US2900914A - Incendiary projectile - Google Patents
Incendiary projectile Download PDFInfo
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- US2900914A US2900914A US720802A US72080258A US2900914A US 2900914 A US2900914 A US 2900914A US 720802 A US720802 A US 720802A US 72080258 A US72080258 A US 72080258A US 2900914 A US2900914 A US 2900914A
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- Prior art keywords
- incendiary
- nose
- projectile
- anvil
- mixture
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- 239000000203 mixture Substances 0.000 description 48
- 230000035945 sensitivity Effects 0.000 description 18
- 239000013078 crystal Substances 0.000 description 8
- 229910045601 alloy Inorganic materials 0.000 description 7
- 239000000956 alloy Substances 0.000 description 7
- SNAAJJQQZSMGQD-UHFFFAOYSA-N aluminum magnesium Chemical compound [Mg].[Al] SNAAJJQQZSMGQD-UHFFFAOYSA-N 0.000 description 7
- 239000000463 material Substances 0.000 description 7
- IWOUKMZUPDVPGQ-UHFFFAOYSA-N barium nitrate Chemical compound [Ba+2].[O-][N+]([O-])=O.[O-][N+]([O-])=O IWOUKMZUPDVPGQ-UHFFFAOYSA-N 0.000 description 6
- AXZAYXJCENRGIM-UHFFFAOYSA-J dipotassium;tetrabromoplatinum(2-) Chemical compound [K+].[K+].[Br-].[Br-].[Br-].[Br-].[Pt+2] AXZAYXJCENRGIM-UHFFFAOYSA-J 0.000 description 4
- 229910001487 potassium perchlorate Inorganic materials 0.000 description 4
- 239000007779 soft material Substances 0.000 description 4
- 239000007787 solid Substances 0.000 description 4
- DWPDSISGRAWLLV-JHZYRPMRSA-L calcium;(1r,4ar,4br,10ar)-1,4a-dimethyl-7-propan-2-yl-2,3,4,4b,5,6,10,10a-octahydrophenanthrene-1-carboxylate Chemical compound [Ca+2].C([C@@H]12)CC(C(C)C)=CC1=CC[C@@H]1[C@]2(C)CCC[C@@]1(C)C([O-])=O.C([C@@H]12)CC(C(C)C)=CC1=CC[C@@H]1[C@]2(C)CCC[C@@]1(C)C([O-])=O DWPDSISGRAWLLV-JHZYRPMRSA-L 0.000 description 3
- 239000000945 filler Substances 0.000 description 3
- 229910052751 metal Inorganic materials 0.000 description 3
- 239000002184 metal Substances 0.000 description 3
- 230000000149 penetrating effect Effects 0.000 description 3
- 239000002360 explosive Substances 0.000 description 2
- 239000004449 solid propellant Substances 0.000 description 2
- OYPRJOBELJOOCE-UHFFFAOYSA-N Calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 description 1
- 229910000737 Duralumin Inorganic materials 0.000 description 1
- 229910002651 NO3 Inorganic materials 0.000 description 1
- NHNBFGGVMKEFGY-UHFFFAOYSA-N Nitrate Chemical compound [O-][N+]([O-])=O NHNBFGGVMKEFGY-UHFFFAOYSA-N 0.000 description 1
- 229910052782 aluminium Inorganic materials 0.000 description 1
- FJMNNXLGOUYVHO-UHFFFAOYSA-N aluminum zinc Chemical compound [Al].[Zn] FJMNNXLGOUYVHO-UHFFFAOYSA-N 0.000 description 1
- 229910052788 barium Inorganic materials 0.000 description 1
- DSAJWYNOEDNPEQ-UHFFFAOYSA-N barium atom Chemical compound [Ba] DSAJWYNOEDNPEQ-UHFFFAOYSA-N 0.000 description 1
- 229910052791 calcium Inorganic materials 0.000 description 1
- 239000011575 calcium Substances 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000002708 enhancing effect Effects 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 230000035515 penetration Effects 0.000 description 1
- 229920000136 polysorbate Polymers 0.000 description 1
- 238000003825 pressing Methods 0.000 description 1
- 230000001681 protective effect Effects 0.000 description 1
- 239000000700 radioactive tracer Substances 0.000 description 1
- 238000011076 safety test Methods 0.000 description 1
- 238000004904 shortening Methods 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
- This invention is a continuation-in-part of my copending patent application, Serial No. 585,131, filed May 15, 1956 (abandoned as of March 26, 1958), and relates to incendiary projectiles, and more particularly toward enhancing the uniformity of sensitivity and performance of incendiary projectiles at long ranges.
- An armor piercing incendiary projectile is designed to penetrate a target, and in doing so, to ignite the incendiary material in the projectile. Thereafter, to have the burning incendiary material adhere to the bullet when it strikes the target in back of an outer protective shield, then setting fire to or exploding the protected materiel.
- Incendiary projectiles in the past, have functioned by having the outer jacket split open and allow the incendiary mixture to burn upon reaction with the air. More recently, incendiary mixes have been used which ignite upon impact of the projectile with the target. That is, the impact causes crystal shear of the incendiary mix explosive particles, that is, the generation of heat brought about by shear forces acting on the crystals of the incendiary mix, creating friction and releasing heat sufficient to ignite the solid fuel in the mix. The idea behind this arrangement devolved from the primer mixes, which functioned upon impact from a firing pin. However, where the primer mixes needed only J/10 or less ft. lbs.
- the projectile has decelerated, and the impact force at the target correspondingly reduced.
- the projectile must still be capable of penetrating as much as .150 inch of laminar Duralumin; the incendiary material must still ignite; and remain burning until after the primary, protected target is contacted.
- a projectile for the first time, a projectile is made which has a high degree of sensitivity and uniformity of functioning at long ranges, can successfully penetrate the target for which it is designed of the time, is drop safe from a distance of 40 feet, bore safe in a worn tube at extreme temperatures, incorporates a maximum amount of incendiary mixture without reducing sensitivity, and which can be easily adjusted in sensitivity for the desired target.
- the nose of the projectile forms the housing for the mix, while the anvil performs the function of the tiring pin.
- the shape of the forward portion of the anvil and the inner surface of the nose are such that the distance between them is constant over a wide angle, thus allowing for uniform crush-up in this area, resulting in uniform sensitivity.
- the T shape allows for the maximum amount of mix.
- Fig. 1 is an axial sectional view of the projectile assembly
- Fig. 2 shows another preferred loading of the nose section
- Fig. 3 shows the essence of the invention, the manner by which uniformity of functioning and sensitivity is achieved and maintained.
- Fig. l is shown the entire projectile assembly, where 10 is the penetrator, 15 is the projectile rotating band and 16 is the tracer cavity.
- An adapter 14 is assembled to the projectile body, and presents a threaded or interference t for the nose 11.
- the incendiary mix 17 is located around the anvil 12 which is positioned by its outer surface 19 being in close contact with the inner surface 21 of the nose.
- the nose is loaded with incendiary mixture in stages by using a former having a shape like that of the front end 22 of the anvil 12. Suicient mix is put in to form the controlled space 13, and then successive loads until the entire mixture is in the nose. The anvil 12 is then inserted and the nose screwed or pressed into the adapter. The mixture compacts until the nose is seated against the adapter by the action of the nose of the penetrator pressing against the anvil at 20.
- Fig. 1 shows an assembly using the usual 50-50 incendiary mixture. That is 50 parts by weight of barium nitrate, and 50 parts by Weight of a 50/50 alloy of magnesium-aluminum, in the usual powdered form.
- Fig. 2 is shown a preferred loading to further increase the efficiency and sensitivity of the projectile at long ranges.
- the loading of the nose is achieved in stages for the convenience of the loader.
- the first stage, or charge is a special mixture consisting of 49 parts by weight of 50/50 alloy of magnesium-aluminum, 49 parts by weight of potassium perchlorate, and 2 parts by weight of calcium resinate. Although 1-2 grains of this mixture in the tip would be sufiicient, more is used so that it fills the area 18, when the assembly is made.
- Fig. 3 shows the essence of the invention.
- the anvil is shaped as is the inside of the nose, so that the distance 13 is uniform over a large angle (a).
- the angle is made as large as possible so that the projectile functioning will be uniform over a wide range of impact angles.
- the distance can be made larger or smaller by shortening the anvil and reducing the diameter of the elongated portion 12.
- This invention then employs the age-old primer principle to function an incendiary projectile. It has been found that varying the incendiary composition to achieve sensitivity does not solve the problem of functioning uniformity at long ranges. However, by proper control of tolerances and manufacture of this invention, the space between the anvil and the nose can be kept within a very small tolerance. For instance, on the 20 mm. armor piercing-incendiary projectile, the space 13 is .030 inch, held to a tolerance of as small as ⁇ i.0015 inch. This achieves the uniformity of functioning of 90% or better against designated targets, while still passing the 40 ft. drop safety test.
- the space 13 can be determined to obtain a highly efficient projectile incorporating a maximum amount of incendiary mixture, insuring maximum uniformity of performance while at the same time insuring drop and bore safety.
- AP-I projectile now in use has a length of about 2.9 inches and incorporates a space 13 of .030 inch, or about1% of the total length, and an incendiary mix of 68 grains (by weight) consisting of 17 grains by weight of the more sensitive mix (potassium perchlorate, calcium resinate, magnesium-aluminum) and 51 grains by weight of the less sensitive 50-50 mixture, discussed above.
- the nose should be made of a reasonably soft material, such as an aluminum-zinc casting.
- the anvil should be sufficiently stiff to first allow crush-up of the nose in order to achieve crystal shear of the mixture in front of it but of a material sufficiently less hard than the penetrator so that it does not impede penetration.
- the sensitivity should generally fall within the range of 5-12 ft. lbs.
- the object of this invention is to present the combination of an incendiary and armor piercing projectile whereby the maximum amount of incendiary mixture is incorporated for increasing behind the plate effect while at the same time maintaining a high degree of sensitivity over a large range of impact angles and still not impeding the penetrating ability of the projectile.
- An armor piercing incendiary projectile of the type using crystal shear to ignite the incendiary mixture having a solid penetrator and circumferential band of soft material for imparting spin to the projectile, the combination therewith of the improvement for increasing the uniformity of sensitivity and functioning at long ranges and over a wide range of impact angles, said improvement comprising a nose of softer metal than said penetrator, an adapter secured to said penetrator for mounting said nose, an elongated anvil having a radially extended rear portion mounted slidably inside said adapter, in contact with said penetrator, and a forward extending portion having substantially the same contour as the inner surface of said nose such that the distance between said anvil and the inner surface of said nose is constant over a wide angle, said distance being controlled to a close tolerance by preloading the nose with incendiary mixture prior to assembly and by the length of said anvil such that the incendiary mix will ignite by crystal shear upon impact with the target but will still be safe
- a projectile according to claim l in which at least the portion between the anvil and the nose which is kept at a substantially constant distance, is loaded with a more sensitive incendiary mixture than the remaining volume of mixture.
- a projectile according to claim 3 in which the distance is adjusted to yield a minimum impact sensitivity of 5 to 12 foot pounds.
- a 20 mm. armor piercing incendiary projectile comprising a solid penetrator having a circumferential band of soft material for imparting spin to the projectile, a nose of softer metal than said penetrator, an adapter secured to said penetrator for mounting said nose, an elongated anvil having a radially extended rear portion mounted slidably inside said adapter in contact with said penetrator, and a forward extending portion having substantially the same contour as the inner surface of said nose such that a distance of .03 inch is maintained between said anvil and the inner surface of said nose Within a close tolerance and over a wide angle, said distance being controlled by preloading the nose with an incendiary mix subject to ignition by crystal shear, said mix consisting essentially of 50 parts by weight of barium nitrate and 50 parts by weight of a 50/50 alloy of powdered magnesium-aluminum, and by controlling the length of said anvil, said anvil being of sufliciently hard material to withstand
- a projectile according to claim 5 containing about 68 grains by weight of incendiary mixture.
- a 20 mm. armor piercing incendiary projectile comprising a solid penetrator having a circumferential band of soft material for imparting spin to the projectile, a nose of softer metal than said penetrator, an adapter secured to said penetrator for mounting said nose, and an elongated anvil having a radially extended rear portion mounted slidably inside said adapter in contact with said penetrator, a forward extending portion of said anvil having substantially the same contour as the inner surface of said nose such that a distance of 0.3 inch is maintained between said anvil and the inner surface of said nose within a close tolerance and over a wide angle, said distance being controlled by preloading the nose with an incendiary filler subject to ignition by crystal shear, said filler consisting of two mixtures, a first mixture consisting of 49 parts by weight of potassium perchlorate, 49 parts by Weight of 50/50 alloy of powdered mag- 5 nesium-aluminum and 2 parts by weight of calcium References Ci
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Description
Ag- 25., 1959 T. Q. clccoNE 2,900,914
INCENDIARY PROJECTILE Filed March 11, 1958 INVENTOR. THOMAS Q. CICCONE MMM/.MM
United States Patent O f INCENDIARY PROJECTILE Thomas Q. Ciccone, Langhorne, Pa., assignor to the United States of America as represented by the Secretary of the Army Application March 11, 1958, Serial No. 720,802
7 Claims. (Cl. 102-90) (Granted under Title 35, U.S. Code (1952), sec. 266) The invention described herein may be manufactured and used by or for the Government for governmental purposes without payment of any royalty thereon.
This invention is a continuation-in-part of my copending patent application, Serial No. 585,131, filed May 15, 1956 (abandoned as of March 26, 1958), and relates to incendiary projectiles, and more particularly toward enhancing the uniformity of sensitivity and performance of incendiary projectiles at long ranges.
An armor piercing incendiary projectile is designed to penetrate a target, and in doing so, to ignite the incendiary material in the projectile. Thereafter, to have the burning incendiary material adhere to the bullet when it strikes the target in back of an outer protective shield, then setting fire to or exploding the protected materiel.
Incendiary projectiles, in the past, have functioned by having the outer jacket split open and allow the incendiary mixture to burn upon reaction with the air. More recently, incendiary mixes have been used which ignite upon impact of the projectile with the target. That is, the impact causes crystal shear of the incendiary mix explosive particles, that is, the generation of heat brought about by shear forces acting on the crystals of the incendiary mix, creating friction and releasing heat sufficient to ignite the solid fuel in the mix. The idea behind this arrangement devolved from the primer mixes, which functioned upon impact from a firing pin. However, where the primer mixes needed only J/10 or less ft. lbs. of impact to result in ignition, this would not be safe to handle in an incendiary projectile, as it would function if dropped or if it balloted in a worn gun tube. To use incendiary mixes which were drop and bore safe required less sensitive mixes, and construction which utilized some means of obtaining crystal shear to generate the heat for ignition, which resulted in lack of uniformity of functioning and sensitivity.
In the past, there were two general ways of achieving what was then considered an efficient projectile. One way was to provide a hollow penetrator, filling it with incendiary mix, and loading it right to the nose of the projectile. The nose was then thinned to increase sensitivity to impact or another more sensitive mixture was inserted at the front of the main column of incendiary. Diculties with this design were in its lack of uniformity of sensitivity, not being drop or bore safe when sensitive mixes are used in the nose; and being unable, due to the hollow penetrator, to defeat the heavier aircraft armor in use in recent years, and the inefficient use of the incendiary mixture. The applicant has found that increasing the column of incendiary mixture does not increase ethciency.
The other way of achieving an efficient projectile was to work on the penetrating angle. That is, to incorporate a solid penetrator, and then have either a sensitive mix in front, or reduce the space between the penetrator and the nose, and thin out the nose section of the projectile so that functioning will occur by preferential failure of the nose resulting in a pinching of the explosive compo- Patented Aug. 25, 1959 nent of the mix to achieve the release of heat to ignite the solid fuel. This arrangement did not prove uniform in functioning at long ranges due to low impact forces and high angles of Obliquity dueto variation in column of mix compressed. Also when increasing the sensitivity, the distance between the penetrator and jacket is reduced, thereby substantially reducing the volume of incendiary in the nose of the projectile.
As a result of this, the greatest problem encountered was sensitivity at long ranges. At long ranges the projectile has decelerated, and the impact force at the target correspondingly reduced. The projectile must still be capable of penetrating as much as .150 inch of laminar Duralumin; the incendiary material must still ignite; and remain burning until after the primary, protected target is contacted.
According to this invention, for the first time, a projectile is made which has a high degree of sensitivity and uniformity of functioning at long ranges, can successfully penetrate the target for which it is designed of the time, is drop safe from a distance of 40 feet, bore safe in a worn tube at extreme temperatures, incorporates a maximum amount of incendiary mixture without reducing sensitivity, and which can be easily adjusted in sensitivity for the desired target.
These new results are achieved by employing the primer functioning principle. That is, by realizing that both incendiary projectiles and primers function essentially the same, by including in the projectile all the components found in a weapon system, designing the components so that they may be assembled in a `unique way such that the projectile is uniformly sensitive to impact over a wide angle of impacts and striking velocities, at the same time incorporating the maximum amount of incendiary mix, while still maintaining safety requirements. Since primer composition is too sensitive, the projectile was designed to function with both the standard incendiary mix and with a special preliminary igniting mix which is more sensitive than the usual incendiary mixes. The nose of the projectile forms the housing for the mix, while the anvil performs the function of the tiring pin. The shape of the forward portion of the anvil and the inner surface of the nose are such that the distance between them is constant over a wide angle, thus allowing for uniform crush-up in this area, resulting in uniform sensitivity. The T shape allows for the maximum amount of mix.
The specific nature of the invention as well as its advantages will be seen by referring to the drawings.
Fig. 1 is an axial sectional view of the projectile assembly;
Fig. 2 shows another preferred loading of the nose section; and
Fig. 3 shows the essence of the invention, the manner by which uniformity of functioning and sensitivity is achieved and maintained.
In Fig. l is shown the entire projectile assembly, where 10 is the penetrator, 15 is the projectile rotating band and 16 is the tracer cavity. An adapter 14 is assembled to the projectile body, and presents a threaded or interference t for the nose 11. The incendiary mix 17 is located around the anvil 12 which is positioned by its outer surface 19 being in close contact with the inner surface 21 of the nose.
The nose is loaded with incendiary mixture in stages by using a former having a shape like that of the front end 22 of the anvil 12. Suicient mix is put in to form the controlled space 13, and then successive loads until the entire mixture is in the nose. The anvil 12 is then inserted and the nose screwed or pressed into the adapter. The mixture compacts until the nose is seated against the adapter by the action of the nose of the penetrator pressing against the anvil at 20.
Fig. 1 shows an assembly using the usual 50-50 incendiary mixture. That is 50 parts by weight of barium nitrate, and 50 parts by Weight of a 50/50 alloy of magnesium-aluminum, in the usual powdered form.
In Fig. 2 is shown a preferred loading to further increase the efficiency and sensitivity of the projectile at long ranges. The loading of the nose is achieved in stages for the convenience of the loader. The first stage, or charge is a special mixture consisting of 49 parts by weight of 50/50 alloy of magnesium-aluminum, 49 parts by weight of potassium perchlorate, and 2 parts by weight of calcium resinate. Although 1-2 grains of this mixture in the tip would be sufiicient, more is used so that it fills the area 18, when the assembly is made.
Fig. 3 shows the essence of the invention. The anvil is shaped as is the inside of the nose, so that the distance 13 is uniform over a large angle (a). The angle is made as large as possible so that the projectile functioning will be uniform over a wide range of impact angles. The distance can be made larger or smaller by shortening the anvil and reducing the diameter of the elongated portion 12.
This invention then employs the age-old primer principle to function an incendiary projectile. It has been found that varying the incendiary composition to achieve sensitivity does not solve the problem of functioning uniformity at long ranges. However, by proper control of tolerances and manufacture of this invention, the space between the anvil and the nose can be kept within a very small tolerance. For instance, on the 20 mm. armor piercing-incendiary projectile, the space 13 is .030 inch, held to a tolerance of as small as `i.0015 inch. This achieves the uniformity of functioning of 90% or better against designated targets, while still passing the 40 ft. drop safety test.
The target to be defeated, and the impact velocities being known, with this invention the space 13 can be determined to obtain a highly efficient projectile incorporating a maximum amount of incendiary mixture, insuring maximum uniformity of performance while at the same time insuring drop and bore safety. For example, those skilled in the art know that a standardized 20 mm. AP-I projectile now in use has a length of about 2.9 inches and incorporates a space 13 of .030 inch, or about1% of the total length, and an incendiary mix of 68 grains (by weight) consisting of 17 grains by weight of the more sensitive mix (potassium perchlorate, calcium resinate, magnesium-aluminum) and 51 grains by weight of the less sensitive 50-50 mixture, discussed above.
The nose should be made of a reasonably soft material, such as an aluminum-zinc casting. The anvil should be sufficiently stiff to first allow crush-up of the nose in order to achieve crystal shear of the mixture in front of it but of a material sufficiently less hard than the penetrator so that it does not impede penetration.
The sensitivity should generally fall within the range of 5-12 ft. lbs.
The object of this invention is to present the combination of an incendiary and armor piercing projectile whereby the maximum amount of incendiary mixture is incorporated for increasing behind the plate effect while at the same time maintaining a high degree of sensitivity over a large range of impact angles and still not impeding the penetrating ability of the projectile.
I claim:
1. An armor piercing incendiary projectile of the type using crystal shear to ignite the incendiary mixture, having a solid penetrator and circumferential band of soft material for imparting spin to the projectile, the combination therewith of the improvement for increasing the uniformity of sensitivity and functioning at long ranges and over a wide range of impact angles, said improvement comprising a nose of softer metal than said penetrator, an adapter secured to said penetrator for mounting said nose, an elongated anvil having a radially extended rear portion mounted slidably inside said adapter, in contact with said penetrator, and a forward extending portion having substantially the same contour as the inner surface of said nose such that the distance between said anvil and the inner surface of said nose is constant over a wide angle, said distance being controlled to a close tolerance by preloading the nose with incendiary mixture prior to assembly and by the length of said anvil such that the incendiary mix will ignite by crystal shear upon impact with the target but will still be safe to handle, said anvil being of sufliciently hard material to withstand crush-up of said nose, but not so hard as to impede the penetrator, the entire space around said anvil and between said anvil and said nose being loaded with incendiary mixture.
2. A projectile according to claim l in which at least the portion between the anvil and the nose which is kept at a substantially constant distance, is loaded with a more sensitive incendiary mixture than the remaining volume of mixture.
3. A projectile according to claim 2 in which the more sensitive mixture consists essentially of 49 parts by weight of potassium perchlorate, 49 parts by weight of 50/50 alloy of powdered magnesium-aluminum and 2 parts by weight calcium resinate, the remaining portion of 4the filler being a mixture of 50 parts by weight barium nitrate and 50 parts by weight of a 50/50 alloy of powdered magnesium-aluminum.
4. A projectile according to claim 3 in which the distance is adjusted to yield a minimum impact sensitivity of 5 to 12 foot pounds.
5. A 20 mm. armor piercing incendiary projectile comprising a solid penetrator having a circumferential band of soft material for imparting spin to the projectile, a nose of softer metal than said penetrator, an adapter secured to said penetrator for mounting said nose, an elongated anvil having a radially extended rear portion mounted slidably inside said adapter in contact with said penetrator, and a forward extending portion having substantially the same contour as the inner surface of said nose such that a distance of .03 inch is maintained between said anvil and the inner surface of said nose Within a close tolerance and over a wide angle, said distance being controlled by preloading the nose with an incendiary mix subject to ignition by crystal shear, said mix consisting essentially of 50 parts by weight of barium nitrate and 50 parts by weight of a 50/50 alloy of powdered magnesium-aluminum, and by controlling the length of said anvil, said anvil being of sufliciently hard material to withstand crush-up of said nose but not so hard as to impede the penetrator, substantially the entire space between said anvil and the inner surface of said nose being filled with said incendiary mixture.
6. A projectile according to claim 5 containing about 68 grains by weight of incendiary mixture.
7. A 20 mm. armor piercing incendiary projectile comprising a solid penetrator having a circumferential band of soft material for imparting spin to the projectile, a nose of softer metal than said penetrator, an adapter secured to said penetrator for mounting said nose, and an elongated anvil having a radially extended rear portion mounted slidably inside said adapter in contact with said penetrator, a forward extending portion of said anvil having substantially the same contour as the inner surface of said nose such that a distance of 0.3 inch is maintained between said anvil and the inner surface of said nose within a close tolerance and over a wide angle, said distance being controlled by preloading the nose with an incendiary filler subject to ignition by crystal shear, said filler consisting of two mixtures, a first mixture consisting of 49 parts by weight of potassium perchlorate, 49 parts by Weight of 50/50 alloy of powdered mag- 5 nesium-aluminum and 2 parts by weight of calcium References Cited in the file of this patent resinate, used as a preliminary igniter to achieve a minimum impact sensitivity of 5-12 foot pounds, and a UNITED STATES PATENTS second mixture consisting of 50 parts by Weight of barium 1,380,773 Clay Junek 7, 1921 nitrate and 50 parts by Weight of a 50/50 alloy of 5 2409 380 Nichols Oct 15 1946 powdered magnesium-aluminum, and by controlling the 2'446082 D. "u" length of said anvil, said anvil being of suciently hard mm July 27 1948 material to withstand crush-up of said nose but not so 2,459,175 Moore Jan- 18: 1949 hard as -to impede the penetrator, the entire space be- 2,532,323 Miller Dec. 5, 1950 tween said anvil and the inner surface of said nose being 10 lled with said incendiary ller.
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US720802A US2900914A (en) | 1958-03-11 | 1958-03-11 | Incendiary projectile |
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US720802A US2900914A (en) | 1958-03-11 | 1958-03-11 | Incendiary projectile |
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Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3096715A (en) * | 1959-01-19 | 1963-07-09 | Brevets Aero Mecaniques | Armor-piercing projectiles |
US3361066A (en) * | 1964-12-24 | 1968-01-02 | Dynamit Nobel Ag | Practice shell |
US3374741A (en) * | 1965-12-28 | 1968-03-26 | Army Usa | Spotting charge |
US3645208A (en) * | 1970-02-17 | 1972-02-29 | Us Army | Fuzeless target practice cartridge |
US3720169A (en) * | 1971-03-30 | 1973-03-13 | Us Army | Incendiary projectile for smooth bore special purpose individual weapon |
EP0531697A2 (en) * | 1991-08-01 | 1993-03-17 | Raufoss A/S | A multipurpose projectile and a method of making it |
US6105505A (en) * | 1998-06-17 | 2000-08-22 | Lockheed Martin Corporation | Hard target incendiary projectile |
US20170299356A1 (en) * | 2016-04-18 | 2017-10-19 | Michael A. Stakes | Armor-piercing projectile |
EP4204756A4 (en) * | 2020-08-25 | 2024-10-16 | General Dynamics Ots Canada Inc | Spotter ammunition projectile and method for making the same |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1380773A (en) * | 1918-11-20 | 1921-06-07 | Wallace L Clay | Armor-piercing, spotlight, and incendiary bullet |
US2409380A (en) * | 1925-03-21 | 1946-10-15 | Nasa | Spotting projectiles |
US2446082A (en) * | 1941-09-15 | 1948-07-27 | Dixon Cecil Aubrey | Incendiary projectile |
US2459175A (en) * | 1941-08-26 | 1949-01-18 | Wiley T Moore | Explosive bullet |
US2532323A (en) * | 1942-03-30 | 1950-12-05 | Jr George A Miller | Bullet |
-
1958
- 1958-03-11 US US720802A patent/US2900914A/en not_active Expired - Lifetime
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1380773A (en) * | 1918-11-20 | 1921-06-07 | Wallace L Clay | Armor-piercing, spotlight, and incendiary bullet |
US2409380A (en) * | 1925-03-21 | 1946-10-15 | Nasa | Spotting projectiles |
US2459175A (en) * | 1941-08-26 | 1949-01-18 | Wiley T Moore | Explosive bullet |
US2446082A (en) * | 1941-09-15 | 1948-07-27 | Dixon Cecil Aubrey | Incendiary projectile |
US2532323A (en) * | 1942-03-30 | 1950-12-05 | Jr George A Miller | Bullet |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3096715A (en) * | 1959-01-19 | 1963-07-09 | Brevets Aero Mecaniques | Armor-piercing projectiles |
US3361066A (en) * | 1964-12-24 | 1968-01-02 | Dynamit Nobel Ag | Practice shell |
US3374741A (en) * | 1965-12-28 | 1968-03-26 | Army Usa | Spotting charge |
US3645208A (en) * | 1970-02-17 | 1972-02-29 | Us Army | Fuzeless target practice cartridge |
US3720169A (en) * | 1971-03-30 | 1973-03-13 | Us Army | Incendiary projectile for smooth bore special purpose individual weapon |
EP0531697A2 (en) * | 1991-08-01 | 1993-03-17 | Raufoss A/S | A multipurpose projectile and a method of making it |
EP0531697A3 (en) * | 1991-08-01 | 1994-03-23 | Raufoss As | |
US6105505A (en) * | 1998-06-17 | 2000-08-22 | Lockheed Martin Corporation | Hard target incendiary projectile |
US20170299356A1 (en) * | 2016-04-18 | 2017-10-19 | Michael A. Stakes | Armor-piercing projectile |
US10436557B2 (en) * | 2016-04-18 | 2019-10-08 | Ammo Technologies, Inc. | Armor-piercing projectile |
EP4204756A4 (en) * | 2020-08-25 | 2024-10-16 | General Dynamics Ots Canada Inc | Spotter ammunition projectile and method for making the same |
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