WO1987000263A1 - Tracer ammunition - Google Patents
Tracer ammunition Download PDFInfo
- 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
Links
- 239000000700 radioactive tracer Substances 0.000 title claims abstract description 79
- 239000000203 mixture Substances 0.000 claims abstract description 48
- 238000004519 manufacturing process Methods 0.000 claims abstract description 36
- 239000011230 binding agent Substances 0.000 claims abstract description 10
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 claims abstract description 7
- AXZAYXJCENRGIM-UHFFFAOYSA-J dipotassium;tetrabromoplatinum(2-) Chemical compound [K+].[K+].[Br-].[Br-].[Br-].[Br-].[Pt+2] AXZAYXJCENRGIM-UHFFFAOYSA-J 0.000 claims abstract description 7
- 229910052751 metal Inorganic materials 0.000 claims abstract description 7
- 239000002184 metal Substances 0.000 claims abstract description 7
- 229910001487 potassium perchlorate Inorganic materials 0.000 claims abstract description 7
- 241000237858 Gastropoda Species 0.000 claims abstract description 3
- 239000000463 material Substances 0.000 claims description 9
- 238000000034 method Methods 0.000 claims description 9
- 238000006243 chemical reaction Methods 0.000 claims description 3
- 238000010304 firing Methods 0.000 claims description 3
- 239000007800 oxidant agent Substances 0.000 claims description 2
- 239000003380 propellant Substances 0.000 claims 3
- 230000000295 complement effect Effects 0.000 claims 1
- 150000001875 compounds Chemical class 0.000 claims 1
- 239000000446 fuel Substances 0.000 claims 1
- 238000007493 shaping process Methods 0.000 claims 1
- 238000002788 crimping Methods 0.000 abstract 1
- 229910001369 Brass Inorganic materials 0.000 description 5
- 239000010951 brass Substances 0.000 description 5
- 238000007596 consolidation process Methods 0.000 description 5
- 229910052782 aluminium Inorganic materials 0.000 description 4
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 4
- 229910052787 antimony Inorganic materials 0.000 description 4
- 229920000728 polyester Polymers 0.000 description 4
- 229910001245 Sb alloy Inorganic materials 0.000 description 3
- 239000002140 antimony alloy Substances 0.000 description 3
- 238000010276 construction Methods 0.000 description 3
- 238000005553 drilling Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 239000000945 filler Substances 0.000 description 3
- 238000009472 formulation Methods 0.000 description 3
- 230000002093 peripheral effect Effects 0.000 description 3
- NIOPZPCMRQGZCE-WEVVVXLNSA-N 2,4-dinitro-6-(octan-2-yl)phenyl (E)-but-2-enoate Chemical compound CCCCCCC(C)C1=CC([N+]([O-])=O)=CC([N+]([O-])=O)=C1OC(=O)\C=C\C NIOPZPCMRQGZCE-WEVVVXLNSA-N 0.000 description 2
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 2
- 229910052802 copper Inorganic materials 0.000 description 2
- 239000010949 copper Substances 0.000 description 2
- 239000004615 ingredient Substances 0.000 description 2
- 230000000007 visual effect Effects 0.000 description 2
- QTBSBXVTEAMEQO-UHFFFAOYSA-M Acetate Chemical compound CC([O-])=O QTBSBXVTEAMEQO-UHFFFAOYSA-M 0.000 description 1
- IMROMDMJAWUWLK-UHFFFAOYSA-N Ethenol Chemical compound OC=C IMROMDMJAWUWLK-UHFFFAOYSA-N 0.000 description 1
- QQHJESKHUUVSIC-UHFFFAOYSA-N antimony lead Chemical compound [Sb].[Pb] QQHJESKHUUVSIC-UHFFFAOYSA-N 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 230000000711 cancerogenic effect Effects 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 230000007613 environmental effect Effects 0.000 description 1
- 239000002360 explosive Substances 0.000 description 1
- 230000007257 malfunction Effects 0.000 description 1
- 239000011347 resin Substances 0.000 description 1
- 229920005989 resin Polymers 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
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
- F42B12/38—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 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.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Air Bags (AREA)
- Indicating Or Recording The Presence, Absence, Or Direction Of Movement (AREA)
Priority Applications (6)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US06/507,063 US4528911A (en) | 1983-06-23 | 1983-06-23 | Tracer ammunition |
| AT86900682T ATE81905T1 (de) | 1985-07-10 | 1985-07-10 | Leuchtmunition. |
| DE8686900682T DE3586786D1 (de) | 1985-07-10 | 1985-07-10 | Leuchtmunition. |
| PCT/US1985/001321 WO1987000263A1 (en) | 1985-07-10 | 1985-07-10 | Tracer ammunition |
| EP86900682A EP0229763B1 (en) | 1985-07-10 | 1985-07-10 | Tracer ammunition |
| IN522/CAL/85A IN164215B (enrdf_load_stackoverflow) | 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 |
Family
ID=22188764
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/US1985/001321 WO1987000263A1 (en) | 1983-06-23 | 1985-07-10 | Tracer ammunition |
Country Status (5)
| Country | Link |
|---|---|
| EP (1) | EP0229763B1 (enrdf_load_stackoverflow) |
| AT (1) | ATE81905T1 (enrdf_load_stackoverflow) |
| DE (1) | DE3586786D1 (enrdf_load_stackoverflow) |
| IN (1) | IN164215B (enrdf_load_stackoverflow) |
| WO (1) | WO1987000263A1 (enrdf_load_stackoverflow) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US12247810B2 (en) | 2013-03-21 | 2025-03-11 | Nostromo, Llc | Optically tracked projectile |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102011116594B4 (de) * | 2011-10-21 | 2022-02-03 | Diehl Defence Gmbh & Co. Kg | Verwendung von Zirkonium oder eines Zirkonium enthaltenden Gemischs |
Citations (10)
| 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. |
| 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 |
-
1985
- 1985-07-10 AT AT86900682T patent/ATE81905T1/de not_active IP Right Cessation
- 1985-07-10 EP EP86900682A patent/EP0229763B1/en not_active Expired
- 1985-07-10 DE DE8686900682T patent/DE3586786D1/de not_active Expired - Lifetime
- 1985-07-10 WO PCT/US1985/001321 patent/WO1987000263A1/en active IP Right Grant
- 1985-07-15 IN IN522/CAL/85A patent/IN164215B/en unknown
Patent Citations (10)
| 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)
| Title |
|---|
| Report R-2033, Development of Tracer for XM216 Cartridge, Dept. of the Army, published Feb. 1972, PERKINS et al, pp. 1-45. * |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US12247810B2 (en) | 2013-03-21 | 2025-03-11 | Nostromo, Llc | Optically tracked projectile |
Also Published As
| Publication number | Publication date |
|---|---|
| EP0229763B1 (en) | 1992-10-28 |
| ATE81905T1 (de) | 1992-11-15 |
| EP0229763A4 (en) | 1988-03-07 |
| EP0229763A1 (en) | 1987-07-29 |
| IN164215B (enrdf_load_stackoverflow) | 1989-02-04 |
| DE3586786D1 (de) | 1992-12-03 |
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