said mass of explosive and containing a relatively fast burning smokeless powder comprising another portion of the total charge.
3. A propellant charge for guns comprising .a mass of explosive comprising a portion of the total charge and a container loosely embedded in said mass of explosive and containing a smokeless powder comprising another portion of the total charge, the smokeless powder comprised in said mass and contained in said capsule having, re-
comprising a portion of the total ,charge and a container embedded in said mass and containing an untreated smokeless powder comprising another portion of the total charge.
6. A propellant charge for guns comprising a mass of explosive comprising a portion of the total charge, a container within said massof .explosive containing an explosive comprising another portion of the charge and a container within said rst mentioned container and containing n still another portion of said charge.
7. A propellant charge for guns comprising a,
mass of explosive comprising 'a portion of the total charge and a metallic container loosely embedded in said mass of explosive and containing an explosive comprising another portion of the charge.
8. In combination, a propellant charge for guns comprising a mass of explosive comprising a portion of the total charge and a container loosely vembedded in said mass of explosive and containing an explosive comprising another portion of the total charge and means for firing the said mass vof explosive, the said container being of a character such as to protect its contained charge from flame resultant from ignition of the said mass of explosive for a period after the ignition thereof by the igniting means therefor.
v 9. In combination, a propellant charge for guns comprising a mass of explosive comprising a portion of the total charge and a container containing an explosive comprising another portion of the total charge and means for firing the said mass of explosive, the said container being of a character such as to protect its contained charge from flame resultant from ignition of the said mass of explosive for aperiod after the ignition thereof by the igniting means therefor and of such a character as to conduct heat developed on burning of the said mass of explosive to its -contained charge for the ignition thereof at a time subsequent to the ignition of the said mass of explosive.
10. A propellant charge for guns comprising a mass of explosive comprising a portion of the total charge and a container formed from a combustible material embedded wholly in said mass of explosive and containing an explosive comprising another portion of the total charge.
11. A propellant charge for guns comprising a mass of explosive comprising a portion of the total charge and a. container formed from a combustible material embedded and freely movable within said mass of explosive and containing an explosive compris/ing another portion of the total
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Application Number | Priority Date | Filing Date | Title |
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US750623A US2072671A (en) | 1934-10-30 | 1934-10-30 | Ammunition and propellant charge therefor |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
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US750623A US2072671A (en) | 1934-10-30 | 1934-10-30 | Ammunition and propellant charge therefor |
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US2072671A true US2072671A (en) | 1937-03-02 |
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US750623A Expired - Lifetime US2072671A (en) | 1934-10-30 | 1934-10-30 | Ammunition and propellant charge therefor |
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Cited By (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2455080A (en) * | 1944-12-04 | 1948-11-30 | Powell | Ordnance chambrage and cartridge case |
US2935948A (en) * | 1958-02-14 | 1960-05-10 | American Potash & Chem Corp | Rocket igniter pellets |
US2995088A (en) * | 1959-06-29 | 1961-08-08 | Bermite Powder Company | Multi-stage igniter charge |
US3109375A (en) * | 1956-12-07 | 1963-11-05 | Atlantic Res Corp | Propellent grains |
US3143446A (en) * | 1959-11-27 | 1964-08-04 | Gen Electric | Propellant charge containing fluid encapsulations |
US3204560A (en) * | 1961-04-24 | 1965-09-07 | Lockheed Aircraft Corp | Solid rocket propellant containing metal encapsulated gas |
US3491690A (en) * | 1968-01-10 | 1970-01-27 | Verran Lane Knight | Water boosted shotshell |
US3613597A (en) * | 1964-01-16 | 1971-10-19 | North American Rockwell | Solid propellant grain |
US3706278A (en) * | 1971-02-25 | 1972-12-19 | Us Army | Distributed propulsion for guns |
US3724870A (en) * | 1970-02-18 | 1973-04-03 | Asahi Chemical Ind | Gas-producing device for an inflatable body-protecting bag on a high-speed vehicle |
US3811380A (en) * | 1958-01-30 | 1974-05-21 | Cava Ind | Rocket and propellant therefor |
US3938440A (en) * | 1973-01-18 | 1976-02-17 | Olin Corporation | Mixed propellant charge |
US4974487A (en) * | 1984-10-05 | 1990-12-04 | Gt-Devices | Plasma propulsion apparatus and method |
US5031541A (en) * | 1990-07-16 | 1991-07-16 | Olin Corporation | Stratified propellant charge barriers for small and medium caliber ammunition |
US5841062A (en) * | 1996-01-29 | 1998-11-24 | The United States Of America As Represented By The Secretary Of The Army | Tank cartridge |
US6748870B2 (en) | 2001-10-22 | 2004-06-15 | Armtec Defense Products Company | Ammunition round assembly with combustible cartridge case |
US6901866B2 (en) | 2001-11-27 | 2005-06-07 | Armtec Defense Products Company | Combustible cased telescoped ammunition assembly |
US20060032391A1 (en) * | 2004-08-13 | 2006-02-16 | Brune Neal W | Pyrotechnic systems and associated methods |
US20070289474A1 (en) * | 2006-04-07 | 2007-12-20 | Armtec Defense Products Co. | Ammunition assembly with alternate load path |
US20090308234A1 (en) * | 2005-10-11 | 2009-12-17 | Lennart Gustavsson | Method for producing propellant charges from a granulated propellant, preferably granulated powder, and propellant charges produced in accordance with the aforementioned method |
US20100274544A1 (en) * | 2006-03-08 | 2010-10-28 | Armtec Defense Products Co. | Squib simulator |
US8146502B2 (en) | 2006-01-06 | 2012-04-03 | Armtec Defense Products Co. | Combustible cartridge cased ammunition assembly |
US9182201B2 (en) | 2012-04-06 | 2015-11-10 | II Charles W. Coffman | Cartridge with rapidly increasing sequential ignitions for guns and ordnances |
US10767967B2 (en) | 2018-08-07 | 2020-09-08 | Thomas Faudree, IV | Device for controlling a rate of gas pressure increase in a gun barrel |
-
1934
- 1934-10-30 US US750623A patent/US2072671A/en not_active Expired - Lifetime
Cited By (35)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2455080A (en) * | 1944-12-04 | 1948-11-30 | Powell | Ordnance chambrage and cartridge case |
US3109375A (en) * | 1956-12-07 | 1963-11-05 | Atlantic Res Corp | Propellent grains |
US3811380A (en) * | 1958-01-30 | 1974-05-21 | Cava Ind | Rocket and propellant therefor |
US2935948A (en) * | 1958-02-14 | 1960-05-10 | American Potash & Chem Corp | Rocket igniter pellets |
US2995088A (en) * | 1959-06-29 | 1961-08-08 | Bermite Powder Company | Multi-stage igniter charge |
US3143446A (en) * | 1959-11-27 | 1964-08-04 | Gen Electric | Propellant charge containing fluid encapsulations |
US3204560A (en) * | 1961-04-24 | 1965-09-07 | Lockheed Aircraft Corp | Solid rocket propellant containing metal encapsulated gas |
US3613597A (en) * | 1964-01-16 | 1971-10-19 | North American Rockwell | Solid propellant grain |
US3491690A (en) * | 1968-01-10 | 1970-01-27 | Verran Lane Knight | Water boosted shotshell |
US3724870A (en) * | 1970-02-18 | 1973-04-03 | Asahi Chemical Ind | Gas-producing device for an inflatable body-protecting bag on a high-speed vehicle |
US3706278A (en) * | 1971-02-25 | 1972-12-19 | Us Army | Distributed propulsion for guns |
US3938440A (en) * | 1973-01-18 | 1976-02-17 | Olin Corporation | Mixed propellant charge |
USRE30002E (en) * | 1973-01-18 | 1979-05-22 | Olin Corporation | Mixed propellant charge |
US4974487A (en) * | 1984-10-05 | 1990-12-04 | Gt-Devices | Plasma propulsion apparatus and method |
US5031541A (en) * | 1990-07-16 | 1991-07-16 | Olin Corporation | Stratified propellant charge barriers for small and medium caliber ammunition |
US5841062A (en) * | 1996-01-29 | 1998-11-24 | The United States Of America As Represented By The Secretary Of The Army | Tank cartridge |
US6748870B2 (en) | 2001-10-22 | 2004-06-15 | Armtec Defense Products Company | Ammunition round assembly with combustible cartridge case |
US6901866B2 (en) | 2001-11-27 | 2005-06-07 | Armtec Defense Products Company | Combustible cased telescoped ammunition assembly |
US20060032391A1 (en) * | 2004-08-13 | 2006-02-16 | Brune Neal W | Pyrotechnic systems and associated methods |
US7363861B2 (en) | 2004-08-13 | 2008-04-29 | Armtec Defense Products Co. | Pyrotechnic systems and associated methods |
US20090223402A1 (en) * | 2004-08-13 | 2009-09-10 | Brune Neal W | Pyrotechnic systems and associated methods |
US7997178B2 (en) * | 2005-10-11 | 2011-08-16 | Bae Systems Bofors Ab | Method for producing propellant charges from a granulated propellant, preferably granulated powder, and propellant charges produced in accordance with the aforementioned method |
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