EP1552240A1 - Method and system utilizing a laser for explosion of an encased high explosive - Google Patents
Method and system utilizing a laser for explosion of an encased high explosiveInfo
- Publication number
- EP1552240A1 EP1552240A1 EP02807785A EP02807785A EP1552240A1 EP 1552240 A1 EP1552240 A1 EP 1552240A1 EP 02807785 A EP02807785 A EP 02807785A EP 02807785 A EP02807785 A EP 02807785A EP 1552240 A1 EP1552240 A1 EP 1552240A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- laser
- range
- laser beam
- high explosive
- microns
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Ceased
Links
- 239000002360 explosive Substances 0.000 title claims abstract description 56
- 238000000034 method Methods 0.000 title claims abstract description 28
- 238000004880 explosion Methods 0.000 title claims description 26
- 239000000463 material Substances 0.000 claims abstract description 94
- 230000001678 irradiating effect Effects 0.000 claims abstract description 3
- 230000002123 temporal effect Effects 0.000 claims description 3
- 238000005474 detonation Methods 0.000 description 18
- 229910000831 Steel Inorganic materials 0.000 description 16
- 239000010959 steel Substances 0.000 description 16
- 238000012360 testing method Methods 0.000 description 16
- 238000002474 experimental method Methods 0.000 description 13
- 230000000977 initiatory effect Effects 0.000 description 12
- 229910052751 metal Inorganic materials 0.000 description 11
- 239000002184 metal Substances 0.000 description 11
- 239000000203 mixture Substances 0.000 description 7
- 230000008569 process Effects 0.000 description 7
- 238000006243 chemical reaction Methods 0.000 description 5
- 238000004200 deflagration Methods 0.000 description 5
- 230000007246 mechanism Effects 0.000 description 5
- 230000035515 penetration Effects 0.000 description 5
- 230000035939 shock Effects 0.000 description 5
- 230000007704 transition Effects 0.000 description 5
- 239000007789 gas Substances 0.000 description 4
- 230000003993 interaction Effects 0.000 description 4
- 230000000149 penetrating effect Effects 0.000 description 4
- 229910052594 sapphire Inorganic materials 0.000 description 4
- 239000010980 sapphire Substances 0.000 description 4
- SPSSULHKWOKEEL-UHFFFAOYSA-N 2,4,6-trinitrotoluene Chemical compound CC1=C([N+]([O-])=O)C=C([N+]([O-])=O)C=C1[N+]([O-])=O SPSSULHKWOKEEL-UHFFFAOYSA-N 0.000 description 3
- 229910052782 aluminium Inorganic materials 0.000 description 3
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 3
- 230000008901 benefit Effects 0.000 description 3
- 239000011230 binding agent Substances 0.000 description 3
- 238000010586 diagram Methods 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- 238000009472 formulation Methods 0.000 description 3
- 238000005286 illumination Methods 0.000 description 3
- 230000035945 sensitivity Effects 0.000 description 3
- 239000000015 trinitrotoluene Substances 0.000 description 3
- MGTZNGICWXYDPR-ZJWHSJSFSA-N 3-[[(2r)-2-[[(2s)-2-(azepane-1-carbonylamino)-4-methylpentanoyl]amino]-3-(1h-indol-3-yl)propanoyl]amino]butanoic acid Chemical compound N([C@@H](CC(C)C)C(=O)N[C@H](CC=1C2=CC=CC=C2NC=1)C(=O)NC(C)CC(O)=O)C(=O)N1CCCCCC1 MGTZNGICWXYDPR-ZJWHSJSFSA-N 0.000 description 2
- 238000010521 absorption reaction Methods 0.000 description 2
- BJQHLKABXJIVAM-UHFFFAOYSA-N bis(2-ethylhexyl) phthalate Chemical compound CCCCC(CC)COC(=O)C1=CC=CC=C1C(=O)OCC(CC)CCCC BJQHLKABXJIVAM-UHFFFAOYSA-N 0.000 description 2
- 239000000470 constituent Substances 0.000 description 2
- 238000000354 decomposition reaction Methods 0.000 description 2
- 230000007123 defense Effects 0.000 description 2
- 230000008021 deposition Effects 0.000 description 2
- DMBHHRLKUKUOEG-UHFFFAOYSA-N diphenylamine Chemical compound C=1C=CC=CC=1NC1=CC=CC=C1 DMBHHRLKUKUOEG-UHFFFAOYSA-N 0.000 description 2
- 238000010304 firing Methods 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 230000008018 melting Effects 0.000 description 2
- 238000002844 melting Methods 0.000 description 2
- 239000008188 pellet Substances 0.000 description 2
- 230000005855 radiation Effects 0.000 description 2
- 229910000975 Carbon steel Inorganic materials 0.000 description 1
- MQIUGAXCHLFZKX-UHFFFAOYSA-N Di-n-octyl phthalate Natural products CCCCCCCCOC(=O)C1=CC=CC=C1C(=O)OCCCCCCCC MQIUGAXCHLFZKX-UHFFFAOYSA-N 0.000 description 1
- 238000002679 ablation Methods 0.000 description 1
- 230000001133 acceleration Effects 0.000 description 1
- 150000001540 azides Chemical class 0.000 description 1
- 239000010962 carbon steel Substances 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 238000013467 fragmentation Methods 0.000 description 1
- 238000006062 fragmentation reaction Methods 0.000 description 1
- 230000008570 general process Effects 0.000 description 1
- 231100000225 lethality Toxicity 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 230000003287 optical effect Effects 0.000 description 1
- 239000013307 optical fiber Substances 0.000 description 1
- 238000009877 rendering Methods 0.000 description 1
- 230000004044 response Effects 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 230000002459 sustained effect Effects 0.000 description 1
- JDFUJAMTCCQARF-UHFFFAOYSA-N tatb Chemical compound NC1=C([N+]([O-])=O)C(N)=C([N+]([O-])=O)C(N)=C1[N+]([O-])=O JDFUJAMTCCQARF-UHFFFAOYSA-N 0.000 description 1
- 230000008016 vaporization Effects 0.000 description 1
- 238000009834 vaporization Methods 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H13/00—Means of attack or defence not otherwise provided for
- F41H13/0043—Directed energy weapons, i.e. devices that direct a beam of high energy content toward a target for incapacitating or destroying the target
- F41H13/005—Directed energy weapons, i.e. devices that direct a beam of high energy content toward a target for incapacitating or destroying the target the high-energy beam being a laser beam
- F41H13/0062—Directed energy weapons, i.e. devices that direct a beam of high energy content toward a target for incapacitating or destroying the target the high-energy beam being a laser beam causing structural damage to the target
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
- F41H11/00—Defence installations; Defence devices
- F41H11/12—Means for clearing land minefields; Systems specially adapted for detection of landmines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B33/00—Manufacture of ammunition; Dismantling of ammunition; Apparatus therefor
- F42B33/06—Dismantling fuzes, cartridges, projectiles, missiles, rockets or bombs
- F42B33/065—Dismantling fuzes, cartridges, projectiles, missiles, rockets or bombs by laser means
Definitions
- TITLE METHOD AND SYSTEM UTILIZING A LASER FOR EXPLOSION OF
- the invention relates to a method to explode an encased high explosive (HE) material, and more particularly to a method for utilizing a laser to explode a metal encased HE material.
- HE high explosive
- Types of explosions There exist several ways in which HE material can "burn" that ultimately determines the magnitude of an explosion relative to the explosive potential of a given material.
- the most explosive event is referred to as a detonation , which indicates presence of a pressure shock wave within the HE which moves in the HE material at a speed faster than the speed of sound.
- the next most explosive event is referred to as a deflagra tion in which the pressure shock wave associated with the burn moves in the HE material at a speed (the exact speed depending on the local pressure) which is at or below the speed of. This event may or may not be visibly. distinguishable from a detonation event, depending on the burn rate of the HE material and the resulting pressure wave generated. .
- a detonation typically leads to a total consumption of the HE material while a deflagration, because it is more readily quenched, may or may not consume all of the HE material.
- both a detonation and a deflagration can be initiated via an initial localized pressure wave
- both events may also be initiated via thermal mechanisms in a very specific manner.
- the most common and probable thermal mechanism that leads to either detonation or a violent deflagration is a so-called slow cookoff. Slow cookoff describes a situation in which the encased HE material is heated in a slow manner causing the initial temperature to be raised in a relatively uniform fashion.
- thermally induced chemical and/or structural (porosity and density) changes of the HE material take place throughout the entire volume which typically lead to a more sensitive HE material as compared to the original material.
- gases released from the HE material increase the internal pressure of the container.
- a temperature and pressure threshold is reached near the center of the HE material that leads to an explosion (initially ' a deflagration that may or may not transition to detonation) .
- fast cookoff is a process by which the temperature of the encased HE material is raised rapidly causing only the outer perimeter of the HE material to be affected.
- the rapid rise in the temperature soon reaches an ignition (burn) temperature for the HE material causing an increase in the internal pressure.
- ignition burn
- the pressures associated with the burn are not significant enough to lead to the propagation of a self-sustained violent reaction prior to eruption of the HE casing.
- the release of pressure typically quenches the intensity of the burn, resulting in an overall less violent explosive event.
- Types of explosives There exist a wide variety of HE materials which can be classified in several ways. Sensitive and insensitive explosives typically refer to the relative ease in which these materials may be initiated resulting in an explosive event.
- the specific term insensitive high explosives (IHEs) refers to a very special class of high explosives (e.g., TATB) that are very difficult to initiate, and are not the type of explosive with which the present invention is concerned.
- IHEs insensitive high explosives
- TATB very special class of high explosives
- secondary HE material is much less sensitive when compared to the detonator explosive, which requires a smaller thermal input or pressure pulse to initiate.
- secondary HE materials are also categorized in terms of their formulation. Secondary HE material formulations can be described in terms of two broad categories: melt cast and pressed. Melt cast explosives are created by melting together the basic constituents of a formulation and pouring the resulting mixture into a warhead or confinement vessel. Melt cast explosives typically consist of TNT as one of the main constituents. The other broad category of secondary HE materials is so-called pressed HE material. Pressed HE materials are typically composed of a crystalline explosive material combined with a binder and compressed so large samples can be produced.
- Prior attempts to initiate laser HE explosions can be categorized in two general forms: thermal and shock initiation.
- thermal and shock initiation A laser initiated explosion of HE material resulting from a thermal mechanism has typically been performed on sensitive HE materials designed to respond to laser radiation. Less catastrophic events arising from thermal events on less sensitive HE material, such as fast cookoff, are the result of rapid overpressure of the confinement vessel. In this situation, almost all cases have lead to a quenched burn once the confinement vessel has ruptured (pressure vents) and the HE material has ceased to burn.
- the other method to achieve laser initiation of a HE material is related to laser detonators.
- Laser detonation of a secondary HE material typically takes advantage of confinement of the HE material and strong absorption of metallic films.
- a common scenario involves a sapphire window with an aluminum film on one side. The aluminum film is in contact with the HE material and the sapphire window acts as a confining element that is transparent to the laser radiation. When the laser passes through the sapphire it is absorbed by the aluminum film, which immediately generates a plasma.
- the laser generated plasma can only propagate into the HE material, initiating a pressure pulse of sufficient magnitude to lead to a detonation wave in the HE material. In this situation, confinement is critical to achieve to pressures required for a detonation.
- a method for initiating a high explosive material enclosed in a casing comprising: generating a high energy laser beam; directing the high energy laser beam toward a location on a surface of the casing; irradiating the surface location with the laser beam for a sufficient length of time to initiate the high explosive.
- the high energy laser produces a high energy pulsed laser beam, and more preferably a pulsed laser beam having a wavelength absorbed by the casing material and a pulse width on the order 1 millisecond.
- a pulsed laser beam having a wavelength absorbed by the casing material and a pulse width on the order 1 millisecond.
- Figures la-Id are graphical depictions illustrating the use of a laser to initiate ignition of a steel encased explosive material in accordance with the method of the invention .
- Figure 2 is a diagram of a laser temporal pulse shape used in experiments for carrying out the method of the invention .
- Figure 3 illustrates use of a laser defense weapon onboard a ship for destroying a projectile containing a metal encased explosive.
- FIG. 4 is a block diagram of a defensive weapon system employing a laser in accordance with the invention.
- DOI Direct Optical Initiation
- LDDI Laser-Diode Ignition
- DOI Direct Optical Initiation
- LDI Laser-Diode Ignition
- CW continuous wave
- CW continuous wave
- FIG. la-Id illustrate the steps in laser penetration of encased materials, leading to ignition and rapid disassembly (explosion) in accordance with the invention.
- a conventional high explosive 1 is confined in a metal casing 2, such as a steel casing, on all sides.
- a laser beam depicted by arrow 4, initially impinges on a surface 3 of the metal casing 2 resulting in surface heating of the casing 2.
- Step two illustrated in Fig lb, shows the laser beam 4 penetrating the casing with an irradiance sufficient for penetration of the metal casing 2 by melting and/or vaporization of the material of the casing 2.
- step three illustrated in Fig. lc, sustained irradiance of the laser beam 4 eventually causes penetration of the casing 2 whereby metal liquid and vapor are expelled toward the interior of the casing 2 and into the encased material 1.
- step four of the process illustrated at Fig.
- the minimum condition is that the energy deposition rate exceed that of the energy loss rate arising from the pressure vent (hole) in 'the casing material.
- the laser interacting with the encased HE material did not lead to e.xplosion, indicating an energetic threshold for an explosion had not yet occurred.
- the majority, if not all, of the HE material was consumed and the violence of the explosion was sufficient to cause rapid disassembly of the steel casing.
- the HE material was in the form of pellets, 1 inch long, 1 inch in diameter and with masses in the range of 20-25 grams. Table I below lists the HE materials used in the ignition test experiments .
- HMX 1, 3 , 5, 7-tetranotro-l, 3, 5 , 7-tetraazacyclooctane
- TNT Trinitrotoluene
- Table II HE samples used in the seven explosive ignition tests
- the tests were intended to judge potential violence of an explosion of a confined HE material.
- An explosive fixture encasing the HE material was made of 1018 mild carbon steel.
- the HE pellet was radially confined in a steel tube 1-inch in length, 1-inch inside diameter, 0.25 inches thick. Both ends of the tube were grooved to accommodate O-rings to seal decomposition gases and to aid the growth of the deflagation. End plates were made of 0.5 inch thick steel, with the front confining plate having a hole and countersink for laser access to the 0.1 inch steel cover plate over the explosive.
- Four grade 8 steel bolts and nuts 1/4-20' s were used to assemble the fixture and were the weakest part of the confinement.
- the nuts were fully tightened in all of the shots accept for shot number 4 where the bolts were tightened only to 18 in-lb to examine the effects of weaker confinement.
- the laser used to ignite the HE material was a Lumonics JK701H ND:YAG laser having a 1.06 micron wavelength output which was routed into a firing area using a 1 millimeter diameter optical fiber. Lenses were used to re-image the spot to the front face of the explosive test device. The laser delivered approximately 4.5 J/pulse at the position of the explosive test fixture and the laser spot size was approximately 1 millimeter in diameter. With optimized positioning of a steel plate, 300 to 400 laser pulses were required to open a hole through a bare 0.1 inch thick steel plate used as the front face of the test fixture. The temporal profile of the laser pulse is shown in Fig. 2.
- Fig. 2 Although various pulse formats were selectable for the laser, the one shown in Fig. 2 was used for all ignition test shots which consisted of two closely spaced peaks spaced approximately 1 millisecond apart. The laser was fired at 35Hz repetition rate for all initiation tests. For all tests, an arbitrary number of laser pulses for the complete duration of the laser exposure was selected between 1,000 and 5,000 pulses. Table III below summarizes the results of the tests.
- FIG. 3 illustrates a shipboard use of such a self- defense laser weapon for destroying a missile-carrying warhead by initiating the warhead through a thermal event as discussed above .
- Fig. 4 is a block diagram showing the major components of a laser weapon system 12. As shown in Fig. 4, a laser weapon control system 20 is coupled to an operator console 22, a radar acquisition system 24, high energy laser 26 and a tracking system 28. The output of laser 26 is coupled to a beam director 30 by way of coupling and control optics 32.
- the beam director produces a beacon beam 34 and a high energy weapon beam 36.
- the individual components of the laser weapon system 12 are well known and need not be described in detail.
- the acquisition system 24 is utilized to acquire the position of an object to be irradiated, such as a projectile.
- Information from the radar acquisition system 24 is fed to the tracking system 28 which is coupled to beam director 30 for controlling the beacon beam 34 and the high energy weapon beam
- the beacon beam 34 is utilized for fine tracking of the projectile and precisely aiming the high energy weapon beam 36 at a location on the surface of the projectile where the warhead is typically located.
- the laser 26 preferably produces a pulsed output having a wavelength in a range of about .1 microns to about 10 microns, and most preferably approximately 1.1 microns. Additionally, it is preferred that the output of the laser 26 have a pulse width in the millisecond range, for example from about .1 microseconds to about 100 milliseconds. Preferably the laser pulses are generated at a rate of about 5 Hz to about 5 MHz.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Manufacturing & Machinery (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Optical Radar Systems And Details Thereof (AREA)
Abstract
Description
Claims
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| PCT/US2002/028103 WO2004023061A1 (en) | 2002-09-05 | 2002-09-05 | Method and system utilizing a laser for explosion of an encased high explosive |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| EP1552240A1 true EP1552240A1 (en) | 2005-07-13 |
Family
ID=31975581
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP02807785A Ceased EP1552240A1 (en) | 2002-09-05 | 2002-09-05 | Method and system utilizing a laser for explosion of an encased high explosive |
Country Status (3)
| Country | Link |
|---|---|
| EP (1) | EP1552240A1 (en) |
| AU (1) | AU2002367806A1 (en) |
| WO (1) | WO2004023061A1 (en) |
Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2534672B1 (en) | 2010-02-09 | 2016-06-01 | Energetiq Technology Inc. | Laser-driven light source |
| RU2489677C1 (en) * | 2012-02-28 | 2013-08-10 | Общество с ограниченной ответственностью "Научно-производственный центр "СИСТЕМА" (ООО "НПЦ "СИСТЕМА") | Method for laser neutralisation of explosive objects |
| US11587781B2 (en) | 2021-05-24 | 2023-02-21 | Hamamatsu Photonics K.K. | Laser-driven light source with electrodeless ignition |
| US12165856B2 (en) | 2022-02-21 | 2024-12-10 | Hamamatsu Photonics K.K. | Inductively coupled plasma light source |
| US12144072B2 (en) | 2022-03-29 | 2024-11-12 | Hamamatsu Photonics K.K. | All-optical laser-driven light source with electrodeless ignition |
| US12156322B2 (en) | 2022-12-08 | 2024-11-26 | Hamamatsu Photonics K.K. | Inductively coupled plasma light source with switched power supply |
| US12578076B2 (en) | 2023-06-05 | 2026-03-17 | Hamamatsu Photonics K.K. | Dual-output laser-driven light source |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1987005994A1 (en) * | 1986-03-27 | 1987-10-08 | Affärsverket Ffv | A reactive armour wall structure |
| EP1227293A2 (en) * | 2001-01-27 | 2002-07-31 | Dynamit Nobel GmbH Explosivstoff- und Systemtechnik | Reactive armour fixed to military vehicles |
| GB2375587A (en) * | 1990-11-19 | 2002-11-20 | Royal Ordnance Plc | Armour panel |
Family Cites Families (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3542787A1 (en) * | 1985-12-04 | 1987-06-11 | Jastram Werke | METHOD FOR THE NEUTRALIZATION OF SURFACE-MOUNTED OR CLOTHED LANDMINES AND MOBILE DEVICE FOR IMPLEMENTING THE METHOD |
| DE3544364A1 (en) * | 1985-12-14 | 1987-06-19 | Krauss Maffei Ag | METHOD AND DEVICE FOR CLEARING EXPLOSIVE BODIES |
| DE3836014A1 (en) * | 1988-10-22 | 1996-05-02 | Diehl Gmbh & Co | Tank reactive armour-plating module release system |
| EP0451304B1 (en) * | 1990-04-07 | 1994-02-16 | Blohm + Voss international GmbH | Method for desintegrating an object by laser |
| US5198607A (en) | 1992-02-18 | 1993-03-30 | Trw Inc. | Laser anti-missle defense system |
| SE501138C2 (en) * | 1993-04-08 | 1994-11-21 | Bofors Ab | Method and apparatus for the destruction of explosive-filled objects or bodies |
| US5955724A (en) * | 1996-10-11 | 1999-09-21 | Trw Inc. | Laser along-body tracker comprising laser beam dithering |
| US6014922A (en) * | 1997-12-11 | 2000-01-18 | Trw Inc. | Short range/intermediate range laser defense against chemical and biological weapons |
| FR2797043B1 (en) * | 1999-07-26 | 2002-09-20 | Anne Marie Coudert | REMOTE DETECTION AND DESTRUCTION OF MINES AND EXPLOSIVE DEVICES - TECHNICAL STUDY - APPARATUS |
| US6460459B1 (en) * | 2000-04-07 | 2002-10-08 | Raytheon Company | Method and system utilizing a laser for explosion of an encased high explosive |
-
2002
- 2002-09-05 WO PCT/US2002/028103 patent/WO2004023061A1/en not_active Ceased
- 2002-09-05 EP EP02807785A patent/EP1552240A1/en not_active Ceased
- 2002-09-05 AU AU2002367806A patent/AU2002367806A1/en not_active Abandoned
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1987005994A1 (en) * | 1986-03-27 | 1987-10-08 | Affärsverket Ffv | A reactive armour wall structure |
| GB2375587A (en) * | 1990-11-19 | 2002-11-20 | Royal Ordnance Plc | Armour panel |
| EP1227293A2 (en) * | 2001-01-27 | 2002-07-31 | Dynamit Nobel GmbH Explosivstoff- und Systemtechnik | Reactive armour fixed to military vehicles |
Non-Patent Citations (1)
| Title |
|---|
| See also references of WO2004023061A1 * |
Also Published As
| Publication number | Publication date |
|---|---|
| AU2002367806A1 (en) | 2004-03-29 |
| WO2004023061A1 (en) | 2004-03-18 |
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| RIN1 | Information on inventor provided before grant (corrected) |
Inventor name: PAUL, ANDREW, E. Inventor name: KNOX, ROBERT, W. Inventor name: MARTIN, SCOTT, G. Inventor name: MCCAHON, STEVEN, W. |
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