WO1987000263A1 - Tracer ammunition - Google Patents

Tracer ammunition Download PDF

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Publication number
WO1987000263A1
WO1987000263A1 PCT/US1985/001321 US8501321W WO8700263A1 WO 1987000263 A1 WO1987000263 A1 WO 1987000263A1 US 8501321 W US8501321 W US 8501321W WO 8700263 A1 WO8700263 A1 WO 8700263A1
Authority
WO
WIPO (PCT)
Prior art keywords
pyrotechnic
tracer
column
round
diameter
Prior art date
Application number
PCT/US1985/001321
Other languages
French (fr)
Inventor
Thomas E. De Phillipo
James F. Kowalick
Original Assignee
Lsi Technologies, Inc.
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Priority to US06/507,063 priority Critical patent/US4528911A/en
Application filed by Lsi Technologies, Inc. filed Critical Lsi Technologies, Inc.
Priority to PCT/US1985/001321 priority patent/WO1987000263A1/en
Priority to DE8686900682T priority patent/DE3586786D1/en
Priority to EP86900682A priority patent/EP0229763B1/en
Priority to AT86900682T priority patent/ATE81905T1/en
Priority to IN522/CAL/85A priority patent/IN164215B/en
Publication of WO1987000263A1 publication Critical patent/WO1987000263A1/en

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B12/00Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material
    • F42B12/02Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect
    • F42B12/36Projectiles, 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
    • F42B12/38Projectiles, 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 tracer type

Definitions

  • This invention relates generally to the field of small aims and cannon caliber eommunition, and more particularly, is directed to improved tracer ammunition including an improved method of manufacture of the tracer ammunition.
  • Tracer ammunition that is, ammunition including pyrotechnic compositions, has long been employed by the military and other organizations to provide a visible "trace" of a projectile's trajectory after the projectile has been fired from a weapon.
  • Such tracer ammunition provides visual assurance that all rounds or slugs are being delivered to the exact area wherein it is desired to direct the fire. Accordingly, for small arms, it is important that the tracer rounds be similar in size, weight and configuration to the other non-tracer rounds so that all ammunition will exhibit similar trajectories and flight patterns.
  • cannon caliber rounds all types of a mm unitnon (e.g., armor-piercing, high-explosive, target-practice, etc.) will contain a tracer.
  • Such prior art pyrotechnic compositions have conventionally been loaded into a hole drilled in the base of the projectile to a predetermined depth wherein the depth of the hole is related to the total visible burning time required.
  • the visible burning time for a pyrotechnic tracer projectile is usually defined as the "trace" of the projectile.
  • This hole in the base of the projectile is filled during the manufacturing process with a pyrotechnic powdered composition, which composition must be consolidated under extremely high compression forces, usually by employing a hydraulic or pneumatic press.
  • This consolidation process may require several consolidation steps and may require the addition of a separate igniter composition in order to assure ignition after firing.
  • the extremely high tamping pressures previously required in the tracer ammunition manufacturing process proved to be extremely cumbersome and difficult when encountering small cavity projectiles to thereby greatly increase production costs while at the same time decreasing reliability and predictability.
  • the consolidation process presently necessary to produce the currently available tracer ammunition has rendered the manufacture of such ammunition unadaptable to fast production by employment of the usual automatic ammunition manufacturing equipment. This results in the requirement to utilize special, slow functioning machines, thus considerably slowing down the production of tracer ammunition and causing increased production costs.
  • the consolidation process also contributes to the relatively unreliable performance of currently available military tracer ammunition.
  • Military specifications usually set forth the common "trace" requirement that ninety to ninety-five percent of the tracer projectiles actually trace at a reliability level of ninety percent. Ammunition manufacturers have experienced difficulties in meeting such standards.
  • the presently available tracer ammunition usually exhibits poor visibility at long ranges from the gunner's location.
  • the relatively large pyrotechnic display of the presently available tracer ammunition provides a close range of visibility which may serve as a locater and thus permit enemy detection of the firing source. Accordingly, many gunners have been faced with the choice of discarding tracer ammunition entirely and thus losing the accuracy and locating affect of the tracer rounds or else, by employing the tracer a mm unition for accuracy purposes, they might then find themselves unduely attracting return fire because of the locater effect of the tracers.
  • the present invention relates generally to the field of tracer ammunition, and more particularly, is directed to tracer ammunition featuring a longitudinally extending pyrotechnic core having an extremely small cross sectional diameter.
  • a continuous pyrotechnic composition filled cord is formed by employing a continuous reel lead, or lead-antimony alloy wire or any other soft metal such as aluminum, copper, etc. and then drilling or otherwise providing a continuous, concentric hole therethrough.
  • the concentric, central opening is then filled with a suitable pyrotechnic formulation and the two ends of the cord are closed with lead or antimony-lead steppers.
  • the continuous cord with the filled pyrotechnic composition is then swaged down in size to the desised final diameter, which diameter usually is the inside diameter of the projectile jacket.
  • this size will be the same size as the lead oord material usually employed in the conventional manufacture of ball-type ammunition and accordingly, the same manufacturing techniques and equipment usually employed with ball-type ammunition can be utilized when manufacturing the tracer ammunition of the present invention.
  • the continuous cord is swaged or drawn down to the desired outside diameter and the cord is cropped or cut into slug size segments.
  • Each slug sized segment contains an outer lead or lead-antimony slug with a concentric, small diameter, pyrotechnic column there-within.
  • the pyrotechnic column extends throughout the length of the slug.
  • the slug is then shaped in known manner to provide a generally pointed front end and generally cylindrical rear end of suitable size to allow loading into a brass jacket using conventional ammunition manufacturing equipment.
  • Fig. 1 is a cross sectional view, partly in elevation, showing a conventional, prior art type of tracer round.
  • Fig. 2 is an enlarged, partial, side elevational view of continuous cord containing a continuous, small diameter pyrotechnic column, and partially broken away to expose interior construction details.
  • Fig. 3 is a side elevational view of a segment of the cord of Fig. 2, cut to the desired length,, and partially broken away to expose interior construction details.
  • Fig. 4 is an enlarged, cross sectional view taken along line 4-4 on Fig. 3, looking in the direction of the arrows.
  • Fig. 5 is a side elevational view of the segment of Fig. 3, partially broken away, shewing a preformed, tracer charged lead slug.
  • Fig. 6 is a cross sectional view shewing the preformed slug of Fig. 5 inserted within a bullet jacket, and partly in elevation to illustrate the jacket crimp.
  • Fig. 7 is a cross sectional view taken along line 7-7 on Fig. 6, looking in the direction of the arrows. DESCRIPTION OF THE PREFERRED EMBODIMENT OF THE INVENTION
  • a prior art type of tracer bullet 10 which includes generally a brass or other metal jacket 12 which is shaped to the desired configuration for the desired path of flight.
  • a point filler 14 completely fills the forward portion of the jacket 12 and preferably, the filler material can be formed of lead in the known manner.
  • the forward aid 16 of the jacket 12 is generally pointed in configuration and the rearward end 18 of the jacket is blunt and is provided with a rear opening 20.
  • the rearward portion of the lead filler 14 is usually drilled or otherwise treated to define a concentric opening 24.
  • a pyrotechnic compsition or tracer 22 is inserted into the lead.
  • a pyrotechnic composition can be loaded through the jacket rear opening 20 to abut directly the rear end of a shortened lead slug 14 in face to face contact.
  • the rearward end of the tracer composition 22 can be drilled or otherwise worked to provide an opening for receipt therein of an igniter composition 26.
  • a sub-igniter composition 28 can also be provided to assure ignition of the pyrotechnic composition 22.
  • a closure disc 30 is provided rearwardly of the pyrotechnic composition 22, the igniter 25 and sub-igniter 28 in a manner to close the rear jacket opening 20 and to facilitate the manufacturing process.
  • a peripheral crimp 32 is impressed in the jacket 12 to secure the jacket to the lead slug 14.
  • the peripheral crimp may be provided with a knurled cannelure 34 to aid in the mechanical bonding of the parts.
  • a continuous pyrotechnic composition filled cord 36 is formed by employing a continuous reel lead, or lead-antimony alloy wire or any other soft metal such as aluminum, copper, etc. and then drilling or otherwise providing a continuous, concentric hole 38 therethrough.
  • a tube of lead, lead-antimony alloy or aluminum, entc. with relatively thick side walls and with a relatively small diameter longitudinal opening can be employed.
  • the concentric, central opening 38 is then filled with a suitable pyrotechnic formulation and the two ends of the cord can be closed with lead or antimory-lead stoppers.
  • the continuous cord 36 with the filled pyrotechnic composition is then swaged down in size to the desired final diameter, which diameter usually is the inside diameter of the projectile jacket.
  • this size will be the same size as the lead cord material usually employed in the conventional manufacture of ball-type ammunition and accordingly, the same manufacturing techniques usually employed with ball-type ammunition can be utilized when manufacturing tracers. It is notaworthy that there is no need to individually drill a rear opening in each round, nor to insert a suitable pyrotechnic composition into that hole under considerable pressure in the manner previously required when producing tracer ammunition. Thus, the manufacture of tracers will take no longer than the manufacture of non-tracer ammunition when using the method of the present invention.
  • each segment 42 contains an outer lead or lead-antimony slug 44 with a concentric, pyrotechnic column 46 therewithin.
  • the pyrotechnic column 46 extends throughout the length of the slug 44.
  • the slug 44 can be shaped in known manner to provide a generally pointed front end 48 and generally cylindrical rear end 50 of size to allow loading into a brass jacket 12 using conventional ammunition manufacturing equipment. See Fig. 6.
  • the pyrotechnic column 46 illustrated in Fig. 5 after swagging or drawing down the cord 36 to the required size, preferable measures between .030 inches to .055 inches in diameter and the core loading density of pyrotechnic material is between approximately twelve grains per linear foot and twenty-four grains per linear foot.
  • a core size of approximately .044 inches in diameter has provided improved results with better ignition reliability over smaller core diameters due to the larger core area that is exposed, while sacrificing only a minor amount of trace distance.
  • the relatively small diameter of the pryrotechnic column surprisingly produces an improved tracer capable of yielding a highly intense, yet distinct line of light along the trajectory which is visible over a range 140% that of conventional tracers.
  • the tracer of the present invention is visible to the gunner within a ⁇ 20° angle from the trajectory, but due to its small diameter, is not visible to the enemy.
  • trace quality is defined to mean the evenness and continuity of the trace output, where a bright, thin, straight line is preferable.
  • the larger core sizes (.060 inches and larger). display a larger, unacceptable amount of what is usually termed "frazzle", that is, a widely dispersed sparkling effect in the trail of the tracer.
  • the pyrotechnic composition 40 mast be of a type that will burn brightly at a controlled rate, that will burn for a sufficient length of time to penrtit visual observation over the entire range and that will not be subject to burn-outs or misfiring.
  • the compositions employed in each test are set forth below. In each test, various composition by weight of zirconium powder, potassium perchlorate and a polyester binder have been employed. In each instance, the zirconium powder employed was finely divided through a forty micron sieve, granular type one, meeting the requirements of Mil-399, class 3.
  • the potassium perchlorate utilized was "primer grade", sieved through a sixty mesh sieve size, meeting the requirements of Mil-P-217, grade A, class 3.
  • the polyester binder was type B, high strength.
  • An alternate binder comprising vinyl alcohol acetate resin (VAAR) as manufactured by union Carbide Company, company specification US-MA-28-18, 28% solids was also tested in the first three composition .
  • the following composition expressed in percentage by weight were tested: INGREDIENT TEST NEMBER
  • compositions of Tests 1 , 2 and 3 using the VAAR binder and the compositions of Tests 7 and 8 using the polyester binder have proved to be most satisfactory for the purpose and test composition have been designated by the applicants as LSI-PT-44, LSI-PT-45, LSI-FT-46, LSI-PT-47 and LSI-PT-48.
  • the slug can be loaded into the open rear 54 of the brass jacket 52 by employing the usual equipment utilized to load lead rounds (not shown) in substantially the same manner and in substantially the same amount of time.
  • the medial crimp 32 can be applied about the periphery of the jacket to secure the parts together.
  • a knurled cannelure 34 can also be formed.
  • the rear end 58 of the jacket 52 can be pressed, molded or otherwise formed to provide conventional boattail 56.
  • a finished tracer round 60 can be provided having a pyrotechnic column 46 of relatively thin diameter extending the entire length of the tracer round 60.
  • the pyrotechnic column 46 extends the entire length of the jacket 52 and that the diameter of the pyrotechnic column 46 is relatively small in comparison to the diameter of the lead or lead-antirrony slug. Additionally, in view of the fact that the pyrotechnic column 46 extends the entire length of the slug, there is no tendency or possibility of the pyrotechnic material separating from the lead or lead-antimony slug.
  • the lead slug 44' completely surrounds the pyrotechnic column 46 for its entire length and fills the entire interior cavity of the jacket.
  • the lead slug 44' then acts as a heat sink in a manner to control and slew the rate of burning of the pyrotechnic column 46.
  • heat is generated upon ignition of the pyrotechnic column, a significant portion of the heat will be absorbed into the surrounding heat sink material, thereby slowing the rate of combustion of the pyrotechnic material to assure tracer burn over the entire, range.
  • the ratio of the length of the pyrotechnic column to the diameter of the column is greater than five. This results in an elongated pyrotechnic column of very small diameter. For exarrple, for 22 cal. ammunition, a pyrotechnic column having a diameter of approximately .030 inches has been satisfactorially tested.
  • the applicants' composition ISI-PT-44, LSI-PT-45, LSI-PT-46, LSI-PT-47 and LSI-PT-48 have been selected for their reliability in ignition and their burning rate. Because of the relatively large mass to pyrotechnic ratio, upon igniticn, the unique thermal characteristics of the tracer ammunition comes into effect, even for small caliber rounds, and the heat of the reaction is driven off into the surrounding lead, lead-antimony, aluminum or other soft metal sidewalls. The sidewalls function as a heat sink to thereby slow down the speed of reaction to assure trace over the entire flight path.

Abstract

An improved tracer ammunition round and method of manufacturing the tracer ammunition. Each round is fabricated by first providing an elongated hole (38) in a cord (36) of soft metal, filling the hole with a special pyrotechnic composition (40) and then reducing the diameter of the cord to a desired size. The cord is then cropped into round size lengths (42) and each length is treated to provide a shaped slug (44') with a pyrotechnic column throughout its length. The shaped slugs are then inserted into the interior cavities of shaped metallic jackets (52) and are secured therein by crimping (32). The pyrotechnic column (46) is formed of zirconium powder, potassium perchlorate and a suitable binder. The ratio of the length of the column to its diameter is between five and two hundred, the diameter of the pyrotechnic column is between .030 inches and .055 inches and the quantity of pyrotechnic composition in the pyrotechnic column is between 12 grains and 24 grains per linear foot of column.

Description

TRACER AMMUNITION
BACKGROUND OF THE INVENTION
1. Field of the Invention
This invention relates generally to the field of small aims and cannon caliber eommunition, and more particularly, is directed to improved tracer ammunition including an improved method of manufacture of the tracer ammunition.
2. Discussion of the Prior Art
Tracer ammunition, that is, ammunition including pyrotechnic compositions, has long been employed by the military and other organizations to provide a visible "trace" of a projectile's trajectory after the projectile has been fired from a weapon. Such tracer ammunition provides visual assurance that all rounds or slugs are being delivered to the exact area wherein it is desired to direct the fire. Accordingly, for small arms, it is important that the tracer rounds be similar in size, weight and configuration to the other non-tracer rounds so that all ammunition will exhibit similar trajectories and flight patterns. For cannon caliber rounds, all types of a mm unitnon (e.g., armor-piercing, high-explosive, target-practice, etc.) will contain a tracer.
Such prior art pyrotechnic compositions have conventionally been loaded into a hole drilled in the base of the projectile to a predetermined depth wherein the depth of the hole is related to the total visible burning time required. The visible burning time for a pyrotechnic tracer projectile is usually defined as the "trace" of the projectile. This hole in the base of the projectile is filled during the manufacturing process with a pyrotechnic powdered composition, which composition must be consolidated under extremely high compression forces, usually by employing a hydraulic or pneumatic press. This consolidation process may require several consolidation steps and may require the addition of a separate igniter composition in order to assure ignition after firing. The extremely high tamping pressures previously required in the tracer ammunition manufacturing process proved to be extremely cumbersome and difficult when encountering small cavity projectiles to thereby greatly increase production costs while at the same time decreasing reliability and predictability.
The consolidation process presently necessary to produce the currently available tracer ammunition has rendered the manufacture of such ammunition unadaptable to fast production by employment of the usual automatic ammunition manufacturing equipment. This results in the requirement to utilize special, slow functioning machines, thus considerably slowing down the production of tracer ammunition and causing increased production costs. The consolidation process also contributes to the relatively unreliable performance of currently available military tracer ammunition. Military specifications usually set forth the common "trace" requirement that ninety to ninety-five percent of the tracer projectiles actually trace at a reliability level of ninety percent. Ammunition manufacturers have experienced difficulties in meeting such standards. The presently employed consolidation process and the use of standard metal-oxidizer chanical formulation has led to various ammunition malfunctions such as "blinds" (wherein there is no tracing at all), short traces, dim traces or even the ejection of all or part of the pyrotechnic composition during flight (usually called "popout"). Further difficulties have been experienced by prior workers in the art because the proper functioning of many tracer compositions exhibited an undesirable dependence en the ambient temperatures.
Additionally, inasmuch as present small-arms tracer projectiles often do not or can not have the same exterior ballistics as the companion (non-tracer) projectiles such as ball projectiles or HE projectiles, which they must simulate in flight trajectory, it will be appreciated that other design and manufacturing problems exist which have not been fully mastered by those skilled in the art of tracer ammunition production.
It has been found by prior workers in the field that the reliability of ignition and the burning time of a tracer is a sensitive function of several manufacturing and environmental variables. The tracer assembly takes up critical space in the round as a whole and is not readily compatible with other ammunition types. Further, the tracer functioning can perturb the exterior ballistics, and because of this, tracer sub-caliber rounds for large caliber systems or the same caliber tracer rounds for small caliber systems can experience ballistic mismatches as compared with the main or non-tracer round when in flight.
Additionally, the presently available tracer ammunition usually exhibits poor visibility at long ranges from the gunner's location. The relatively large pyrotechnic display of the presently available tracer ammunition provides a close range of visibility which may serve as a locater and thus permit enemy detection of the firing source. Accordingly, many gunners have been faced with the choice of discarding tracer ammunition entirely and thus losing the accuracy and locating affect of the tracer rounds or else, by employing the tracer a mm unition for accuracy purposes, they might then find themselves unduely attracting return fire because of the locater effect of the tracers. Further, it has been found that in many instances, certain chlorinated ingredients of current tracer ccnpositions have histories of manifesting carcinogenic effects during manufacturing, thereby possibly creating a considerable job hazard. Additionally, as above set forth, automated tracer manufacturing procedures have not heretofore been available and accordingly, the cost of tracer ammunitiαn manufacturing is considerably greater than that of the main, non-tracer rounds.
SEMMARY OF THE __NVENTION
The present invention relates generally to the field of tracer ammunition, and more particularly, is directed to tracer ammunition featuring a longitudinally extending pyrotechnic core having an extremely small cross sectional diameter.
A continuous pyrotechnic composition filled cord is formed by employing a continuous reel lead, or lead-antimony alloy wire or any other soft metal such as aluminum, copper, etc. and then drilling or otherwise providing a continuous, concentric hole therethrough. The concentric, central opening is then filled with a suitable pyrotechnic formulation and the two ends of the cord are closed with lead or antimony-lead steppers. The continuous cord with the filled pyrotechnic composition is then swaged down in size to the desised final diameter, which diameter usually is the inside diameter of the projectile jacket. Preferably, this size will be the same size as the lead oord material usually employed in the conventional manufacture of ball-type ammunition and accordingly, the same manufacturing techniques and equipment usually employed with ball-type ammunition can be utilized when manufacturing the tracer ammunition of the present invention.
In the manufacturing process, the continuous cord is swaged or drawn down to the desired outside diameter and the cord is cropped or cut into slug size segments. Each slug sized segment contains an outer lead or lead-antimony slug with a concentric, small diameter, pyrotechnic column there-within. The pyrotechnic column extends throughout the length of the slug. After cropping, the slug is then shaped in known manner to provide a generally pointed front end and generally cylindrical rear end of suitable size to allow loading into a brass jacket using conventional ammunition manufacturing equipment.
It is therefore an object of the present invention to provide an improved tracer ammunition of the type set forth.
It is another object of the present invention to provide a novel tracer ammunition featuring pyrotechnic columns including means to produce long burning times with highly intense displays visible over long ranges.
It is another object of the present inventicm to provide a novel small arms tracer ammunition which can be manufactured utilizing the same equipment and the same manufacturing techniques which are employed when manufacturing the non-tracing rounds.
It is another object of the present invention to provide a novel tracer ammunition featuring a pyrotechnic column characterized by a length-to-diameter ratio which exceeds the value of five.
It is another object of the present invention to provide a novel tracer ammunition including a pyrotechnic column of small diameter and means to slow the burnirig rate of the pyrotechnic column.
It is another object of the present invention to provide a novel method of manufacturing an improved tracer ammunition wherein the need for a drilled hole to receive a pyrotechnic cotmposition in the base of the projectile can be eliminated.
It is a further cbject of the present invention to provide a metal encased tracer element for use in cannon caliber ammunition. It is another object of the present invention to provide a novel tracer ammunition and an improved method of manufacturing the same.
Other objects and a fuller understanding of the invention will be had by referring to the following description and claims of a preferred embodiment thereof, taken in conjunction with the accompanying drawings, wherein like reference characters refer to similar parts throughout the severed views and in which:
BRIEF DESCRIPTION OF THE DRAWINGS
Fig. 1 is a cross sectional view, partly in elevation, showing a conventional, prior art type of tracer round.
Fig. 2 is an enlarged, partial, side elevational view of continuous cord containing a continuous, small diameter pyrotechnic column, and partially broken away to expose interior construction details.
Fig. 3 is a side elevational view of a segment of the cord of Fig. 2, cut to the desired length,, and partially broken away to expose interior construction details.
Fig. 4 is an enlarged, cross sectional view taken along line 4-4 on Fig. 3, looking in the direction of the arrows.
Fig. 5 is a side elevational view of the segment of Fig. 3, partially broken away, shewing a preformed, tracer charged lead slug.
Fig. 6 is a cross sectional view shewing the preformed slug of Fig. 5 inserted within a bullet jacket, and partly in elevation to illustrate the jacket crimp.
Fig. 7 is a cross sectional view taken along line 7-7 on Fig. 6, looking in the direction of the arrows. DESCRIPTION OF THE PREFERRED EMBODIMENT OF THE INVENTION
Although specific terms are used in the following description for the sake of clarity, these terms are intended to refer only to the particular structure of the invention selected for illustration in the drawings, and are not intended to define or limit the scope of the invention.
Referring now to the drawings, there is illustrated in Fig. 1 a prior art type of tracer bullet 10 which includes generally a brass or other metal jacket 12 which is shaped to the desired configuration for the desired path of flight. A point filler 14 completely fills the forward portion of the jacket 12 and preferably, the filler material can be formed of lead in the known manner.
The forward aid 16 of the jacket 12 is generally pointed in configuration and the rearward end 18 of the jacket is blunt and is provided with a rear opening 20. The rearward portion of the lead filler 14 is usually drilled or otherwise treated to define a concentric opening 24. Through the rear opening 20 is inserted under pressure a pyrotechnic compsition or tracer 22 to fill the slug opening 24. In the illustrated embodiment, the pyrotechnic composition is inserted into the lead. In other configurations, a pyrotechnic composition can be loaded through the jacket rear opening 20 to abut directly the rear end of a shortened lead slug 14 in face to face contact. When required, the rearward end of the tracer composition 22 can be drilled or otherwise worked to provide an opening for receipt therein of an igniter composition 26. In seme types of tracers, if necessary, a sub-igniter composition 28 can also be provided to assure ignition of the pyrotechnic composition 22. A closure disc 30 is provided rearwardly of the pyrotechnic composition 22, the igniter 25 and sub-igniter 28 in a manner to close the rear jacket opening 20 and to facilitate the manufacturing process. Preferably, a peripheral crimp 32 is impressed in the jacket 12 to secure the jacket to the lead slug 14. In known manner, the peripheral crimp may be provided with a knurled cannelure 34 to aid in the mechanical bonding of the parts.
Referring now to Figs. 2-5, a series of operations for forming a preformed tracer charged lead slug in accordance with the present invention can bow be described. A continuous pyrotechnic composition filled cord 36 is formed by employing a continuous reel lead, or lead-antimony alloy wire or any other soft metal such as aluminum, copper, etc. and then drilling or otherwise providing a continuous, concentric hole 38 therethrough. Optionally, a tube of lead, lead-antimony alloy or aluminum, entc. with relatively thick side walls and with a relatively small diameter longitudinal opening can be employed. The concentric, central opening 38 is then filled with a suitable pyrotechnic formulation and the two ends of the cord can be closed with lead or antimory-lead stoppers. The continuous cord 36 with the filled pyrotechnic composition is then swaged down in size to the desired final diameter, which diameter usually is the inside diameter of the projectile jacket. Preferably, this size will be the same size as the lead cord material usually employed in the conventional manufacture of ball-type ammunition and accordingly, the same manufacturing techniques usually employed with ball-type ammunition can be utilized when manufacturing tracers. It is notaworthy that there is no need to individually drill a rear opening in each round, nor to insert a suitable pyrotechnic composition into that hole under considerable pressure in the manner previously required when producing tracer ammunition. Thus, the manufacture of tracers will take no longer than the manufacture of non-tracer ammunition when using the method of the present invention.
In the manufacturing process, after the continuous cord 36 is swaged or drawn down to the desired outside diameter, the cord is cropped or cut into slug size segments 42 as illustrated in Fig. 3. As shown in Figs. 3 and 4, each segment 42 contains an outer lead or lead-antimony slug 44 with a concentric, pyrotechnic column 46 therewithin. In ball type ammunition as illustrated, the pyrotechnic column 46 extends throughout the length of the slug 44. As best seen in Fig. 5, after cropping, the slug 44 can be shaped in known manner to provide a generally pointed front end 48 and generally cylindrical rear end 50 of size to allow loading into a brass jacket 12 using conventional ammunition manufacturing equipment. See Fig. 6.
In the preferred embodiment, the pyrotechnic column 46 illustrated in Fig. 5, after swagging or drawing down the cord 36 to the required size, preferable measures between .030 inches to .055 inches in diameter and the core loading density of pyrotechnic material is between approximately twelve grains per linear foot and twenty-four grains per linear foot. A core size of approximately .044 inches in diameter has provided improved results with better ignition reliability over smaller core diameters due to the larger core area that is exposed, while sacrificing only a minor amount of trace distance. The relatively small diameter of the pryrotechnic column surprisingly produces an improved tracer capable of yielding a highly intense, yet distinct line of light along the trajectory which is visible over a range 140% that of conventional tracers. The tracer of the present invention is visible to the gunner within a ± 20° angle from the trajectory, but due to its small diameter, is not visible to the enemy.
It has been found that with larger pyrotechnic core diameters, that is, core sizes of .060 inches in diameter and larger, the trace distance falls off dramatically with a corresonding loss in trace quality. The term "trace quality" as used herein is defined to mean the evenness and continuity of the trace output, where a bright, thin, straight line is preferable. The larger core sizes (.060 inches and larger). display a larger, unacceptable amount of what is usually termed "frazzle", that is, a widely dispersed sparkling effect in the trail of the tracer.
In view of the extremely small diameter of the pyrotechnic column 46, the pyrotechnic composition 40 mast be of a type that will burn brightly at a controlled rate, that will burn for a sufficient length of time to penrtit visual observation over the entire range and that will not be subject to burn-outs or misfiring. In order to produce a satisfactory pyrotechnic composition capable of meeting this criteria, numerous tests have been conducted and the compositions employed in each test are set forth below. In each test, various composition by weight of zirconium powder, potassium perchlorate and a polyester binder have been employed. In each instance, the zirconium powder employed was finely divided through a forty micron sieve, granular type one, meeting the requirements of Mil-399, class 3. The potassium perchlorate utilized was "primer grade", sieved through a sixty mesh sieve size, meeting the requirements of Mil-P-217, grade A, class 3. The polyester binder was type B, high strength. An alternate binder comprising vinyl alcohol acetate resin (VAAR) as manufactured by union Carbide Company, company specification US-MA-28-18, 28% solids was also tested in the first three composition . The following composition expressed in percentage by weight were tested: INGREDIENT TEST NEMBER
1 2 3 4 5 6 7 8 zirconium powder 69.3 69.0 68.7 58 38 77.5 65 62.5 potassium perchlorate 29.6 29.4 29.3 38 58 17.5 25 22.5
VAAR or polyester binder 1.1* 1.6* 2.0* 4.0 4.0 5.0 10 15
*Compositions tested with VAAR binder
Of the above tested compositions, it has been determined that the composition of Tests 1 , 2 and 3, using the VAAR binder and the compositions of Tests 7 and 8 using the polyester binder have proved to be most satisfactory for the purpose and test composition have been designated by the applicants as LSI-PT-44, LSI-PT-45, LSI-FT-46, LSI-PT-47 and LSI-PT-48.
Referring now to Fig. 6, utilizing the formed and shaped slug 44' of Fig. 5, the slug can be loaded into the open rear 54 of the brass jacket 52 by employing the usual equipment utilized to load lead rounds (not shown) in substantially the same manner and in substantially the same amount of time. After the interior of the brass jacket 52 is loaded with the slug 44', the medial crimp 32 can be applied about the periphery of the jacket to secure the parts together. At the same time, in the manner previously described, a knurled cannelure 34 can also be formed. Additionally, if desired, the rear end 58 of the jacket 52 can be pressed, molded or otherwise formed to provide conventional boattail 56. Thus it is seen that a finished tracer round 60 can be provided having a pyrotechnic column 46 of relatively thin diameter extending the entire length of the tracer round 60.
Also, it will be noted that during the formation of the tracer round 60, there was no requirement for any drilling or filling operations. Accordingly, after the production of the formed slug 44' of Fig. 5, conventional ammunition manufacturing equipment can be utilized in the usual manner to form the tracer ammunition of the present invention. Additionally, it will be noted that the pyrotechnic column 46 extends the entire length of the jacket 52 and that the diameter of the pyrotechnic column 46 is relatively small in comparison to the diameter of the lead or lead-antirrony slug. Additionally, in view of the fact that the pyrotechnic column 46 extends the entire length of the slug, there is no tendency or possibility of the pyrotechnic material separating from the lead or lead-antimony slug. By employing the peripheral crimp 32 to secure the slug within the jacket, assurance can then be made that the pyrotechnic column will also be secured to the jacket.
It will be noted that the lead slug 44' completely surrounds the pyrotechnic column 46 for its entire length and fills the entire interior cavity of the jacket. The lead slug 44' then acts as a heat sink in a manner to control and slew the rate of burning of the pyrotechnic column 46. As heat is generated upon ignition of the pyrotechnic column, a significant portion of the heat will be absorbed into the surrounding heat sink material, thereby slowing the rate of combustion of the pyrotechnic material to assure tracer burn over the entire, range.
As above set forth, in accordance with the teachings of the present invention, the ratio of the length of the pyrotechnic column to the diameter of the column is greater than five. This results in an elongated pyrotechnic column of very small diameter. For exarrple, for 22 cal. ammunition, a pyrotechnic column having a diameter of approximately .030 inches has been satisfactorially tested.
In view of the small diameter of the pyrotechnic column, the applicants' composition ISI-PT-44, LSI-PT-45, LSI-PT-46, LSI-PT-47 and LSI-PT-48, have been selected for their reliability in ignition and their burning rate. Because of the relatively large mass to pyrotechnic ratio, upon igniticn, the unique thermal characteristics of the tracer ammunition comes into effect, even for small caliber rounds, and the heat of the reaction is driven off into the surrounding lead, lead-antimony, aluminum or other soft metal sidewalls. The sidewalls function as a heat sink to thereby slow down the speed of reaction to assure trace over the entire flight path.
Although the present invention has been described with reference to the particular embodiment herein set forth, it is understood that the present disclosure has been made only by way of example and that numerous changes in the details of the construction may be resorted to without departing from the spirit and scope of the invention. Thus, the scope of the invention should not be limited by the foregoing specification, but rather, only by the scope of the claims appended hereto.

Claims

WHAT IS CLAIMED IS:
1. A tracer ammunition round having a propellant charge comprising
a hollow jacket having a generally pointed front end and a generally blunt rear end, the jacket defining a shaped interior cavity;
a shaped slug inserted into the jacket cavity,
the slug comprising a metallic body the body comprising a forward end, a rearward end and a central cpening, the central opening forrrdng a column extending longitudinally through the body from the forward end to the rearward end, the rearward end being exposed to the propellant charge,
the ratio of the length of the central cpening column to diameter of the central cpening column being at least five; and
a pyrotechnic composition within the central cpening and completely filling the central cpening, the pyrotechnic composition comprising a fuel, an oxidizer and a binder, the pyrotechnic composition being capable of being ignited by the propellant charge to provide a visible trace of the trajectory of the round upon firing, the pyrotechnic composition defining an elongated, small diameter, pyrotechnic column.
2. The tracer round of claim 1, wherein the pyrotechnic composition comprises zirconium powder, potassium perchlorate and a binder.
3. The tracer round of claim 2 wherein the zirconium powder comprises between 68.7 percent and 69.3 percent by weight of the pyrotechnic cortposition.
4. The tracer round of claim 2 wherein the potassium perchlorate comprises between 29.3 percent and 29.6 percent and between 25 and 22.5 percent by weight of the pyrotechnic composition.
5. The tracer round of claim 1 wherein the pyrotechnic column has a diameter of at least about .044 inches.
6. The tracer round of claim 5 wherein the ratio of the mass of the slug to the mass of the pyrotechnic column is sufficiently large to cause the slug to act as a heat sink to slow down the speed of reaction of the pyrotechnic composition.
7. The tracer round of claim 2 wherein the zirconium powder comprises between 62.5 percent and 65 percent by weight of the pyrotecihnic composition.
8. The tracer round of claim 2 wherein the potassium perchlorate comprises between 22.5 percent and-25 percent and between 25 and 22.5 percent by weight of the pyrotechnic composition.
9. The tracer round of claim 1 wherein the ratio of length to diameter of the central opening is between five and two hundred.
10. The tracer round of claim 1 wherein the quantity of pyrotechnic composition is between twelve grains and twenty-four grains per linear foot of column.
11. The tracer round of claim 1 wherein the ratio of the diameter of the slug to the diameter of the column is about 6.
12. The tracer round of claim 1 wherein the diameter of the pyrotechnic composition within the column is between about .030 inches and about .055 inches.
13. The tracer round of claim 1 wherein the jacket is cannon caliber in size, between 20mm. and 40mm.
14. The tracer round of claim 1 wherein the jacket is 22 caliber or larger in size.
15. The method of fabricating a tracer ammunition round cαrprising the steps of
providing a small diameter, elongated hole in a cylindrical cord of lead or other soft metal containing material;
filling the elongated hole with a fast burning pyrotechnic compound;
reducing the diameter of the cylindrical cord and the elongated cpening;
cropping the cord into round-size length and shaping the configurations of the cropped lengths into shaped configurations to form shaped slugs;
formdig a hollow metallic jacket to a shaped configuration and defining a shaped interior cavity of complementary configuraticn to the slug-shaped configuration; and
inserting a shaped slug into the shaped interior cavity and securing the slug therewithin.
16. The method of claim 15 wherein the filling comprises inserting between 12 grains and 24 grains of pyrotechnic composition per foot of elongated hole.
17. The method of claim 15 wherein the reducing is by swagging or drawing.
18. The method of claim 15 wherein the providing comprises forming the elongated hole of approximately .044 inches in cross sectional diameter.
19. The method of claim 18 wherein the filling comprises utilizing a core loading density of pyrotechnic material of between approximately twelve grains per linear foot and twenty-four grains per linear foot.
PCT/US1985/001321 1983-06-23 1985-07-10 Tracer ammunition WO1987000263A1 (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
US06/507,063 US4528911A (en) 1983-06-23 1983-06-23 Tracer ammunition
PCT/US1985/001321 WO1987000263A1 (en) 1985-07-10 1985-07-10 Tracer ammunition
DE8686900682T DE3586786D1 (en) 1985-07-10 1985-07-10 LIGHT AMMUNITION.
EP86900682A EP0229763B1 (en) 1985-07-10 1985-07-10 Tracer ammunition
AT86900682T ATE81905T1 (en) 1985-07-10 1985-07-10 FLARE AMMO.
IN522/CAL/85A IN164215B (en) 1985-07-10 1985-07-15

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/US1985/001321 WO1987000263A1 (en) 1985-07-10 1985-07-10 Tracer ammunition

Publications (1)

Publication Number Publication Date
WO1987000263A1 true WO1987000263A1 (en) 1987-01-15

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PCT/US1985/001321 WO1987000263A1 (en) 1983-06-23 1985-07-10 Tracer ammunition

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EP (1) EP0229763B1 (en)
AT (1) ATE81905T1 (en)
DE (1) DE3586786D1 (en)
IN (1) IN164215B (en)
WO (1) WO1987000263A1 (en)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102011116594B4 (en) * 2011-10-21 2022-02-03 Diehl Defence Gmbh & Co. Kg Use of zirconium or a mixture containing zirconium

Citations (10)

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US581946A (en) * 1897-05-04 Projectile
US734966A (en) * 1903-01-17 1903-07-28 Cecil Vilhelm Schou Projectile.
US1094402A (en) * 1913-08-19 1914-04-21 Winchester Repeating Arms Co Bullet for pleasure target-shooting.
US2336143A (en) * 1941-01-04 1943-12-07 Remington Arms Co Inc Method of making projectiles
US2346462A (en) * 1940-10-23 1944-04-11 American Chain & Cable Co Method of making cores for projectiles
US2425418A (en) * 1942-04-18 1947-08-12 Remington Arms Co Inc Ammunition
US2958277A (en) * 1941-05-09 1960-11-01 Trojan Powder Co Self-igniting incendiary devices
US3401636A (en) * 1966-11-30 1968-09-17 Army Usa Clad pyrotechnics
US3988990A (en) * 1975-09-03 1976-11-02 The United States Of America As Represented By The Secretary Of The Army Projectile
US4204895A (en) * 1978-08-17 1980-05-27 The United States Of America As Represented By The Secretary Of The Navy Green flare compositions

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US581946A (en) * 1897-05-04 Projectile
US734966A (en) * 1903-01-17 1903-07-28 Cecil Vilhelm Schou Projectile.
US1094402A (en) * 1913-08-19 1914-04-21 Winchester Repeating Arms Co Bullet for pleasure target-shooting.
US2346462A (en) * 1940-10-23 1944-04-11 American Chain & Cable Co Method of making cores for projectiles
US2336143A (en) * 1941-01-04 1943-12-07 Remington Arms Co Inc Method of making projectiles
US2958277A (en) * 1941-05-09 1960-11-01 Trojan Powder Co Self-igniting incendiary devices
US2425418A (en) * 1942-04-18 1947-08-12 Remington Arms Co Inc Ammunition
US3401636A (en) * 1966-11-30 1968-09-17 Army Usa Clad pyrotechnics
US3988990A (en) * 1975-09-03 1976-11-02 The United States Of America As Represented By The Secretary Of The Army Projectile
US4204895A (en) * 1978-08-17 1980-05-27 The United States Of America As Represented By The Secretary Of The Navy Green flare compositions

Non-Patent Citations (1)

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Title
Report R-2033, Development of Tracer for XM216 Cartridge, Dept. of the Army, published Feb. 1972, PERKINS et al, pp. 1-45. *

Also Published As

Publication number Publication date
ATE81905T1 (en) 1992-11-15
EP0229763B1 (en) 1992-10-28
IN164215B (en) 1989-02-04
EP0229763A4 (en) 1988-03-07
DE3586786D1 (en) 1992-12-03
EP0229763A1 (en) 1987-07-29

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