US2532323A - Bullet - Google Patents
Bullet Download PDFInfo
- Publication number
- US2532323A US2532323A US436818A US43681842A US2532323A US 2532323 A US2532323 A US 2532323A US 436818 A US436818 A US 436818A US 43681842 A US43681842 A US 43681842A US 2532323 A US2532323 A US 2532323A
- Authority
- US
- United States
- Prior art keywords
- bullet
- jacket
- body portion
- shoulder
- ogive
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
Links
- 239000000463 material Substances 0.000 description 10
- 229910052751 metal Inorganic materials 0.000 description 6
- 239000002184 metal Substances 0.000 description 5
- 239000000203 mixture Substances 0.000 description 5
- 229910000831 Steel Inorganic materials 0.000 description 4
- 230000000977 initiatory effect Effects 0.000 description 4
- 230000035515 penetration Effects 0.000 description 4
- 239000010959 steel Substances 0.000 description 4
- 239000007800 oxidant agent Substances 0.000 description 3
- 229910001209 Low-carbon steel Inorganic materials 0.000 description 2
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 2
- 229910052782 aluminium Inorganic materials 0.000 description 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 2
- 238000010304 firing Methods 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 229910052749 magnesium Inorganic materials 0.000 description 2
- 239000011777 magnesium Substances 0.000 description 2
- 239000012255 powdered metal Substances 0.000 description 2
- 230000035945 sensitivity Effects 0.000 description 2
- ZSLUVFAKFWKJRC-IGMARMGPSA-N 232Th Chemical compound [232Th] ZSLUVFAKFWKJRC-IGMARMGPSA-N 0.000 description 1
- 229910001369 Brass Inorganic materials 0.000 description 1
- 229910052684 Cerium Inorganic materials 0.000 description 1
- XTEGARKTQYYJKE-UHFFFAOYSA-M Chlorate Chemical class [O-]Cl(=O)=O XTEGARKTQYYJKE-UHFFFAOYSA-M 0.000 description 1
- 229910000570 Cupronickel Inorganic materials 0.000 description 1
- 229910000978 Pb alloy Inorganic materials 0.000 description 1
- 229910052776 Thorium Inorganic materials 0.000 description 1
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 1
- 229910045601 alloy Inorganic materials 0.000 description 1
- 239000000956 alloy Substances 0.000 description 1
- 239000010951 brass Substances 0.000 description 1
- GWXLDORMOJMVQZ-UHFFFAOYSA-N cerium Chemical compound [Ce] GWXLDORMOJMVQZ-UHFFFAOYSA-N 0.000 description 1
- ZCDOYSPFYFSLEW-UHFFFAOYSA-N chromate(2-) Chemical class [O-][Cr]([O-])(=O)=O ZCDOYSPFYFSLEW-UHFFFAOYSA-N 0.000 description 1
- 230000000295 complement effect Effects 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 230000003467 diminishing effect Effects 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 239000000945 filler Substances 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 150000002823 nitrates Chemical class 0.000 description 1
- 239000008188 pellet Substances 0.000 description 1
- VLTRZXGMWDSKGL-UHFFFAOYSA-N perchloric acid Chemical class OCl(=O)(=O)=O VLTRZXGMWDSKGL-UHFFFAOYSA-N 0.000 description 1
- 238000009527 percussion Methods 0.000 description 1
- 150000002978 peroxides Chemical class 0.000 description 1
- 239000000843 powder Substances 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 230000003014 reinforcing effect Effects 0.000 description 1
- 230000000284 resting effect Effects 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 229910052725 zinc Inorganic materials 0.000 description 1
- 239000011701 zinc Substances 0.000 description 1
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B12/00—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
- F42B12/02—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
- F42B12/36—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information
- F42B12/44—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect for dispensing materials; for producing chemical or physical reaction; for signalling ; for transmitting information of incendiary type
Definitions
- the bullet of the invention provides a reinforcement in the form of an inner sleeve which is efficacious in many respects even though the precise phenomena basically respon sible for its successful employment are n'ot enf tirel'y understood.
- insert 3 nested within the jacket and terminating in "the ogival portion may be of any desired material such as brass, steel plastic,.etc;, dependent on the type of functioning desired.
- a metal body is to be preferred, and for very hard materials, like light armor, a steel body which can be heat treated to increase the hardness and strength'should be used;
- a in Figure 1, the base closure 4 for the body is integral therewith-
- a central annular depression 5 is formed in the body to receive a crimp "I3 in the jacket for keying the body tif) the jacket.
- the jacket is c rimped over the rear of the body as shown at 5.
- U H p In Figure 2 is Shawn a bullet having a seria rate base closure.
- This comprises a shaped cup 7 of suitable material, preferably of metal having sufiicient ductility to be formed to the desired shape.
- This closure may be used both for sealing the base of the bullet against leakage of the chamber gas into the jacket which would disrupt the jacket, and for providing a means for adjusting the longitudinal ballistic balance of the bullet.
- the incendiary composition 8 may consist of a mixture of powdered metal or metals, such as magnesium, aluminum, zinc, cerium, thorium, or a combination of them, with an oxidizing agent or agents, such as metallic or non-metallic chlorates, perchlorates, nitrates, chromates, permanganates or peroxides.
- an oxidizing agent or agents such as metallic or non-metallic chlorates, perchlorates, nitrates, chromates, permanganates or peroxides.
- Projectiles which have been assembled in the manner described in the foregoing description, when fired from a weapon at an appropriate velocity will function with a flash of light and generate sufiicient flame to ignite combustible material, such as gasoline vapor when the projectile strikes an object offering resistance to penetration equal to thin mild steel.
- a lead plug 9 is shown behind the incendiary material in the tubular body, which serves as a pressure-communicating medium during loading, as a filler after the compressing operation is completed and as a further protection for the incendiary charge against firing shocks.
- This plug may first be inserted in the form of a ball which is subsequently shaped by pressure to the form of the tube center, or it may be inserted in any convenient original form.
- a shoulder it is provided on the inner wall of the jacket to form a stop for the body insert, and in order that the shoulder may be located in the thicker portion of the jacket, the point of contact for this shoulder is located on the body insert somewhat behind the forward end, leaving a reduced portion 1 I extending into the ogive to cooperate with the nose in initiating the composition on impact in the required manner.
- the body insert is closed at the rear as in Figure 1.
- the body insert is formed with a shoulder 12 at each end, the rear one resting on the rim of the closure cap.
- the two ends are symmetrical and this presents an advantage since either end may be inserted first in assembling.
- a projectile comprising a tubular body portion, a jacket fitted over said body portion, and tapering to an ogive in front of said body portion, a rearwardly facing annular shoulder in the inner wall of said jacket and a forwardly facing annular shoulder on the outer wall of said tubular body portion fitted on said shoulder on said jacket.
- a projectile as recited in claim 4 the two ends of said body portion being identical.
- a projectile as recited in claim 4 the two ends of said body portion being identical, a cap fitting over the rearward end of said body portion and filling the space formed by said frustoconical reduced end and said jacket, said jacket extending over the rearward end of said cap, said ogive and bore of said body portion forming a single chamber adapted to be filled with a charge.
- a projectile comprising a tubular body portion, a jacket fitted over and completely inclosing the side walls of said .body portion and tapering to an ogive forwardly of said body portion, the wall of said jacket being weakened by a reduction in wall thickness forwardly of said body portion, a charge in said ogive, a boattailed rear end on said tubular body portion, a closure cup with a skirt complementary to said boat-tailed end and nesting therewith and with the jacket, said jacket being turned over the base of said closure cup.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
Description
Dec. 5, 1950 e. A. MILLER, JR
BULLET Filed March 30, 1942 Patented Dec. 5
* UNITED PATENT o BULLET marge A. "time, Jr., weenie, staircases-Matteo, i942, seen its. new males. (01. 102-90) (eases fingertip act of March 3, 1 883, as amended April "30, 1928; 370 O. G. 757) The invention described Herein may be manufactured and used by or for the Government for governmental purposes, Without the payment to me of any royalty thereon. r I r r This invention relates to a bullet, and in particular to a bullet for use with small and medium arms. While the bullet may be loaded partly or wholly with high ekplosive, it is intended principally as a carrierfor incendiarymaterial.
a In a properly designed bu llet the modern types of incendiary compositions will ignite on impact Without any special percussion mechanism. The conditions of intended use of the bullet will in large measure affect the design thereof For example, a successfulattack on the gasoline tank of an airplane requires that the incendiary powers of a bullet be effective after it has. passed through an outer armor and traversed some distance therebeyond, This; maybe accomplished by delaying ignition beyond initial impact or by maintaining the incendiary outburst for a time after initiation. The bullet of the invention is well adapted to accomplish the latter although it is not intended tobe limited to such functioning as will appear as the description proceeds.
It is known to use a hollow bullet with thin nose and filled with incendiary material. Such bullets, however, are not designed for penetration, but areentirely collapsible on impact and therefore limited in use with respect to present day requirements. The bullet of the invention provides a reinforcement in the form of an inner sleeve which is efficacious in many respects even though the precise phenomena basically respon sible for its successful employment are n'ot enf tirel'y understood. It would appear, however; that the reinforcing sleeve serves to retain the form of the main body of the bullet while penetration of the target is effected after initiation, and it would further appear that there is some sort of coaction between the forward edge of the sleeve and the ogive which .conspi'r'es to pro'd'u ce a more effective initiation of the incendiary cornposition than is usual with a simple, loaded, hollow shell, the sleeve being more or less free to advance not only with the bullet body but also in advance thereof as the ogive is checked in flight and collapsed.
It is therefore an object of the invention to produce a charged bullet which will preserve its body form during penetration.
It is a further object of the invention to produce a reinforced incendiary bullet.
It is a further object of the invention to pro- 2 dude a hollow bullet having an inr'ierf'sleeve freinforcement movable relative to the body of the bullet. H
It is a fii'rtlierdbjct of the invention to "reducean incendiary bullet effective to ignite a target after pnetratioi'i 'of an outer 'a'rnior thereon. I r r v The 'js'p'ecific nature of the inventionas other objects and. advantages thereof will clearly appear from a'description of a preferredgembodiiment as shown in the accompanying drawings in n a, I. ,w, u .i I Figures 1 to '4 axial'se ctional views of buli c mmi -on me a Referring to the drawing by characters of ref erence eme-sh wn in s re. l b atr d bullet comprising a jacket i which may =be giild; ing metal, cupronickel, mild steel or coated steel p ovided thatthe thickness near the nose canbcp o' uce t he e r d rum i ns .T e thickness of the metal :near the nose of thejacket determines the sensitivity of the projectile to functioning onimpact. Preferably th-isreduced thickness is obtained through ;a gradual diminishing of the jacket thickness in the ogival portion fi. A tubular body. insert 3; nested within the jacket and terminating in "the ogival portion may be of any desired material such as brass, steel plastic,.etc;, dependent on the type of functioning desired. Where metallic objects are to be penetrated, a metal body is to be preferred, and for very hard materials, like light armor, a steel body which can be heat treated to increase the hardness and strength'should be used; A in Figure 1, the base closure 4 for the body is integral therewith- A central annular depression 5 is formed in the body to receive a crimp "I3 in the jacket for keying the body tif) the jacket. The jacket is c rimped over the rear of the body as shown at 5. Obviously the incendiary material will be loaded partly ti-re ogive as preformed pellets or otherwise, and partly in the tubulary body prior to insertion of the body into tl'ieiacket, U H p In Figure 2 is Shawn a bullet having a seria rate base closure. This comprises a shaped cup 7 of suitable material, preferably of metal having sufiicient ductility to be formed to the desired shape. This closure may be used both for sealing the base of the bullet against leakage of the chamber gas into the jacket which would disrupt the jacket, and for providing a means for adjusting the longitudinal ballistic balance of the bullet. For example, where a light material is needed, aluminum or magnesium or their alloys could be used, and where a heavy material is needed, lead or some lead alloy could be employed. Thus, any material having the desired ductility, specific gravity and resistance to disintegration by the explosive gases in the weapon would be suitable.
The incendiary composition 8 may consist of a mixture of powdered metal or metals, such as magnesium, aluminum, zinc, cerium, thorium, or a combination of them, with an oxidizing agent or agents, such as metallic or non-metallic chlorates, perchlorates, nitrates, chromates, permanganates or peroxides. The sensitivity of the mix-- ture to ignition upon impact can be adjusted by varying the amount of oxidizing agent and by the selection of the combination of metal powders.
Projectiles which have been assembled in the manner described in the foregoing description, when fired from a weapon at an appropriate velocity will function with a flash of light and generate sufiicient flame to ignite combustible material, such as gasoline vapor when the projectile strikes an object offering resistance to penetration equal to thin mild steel.
A lead plug 9 is shown behind the incendiary material in the tubular body, which serves as a pressure-communicating medium during loading, as a filler after the compressing operation is completed and as a further protection for the incendiary charge against firing shocks. This plug may first be inserted in the form of a ball which is subsequently shaped by pressure to the form of the tube center, or it may be inserted in any convenient original form.
In order to further obviate any danger of the jacket stripping from the body insert on firing, the forms shown in Figures 3 and 4 are provided. A shoulder it is provided on the inner wall of the jacket to form a stop for the body insert, and in order that the shoulder may be located in the thicker portion of the jacket, the point of contact for this shoulder is located on the body insert somewhat behind the forward end, leaving a reduced portion 1 I extending into the ogive to cooperate with the nose in initiating the composition on impact in the required manner.
In Figure 3 the body insert is closed at the rear as in Figure 1. In Figure 4 the body insert is formed with a shoulder 12 at each end, the rear one resting on the rim of the closure cap. In this body insert the two ends are symmetrical and this presents an advantage since either end may be inserted first in assembling.
I claim:
1. A projectile comprising a tubular body portion, a jacket fitted over said body portion, and tapering to an ogive in front of said body portion, a rearwardly facing annular shoulder in the inner wall of said jacket and a forwardly facing annular shoulder on the outer wall of said tubular body portion fitted on said shoulder on said jacket.
2. In a projectile according to claim 1, a boattailed portion on said tubular body member in advance of said shoulder on said body member, said boat-tailed portion being spaced from the inner wall of said jacket.
3. In a projectile according to claim 1, a rearwardly facing annular shoulder on said tubular body portion and a cup member closing the rear end of said tubular body portion and engaging said rearwardly facing annular shoulder by its rim.
4. In a projectile, a steel tubular body portion having a closed rearward end, said portion having an externally reduced frusto-conical end forming a forwardly-facing shoulder, a jacket fitting and enclosing said body portion and including an ogive extending forwardly of the extreme forward end of said body portion, said jacket having a rearwardly-facing, internal shoulder fitting against the shoulder of said body portion and having a gradually decreasing wall thickness from said shoulder forwardly to the tip of said ogive, said ogive and body portion forming a single chamber adapted to be filled with a charge. 7
5. A projectile as recited in claim 4, the two ends of said body portion being identical.
6. A projectile as recited in claim 4, the two ends of said body portion being identical, a cap fitting over the rearward end of said body portion and filling the space formed by said frustoconical reduced end and said jacket, said jacket extending over the rearward end of said cap, said ogive and bore of said body portion forming a single chamber adapted to be filled with a charge.
7. A projectile comprising a tubular body portion, a jacket fitted over and completely inclosing the side walls of said .body portion and tapering to an ogive forwardly of said body portion, the wall of said jacket being weakened by a reduction in wall thickness forwardly of said body portion, a charge in said ogive, a boattailed rear end on said tubular body portion, a closure cup with a skirt complementary to said boat-tailed end and nesting therewith and with the jacket, said jacket being turned over the base of said closure cup.
GEORGE A. MILLER, JR.
REFERENCES CITED The following references are of record in the file of this patent:
UNITED STATES PATENTS Number Name Date 2,288,627 Kowalski July 7, 1942 2,426,997 Gray Sept. 9, 1947 2,459,175 Moore Jan. 18, 1949 2,475,632 Moore July 12, 1949 FOREIGN PATENTS Number Country Date 20,970 Great Britain of 1889 764,833 France Mar. 12, 1934 414,005 Great Britain July 26, 1934
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US436818A US2532323A (en) | 1942-03-30 | 1942-03-30 | Bullet |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US436818A US2532323A (en) | 1942-03-30 | 1942-03-30 | Bullet |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2532323A true US2532323A (en) | 1950-12-05 |
Family
ID=23733943
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US436818A Expired - Lifetime US2532323A (en) | 1942-03-30 | 1942-03-30 | Bullet |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2532323A (en) |
Cited By (20)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2801590A (en) * | 1951-06-14 | 1957-08-06 | Claire C Balke | Pyrophoric element |
| US2900914A (en) * | 1958-03-11 | 1959-08-25 | Thomas Q Ciccone | Incendiary projectile |
| US3028808A (en) * | 1958-01-09 | 1962-04-10 | Samuel J Porter | Armor piercing incendiary projectile |
| US3291049A (en) * | 1952-05-22 | 1966-12-13 | Aaron L Hitchens | Impact spotter bullet |
| US3485171A (en) * | 1967-10-23 | 1969-12-23 | Us Army | Stabilizing a smoke shell with an interior plastic liner |
| US3720169A (en) * | 1971-03-30 | 1973-03-13 | Us Army | Incendiary projectile for smooth bore special purpose individual weapon |
| US3861311A (en) * | 1973-07-13 | 1975-01-21 | Us Air Force | Plastic semi armor piercing incendiary projectile |
| US4103620A (en) * | 1975-11-12 | 1978-08-01 | Sarmac S.A. | Projectile explosive |
| US4625650A (en) * | 1984-10-29 | 1986-12-02 | Olin Corporation | Multiple effect ammunition |
| EP0260245A3 (en) * | 1986-09-04 | 1988-10-05 | Fabrique Nationale Herstal En Abrege Fn Societe Anonyme | Multiple-effect projectile multiple-effect projectile |
| US4876964A (en) * | 1986-05-29 | 1989-10-31 | Raufoss A/S | Projectile and method of making it |
| US5020439A (en) * | 1989-05-05 | 1991-06-04 | Olin Corporation | Projectile having improved baseplug |
| US5728968A (en) * | 1989-08-24 | 1998-03-17 | Primex Technologies, Inc. | Armor penetrating projectile |
| US5945629A (en) * | 1996-12-10 | 1999-08-31 | Diehl Stiftung & Co. | Fuseless ballistic explosive projectile |
| US20040055502A1 (en) * | 2002-09-20 | 2004-03-25 | Lockheed Martin Corporation | Penetrator and method for using same |
| US20040055501A1 (en) * | 2002-09-20 | 2004-03-25 | Hunn David L. | Penetrator and method for using same |
| US20050081706A1 (en) * | 2002-01-08 | 2005-04-21 | Alford Sidney C. | Device for the disruption of explosive ordnance |
| US20120167793A1 (en) * | 2000-02-23 | 2012-07-05 | Alliant Techsystems Inc. | Reactive material enhanced projectiles and related methods |
| US8960094B1 (en) | 2013-10-18 | 2015-02-24 | BPOE Associates, Trustee for Bullet push-out explosive CRT Trust | Bullet with push-out explosive |
| US20190017791A1 (en) * | 2017-03-07 | 2019-01-17 | U.S. Army Research Laboratory Attn: Rdrl-Loc-I | Reduced Jacketed Bullet Bore Resistance |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR764833A (en) * | 1933-02-23 | 1934-05-29 | Soc Fr Munitions De Chasse | Further training in the manufacture of projectiles for firearms |
| GB414005A (en) * | 1933-04-07 | 1934-07-26 | Edgar William Brandt | Improvements in or relating to explosive projectiles |
| US2288627A (en) * | 1939-02-21 | 1942-07-07 | Jr Frank Kowalski | Bullet |
| US2426997A (en) * | 1941-03-10 | 1947-09-09 | John C Gray | Projectile |
| US2459175A (en) * | 1941-08-26 | 1949-01-18 | Wiley T Moore | Explosive bullet |
| US2475632A (en) * | 1942-03-19 | 1949-07-12 | Wiley T Moore | Bullet |
-
1942
- 1942-03-30 US US436818A patent/US2532323A/en not_active Expired - Lifetime
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR764833A (en) * | 1933-02-23 | 1934-05-29 | Soc Fr Munitions De Chasse | Further training in the manufacture of projectiles for firearms |
| GB414005A (en) * | 1933-04-07 | 1934-07-26 | Edgar William Brandt | Improvements in or relating to explosive projectiles |
| US2288627A (en) * | 1939-02-21 | 1942-07-07 | Jr Frank Kowalski | Bullet |
| US2426997A (en) * | 1941-03-10 | 1947-09-09 | John C Gray | Projectile |
| US2459175A (en) * | 1941-08-26 | 1949-01-18 | Wiley T Moore | Explosive bullet |
| US2475632A (en) * | 1942-03-19 | 1949-07-12 | Wiley T Moore | Bullet |
Cited By (25)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2801590A (en) * | 1951-06-14 | 1957-08-06 | Claire C Balke | Pyrophoric element |
| US3291049A (en) * | 1952-05-22 | 1966-12-13 | Aaron L Hitchens | Impact spotter bullet |
| US3028808A (en) * | 1958-01-09 | 1962-04-10 | Samuel J Porter | Armor piercing incendiary projectile |
| US2900914A (en) * | 1958-03-11 | 1959-08-25 | Thomas Q Ciccone | Incendiary projectile |
| US3485171A (en) * | 1967-10-23 | 1969-12-23 | Us Army | Stabilizing a smoke shell with an interior plastic liner |
| US3720169A (en) * | 1971-03-30 | 1973-03-13 | Us Army | Incendiary projectile for smooth bore special purpose individual weapon |
| US3861311A (en) * | 1973-07-13 | 1975-01-21 | Us Air Force | Plastic semi armor piercing incendiary projectile |
| US4103620A (en) * | 1975-11-12 | 1978-08-01 | Sarmac S.A. | Projectile explosive |
| US4625650A (en) * | 1984-10-29 | 1986-12-02 | Olin Corporation | Multiple effect ammunition |
| US4876964A (en) * | 1986-05-29 | 1989-10-31 | Raufoss A/S | Projectile and method of making it |
| EP0260245A3 (en) * | 1986-09-04 | 1988-10-05 | Fabrique Nationale Herstal En Abrege Fn Societe Anonyme | Multiple-effect projectile multiple-effect projectile |
| US5020439A (en) * | 1989-05-05 | 1991-06-04 | Olin Corporation | Projectile having improved baseplug |
| US5728968A (en) * | 1989-08-24 | 1998-03-17 | Primex Technologies, Inc. | Armor penetrating projectile |
| US5945629A (en) * | 1996-12-10 | 1999-08-31 | Diehl Stiftung & Co. | Fuseless ballistic explosive projectile |
| EP0848228A3 (en) * | 1996-12-10 | 2000-04-26 | Diehl Stiftung & Co. | Ballistic high-explosive type projectile without a fuze |
| US20120167793A1 (en) * | 2000-02-23 | 2012-07-05 | Alliant Techsystems Inc. | Reactive material enhanced projectiles and related methods |
| US9103641B2 (en) * | 2000-02-23 | 2015-08-11 | Orbital Atk, Inc. | Reactive material enhanced projectiles and related methods |
| US9982981B2 (en) | 2000-02-23 | 2018-05-29 | Orbital Atk, Inc. | Articles of ordnance including reactive material enhanced projectiles, and related methods |
| US20050081706A1 (en) * | 2002-01-08 | 2005-04-21 | Alford Sidney C. | Device for the disruption of explosive ordnance |
| US7299735B2 (en) * | 2002-01-08 | 2007-11-27 | Alford Sidney C | Device for the disruption of explosive ordnance |
| US20040055502A1 (en) * | 2002-09-20 | 2004-03-25 | Lockheed Martin Corporation | Penetrator and method for using same |
| US20040055501A1 (en) * | 2002-09-20 | 2004-03-25 | Hunn David L. | Penetrator and method for using same |
| US6843179B2 (en) | 2002-09-20 | 2005-01-18 | Lockheed Martin Corporation | Penetrator and method for using same |
| US8960094B1 (en) | 2013-10-18 | 2015-02-24 | BPOE Associates, Trustee for Bullet push-out explosive CRT Trust | Bullet with push-out explosive |
| US20190017791A1 (en) * | 2017-03-07 | 2019-01-17 | U.S. Army Research Laboratory Attn: Rdrl-Loc-I | Reduced Jacketed Bullet Bore Resistance |
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