TRACER AMMUNITION

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 fc~¥ BACKGROUND OF THE INVENTION 1. Field of the Invention This invention relates generally to the field of small aims and - cannon caliber eoriππunition, and more particularly, is directed to improved tracer aπiriunition including an improved method of manufacture of the tracer arπrunition. 2. Discussion of the Prior Art Tracer a_rπιunition, that is, arrπiunition including pyrotec nic cαπpositions, 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 frc a weapon. Such tracer ctαrπunition 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 iπportant that the tracer rounds be similar in size, weight and configuration to the other non-tracer rounds so that all airmunition will exhibit similar trajectories and flight patterns. For cannon caliber rounds, all types of aritrunitiαn (e.g., armor-piercing, high-explosive, target-practice, etc.) will contain a tracer. Such prior art py__otec~nnic compositions have conventionally been loaded into a hole drilled in the base of the projectile to a predetermined depth vΛierein 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 ιr_m__Eacrturing process with a pyrotechnic powdered exposition, 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 cαtposition in order to assure ignition after firing. The extrβrely high tairping pressures previously required in the tracer aniriuniticri iraπufacturing prooess proved to be extremely currberscme and difficult when enσox tering snail 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 arriπuniticn has rendered the manufacture of such artTTiunition unadaptable to fast production by employment of the usual aut natic arππunition manufacturing equipment. This results in the requirement to utilize special, slew -π_nctiσr_ing machines, thus considerably slowing down the production of tracer arrcrunition and causing increased production costs. The consolidation process also contributes to the relatively unreliable performance of currently available military tracer airiT-nitiσn. Military specifications usually set forth the <_αnτr ι "trace" requirement that ninety to ninety-five percent of the tracer projectiles actually trace at a reliability level of ninety percent. Aπiπunition manufacturers have experienced difficulties ih meeting such standards. The presently employed consolidation process and the use of standard metal-oxidizer chanical foππulation has led to various arririunitica malfuncticns 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 ccrrposition during flight (usually called "popout") . Further difficulties have been experienced by prior workers in the art because the proper functioning of many tracer cαπpositions exhibited an undesirable dependence en the ambient te_rperatures. Additionally, inasmuch as present small-arms tracer projectiles often do not or can not have the same exterior ballistics as the ccπpanion (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 iranufacturing problems exist which have not been fully mastered by those skilled in the art of tracer arriπunition 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 manxifacturing and environmental variables. The tracer assembly takes up critical space in the round as a whole and is not readily ccmpatible with other _aτ_runition types. Further, the tracer ifhmctiαiing can perturb the exterior ballistics, and because of this, tracer sub-caliber rcwnds 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 arriπuniticn usually exhibits poor visibility at long ranges from the gunner's location. The relatively large pyrotechnic display of the presently available tracer arrmunition 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 aππiunition entirely and thus losing the accuracy and locating affect of the tracer rounds or else, by employing the tracer airtπunition 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 rranufacturing, thereby possibly creating a considerable jcb hazard. Mditionally, as above set forth, automated tracer manufacturing procedures have not heretofore been available and accordingly, the cost of tracer arrϊrunitiαn iranufact ring is considerably greater than that of the main, non-tracer rounds. SEMMftRY OF THE __NVI_NTTCN The present invention relates generally to the field of tracer airirnjiiition, and more particularly, is directed to tracer aτr_tι_nition featuring a longitudinally extending pyrotechnic core having an extremely small cross sectional diameter. A ∞ntinuσus 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 cintirrciny-lead stppers. The continuous cord with the filled pyrotechnic coπposition 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 oord material usually employed in the conventional manufacture of ball-type arrπ-jnition and accordingly, the same irianufacturing techniques and equipment usually employed with ball-type aιιrι_nition can be utilized when irenufacturing the tracer airrruiiition of the present invention. In the manufacturing process, the cx_ntinuous cord is swaged or drawn down to the desired itside diameter and the cord is cropped or cut into slug size segments. Each slug sized segment contai s 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 arrmunitiσn manufacturing equipment. It is therefore an object of the present invention to provide an iirproved tracer ammunition of the type set forth. It is another object of the present invention to provide a novel tracer _ετπunition 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 arπ unitiσn which can be m_inufactured utilizing the same equipment and the same anufacturing techniques which are employed when manufacturing the non-tracing rounds. It is another object of the present invention to provide a novel tracer arrirunition 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 arrcnunition 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 iirproved tracer airmunitiσn Vherein ' the need for a drilled hole to receive a pyrotechnic cctrposition 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 airirfljnition and an iirproved 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, sinewing 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 pyro-techriic 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 PKfc-bl-HRED --MBCD-JME OF THE -__vV___7riCIN 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 coπpletely fills the forward portion of the jacket 12 and preferably, the filler material can be formed of lead in the known manner. The forward ad 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 cαtposition or tracer 22 to fill the slug opening 24. In the illustrated e_r__od__ment, the pyrotechnic cαiposition is inserted into the lead. In other configurations, a pyrotechnic composition can be loaded thrcugh 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 coπposition 22 can be drilled or otherwise worked to provide an opening for receipt therein of an igniter ccrrposition 26. In seme types of tracers, if necessary, a sub-igniter σcπposition 28 can also be provided to assure ignition of the pyrι_rtechnic cαrposition 22. A closure disc 30 is provided rearwardly of the pyrot__chnic ccπposition 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 crirrp 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 coπpositiσn filled cord 36 is formed by employing a continuous reel lead, or lead-antimony alloy wire or any other soft metal such as copper, etc. and then drilling or otherwise providing a c(_nt_inucus, concentric hole 38 theret_hrough. Optionally, a tube of lead, lead-antimony alloy or aluminum, etc. 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 c χ _ntinuσus 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 eπployed in the conventional manufacture of ball-type arπrπunition and accordingly, the same manufacturing -te riiques usually employed with ball-type airmunitiα can be utilized when rrant_facturi_ng tracers. It is notaOrthy 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 arrmunitiαn. Thus, the manufacture of tracers will take no longer than the manufacture of non-tracer air unition 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-antirrony slug 44 with a concentric, pyrotechnic column 46 therewithin. In ball type aπmunition as illustrated, the pyroteci_r_ic column 46 extends ttiroughout 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 arr unition manufacturing equipment. See Fig. 6. In the preferred e_r__odiment, 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 σorresonding 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 cαrposition 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 cccrpositicn capable of meeting this criteria, numerous tests have been conducted and the compositions employed in each test are set forth belcw. In each test, various composition by weight of zirconium powder, potassium perchlorate and a polyester binder have been employed. In each instance, the zirconium p<_wder 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 Cαrpany, cαrpany specification US-MA-28-18, 28% solids was also tested in the first three cαrpositions. The following ccirpositions expressed in percentage by weight were tested: INGK__DI__OT 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 *Ccπpositiαns tested with VAAR binder Of the above tested compositions, it has been det-enriined that the σcrrpositions 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 rrost satisfactory for the purpose and test ∞πpositions have been designated by the applicants as I_3I-PT-44, LSI-PT-45, LSI-FT-46, LSI-PT-47 and LSI-P -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 crirrp 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 arttπuiiition 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 eπplσying the peripheral crirrp 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' cαrpletely 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 su___xunding heat sink material, thereby slowing the rate of o rbustion 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. cEατπunition, 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' ccirpositions I_3I-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 air uniticn comes into effect, even for small caliber rounds, and the heat of the reaction is driven off into the surrounding lead, lead-anti ony, 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 sribodiments herein set forth, it is understood that the present disclosure has been made only by way of exarrple 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 arr unition 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 forrr ng a column extend ng 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 αxidizer and a binder, the pyrotechnic cαrposition 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 o rprises between 29.3 percent and 29.6 percent and between 25 and 22.5 percent by weight of the pyrotechnic cσrposition. 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 ccmprises between 62.5 percent and 65 percent by weight of the pyrotecihnic ccrrposition. 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 p-yrotechnic ccrrposition. 9. The tracer round of claim 1 wherein the ratio of length to diameter of the central cpening is between five and two hundred. 10. The tracer round of claim 1 wherein the quantity of pyrotechnic corrposition 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 cαrpositicn within the column is between about .030 inches and about .055 inches. 13. The tracer round of claim 1 wherein the jacket is carmen caliber in size, between 20rrm. and 40rrm. 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 <_ontaining material; filling the elongated hole with a fast burning pyrotechnic cαrpσund; 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; foπrng a hollcw metallic jacket to a shaped configuration and defining a shaped interior cavity of cαrplementary configuraticn to the slug-shaped configuration; and inserting a shaped slug into the shaped interior cavity and securing the slug t-ierewithin. 16. The method of claim 15 wherein the filling comprises inserting bet_ween 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 o rprises utilizing a core loading density of pyrotechnic material of between approximately twelve grains per linear foot and twenty-four grains per linear foot.

Inventors: DE PHILLIPO THOMAS E, KOWALICK JAMES F, DE PHILLIPO, THOMAS, E., KOWALICK, JAMES, F.
Applicants: LSI TECHN INC, LSI TECHNOLOGIES, INC.
Application year: 1985
Main classification: F42B11
IPC codes: F42B12