WO2006118606A2 - Wide area dispersal warhead - Google Patents
Wide area dispersal warhead Download PDFInfo
- Publication number
- WO2006118606A2 WO2006118606A2 PCT/US2005/040789 US2005040789W WO2006118606A2 WO 2006118606 A2 WO2006118606 A2 WO 2006118606A2 US 2005040789 W US2005040789 W US 2005040789W WO 2006118606 A2 WO2006118606 A2 WO 2006118606A2
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- warhead
- housing
- munitions
- explosive charge
- munition
- Prior art date
Links
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
- F42B12/56—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 for dispensing discrete solid bodies
-
- 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
- F42B12/20—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type
- F42B12/22—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type with fragmentation-hull construction
- F42B12/32—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of high-explosive type with fragmentation-hull construction the hull or case comprising a plurality of discrete bodies, e.g. steel balls, embedded therein or disposed around the explosive charge
Definitions
- the subject invention relates to a warhead designed to simultaneously address multiple potential or actual threats.
- the subject invention results from the realization that by packaging a large number of small munitions in a housing and designing an internal explosive charge to have a conical shape, the munitions are deployed into a hemispherical dome shaped pattern to more comprehensively address multiple potential or actual threats.
- This subject invention features a warhead comprising a housing defining a cavity, an explosive charge in the housing, and a large plurality of individual munitions in the cavity of the housing about the explosive charge.
- the explosive charge is configured to deploy the munitions upon detonation into a hemispherical dome shaped pattern.
- the warhead housing includes a cylindrical body with first (base) and second (nose) end plates attached to the ends thereof.
- the nose end plate is preferably dome shaped.
- the preferred explosive charge is conical in shape tapering from a larger first end at the base to a smaller second end at the nose. It is also
- a buffer material such as foam about the explosive charge.
- the housing is toroid in shape.
- the munitions can be made from materials including glass, metal, tungsten carbide, a phenolic material, and
- the explosive charge may be an insensitive explosive.
- housing typically has a wall thickness of less than 2 mils.
- the munitions include a munition core and a plurality of
- the munition core may be made of a dense material such as a tungsten carbide composition.
- the particles can be micro particle in size and can be made of a brittle material such as glass.
- the particles are attached to the munition core with an adhesive.
- a warhead in accordance with the subject invention includes a housing defining a cavity, an explosive charge in the housing, and a plurality of individual munitions in the cavity of the housing about the explosive charge.
- the munitions include a munition core and a plurality of particles attached to an external surface of the munition core designed to release from the munition core upon impact of the munition with a target.
- a warhead in accordance with the subject invention includes a housing defining a cavity and a nose and a base of the warhead, a large plurality of individual munitions in the cavity of the housing, and an explosive charge in the housing having a conical shape tapering from a smaller first end proximate the nose of the housing to a larger second end proximate the base of the housing to deploy the munitions upon detonation into a hemispherical dome shaped pattern.
- a warhead in accordance with the subject invention includes a housing having a longitudinal axis, an explosive charge in the housing extending along the longitudinal axis thereof and having a conical shape, and a large plurality of individual munitions in the housing about the explosive charge.
- Fig. 1 is a schematic three-dimensional exploded partially cut-away front view of one embodiment of a warhead in accordance with the subject invention
- Fig. 2 is a side view showing the munition pattern created in a volume of space when the warhead shown in Fig. 1 is deployed;
- Fig. 3 is a three-dimensional partial schematic front view of another embodiment of a warhead housing in accordance with the subject invention.
- Fig. 4 is a schematic three-dimensional exploded front view of another embodiment of a warhead in accordance with the subject invention including the toroid shaped housing shown in Fig. 3;
- Fig. 5 is a schematic cross-sectional view showing the toroid shape warhead of Fig. 4 being carried by a traditional rocket powered vehicle;
- Fig. 6 is a graph showing the number of munitions as a function of the number of objects hit for a computer stimulation of three test cases involving the warhead shown in Fig. 1 assuming a large pattern radius;
- Fig. 7 is a schematic three-dimensional view showing one example of a munition in accordance with the subject invention.
- Fig. 8 is a schematic conceptual view showing the individual particles associated with the munition shown in Fig. 7;
- Fig. 9 is a schematic conceptual view of one embodiment of a munition core
- Figs. 10A- 1OD are highly schematic side views showing the deployment of the
- Warhead 10 Fig. 1 includes housing 12 defining a cavity therein filled with a large plurality of individual munitions 14 about lengthy centrally located explosive charge 16. Explosive charge 16 is configured to deploy the munitions upon detonation into a hemispherical dome-shape pattern as shown in Fig. 2 to address multiple potential or actual targets T.
- cylindrical housing 12 is 3-5 feet long, 3 feet in diameter and has first 18 and second 20 end plates.
- First end plate 18 constitutes the base of warhead 10 and is typically secured to housing body 22 after munitions 14 and explosive charge 16 are disposed therein.
- Second end plate 20 may be integral with
- body 22 is typically dome shaped, and constitutes the nose of the warhead.
- Thin (e.g., 1 mil) aluminum may be used for housing 12 rendering it expendable upon
- Munitions 14 maybe small .15" diameter spherical particles made of brittle
- Explosive charge 16 may be an insensitive explosive such as PBXNl 09.
- the preferred explosive charge is conical in shape having a 1/2" diameter proximate base 30 and a 1/4" diameter proximate nose 32. In this way, there is more explosive material at base end 30 than at nose end 32 creating a differential velocity of the particles along the longitudinal axis L of the warhead. In one example, explosive charge 16 is 3 feet long.
- Detonator 34 is typically a safe and arm initiation device.
- Foam buffer liner 36 may be disposed about explosive charge 16 to mitigate shock when explosive charge 16 is detonated by detonator 34.
- Foam buffer 36 may be conical in shape to conform to conical shaped explosive charge 16.
- Warhead 10 is carried by a carrier vehicle such as a missile or other rocket powered vehicle into a position in space in front of multiple potential targets T, Fig. 2.
- the conical shaped centrally disposed explosive charge when detonated, creates a differential velocity between the munitions as shown in Fig. 2 so that the munitions proximate base 30 are deployed at a higher rate as shown in Fig. 2 than the munitions proximate nose 32.
- Conical shaped explosive charge 16, Fig. 1 thus creates a hemispherical dome shaped pattern 40, Fig. 2 of munitions 20 feet in radius or greater to address targets T when warhead 10 is deployed to a position in space in front of the trajectory path of a volume of targets as shown in Fig. 2.
- the spray pattern shown in Fig. 2 can spread thousands of feet generating multiple hits on targets T.
- brittle material such as glass is used for munitions 14 they shatter upon impact with a target and break up into smaller particles which embed themselves.
- Alternative housing 12', Fig. 3 is toroidal in shape as shown and includes cavity 60 which is filled with munitions 14 as shown in Figs. 4-5.
- Toroid shaped explosive charge 16' in this embodiment is also conical in shape due to the conical shape of cavity 60, Fig. 3. In this way, warhead 10' can be carried by vehicle 62, Fig.
- a foam buffer material (not shown) may be incorporated in this design about explosive charge 16' as well to generate an impedance mismatch so the munitions do not shatter upon detonation of explosive charge 16'.
- Fig. 6 shows that in computer simulation, if approximately 1 million munitions are present in warhead 10, Fig. 1, at least one munition will strike each of 30 targets in a large radius.
- munitions 14 in housing 12, Fig. 1 or 12', Figs. 2-5 are composite in configuration and are configured as shown for munition 14', Fig. 7.
- Small particles 70, Fig. 8 in accordance with the subject invention are glued or otherwise adhered to the external surface of munition core 72, Fig. 9 resulting in novel munition 14', Fig. 7.
- Particles 70 may be micro particle in size 400 microns in diameter, for example, and munition core 72 may be 1.25 inches in diameter.
- munition core 72 may be of various sizes and spherical in shape or any other shape. The same is true for particles 70: they may be spherical in shape but they also could be other shapes or random shapes or even flakes.
- the core 72 carries the many smaller particles to enhance the particle density upon impact.
- particles 70 are typically epoxied on core 72 and fracture off during impact of the core
- Such a munition can be used for soft targets because the core has the
- Munition 14', Fig. 1OA is shown propelled to impact target 76 along path P.
- munition 14' impacts target 76, Fig. 1OB the particles 70 break off munition core 72 as shown in Fig. 1OC and create an exit opening generally larger than the entrance opening as shown in Fig. 1OD.
- the munition of the subject invention can also be used to destroy items or structure internal to target 76 but not necessarily directly in the direct path P, Fig. 1OA
- the munition core can be made of a dense material such as a tungsten carbide composition and the particles are made of a more brittle material such as glass.
- An adhesive such as an epoxy may be used to adhere the particles to the munition core. The final selection of the particles or the munition is determined by
- the requirements are based on target thickness, impact velocity and target vulnerability.
- munition core 72, Figs. 7 and 9 was a tungsten carbide composition .15" in diameter.
- Particles 70 constituted 500-1,000 glass spheres each 400 microns in size attached to core 72 by an epoxy.
- the deployment method the lethality desired, and the type of target
- the warhead of the subject invention is designed to address multiple potential or actual targets.
- the warhead may be used in conjunction with a conventional kill vehicle wherein the warhead of the subject invention is deployed first to address multiple potential threats and the kill vehicle is deployed second to target any actual threats revealed when the individual munitions of the warhead strikes the potential threats.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Aerials With Secondary Devices (AREA)
Abstract
Description
Claims
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CA2588780A CA2588780C (en) | 2004-11-29 | 2005-11-14 | Wide area dispersal warhead |
JP2007543125A JP2008522127A (en) | 2004-11-29 | 2005-11-14 | Wide-area distributed warhead |
EP05857830A EP1817539B1 (en) | 2004-11-29 | 2005-11-14 | Wide area dispersal warhead |
IL183480A IL183480A (en) | 2004-11-29 | 2007-05-28 | Wide area dispersal warhead |
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10/998,457 | 2004-11-29 | ||
US10/998,457 US20090320711A1 (en) | 2004-11-29 | 2004-11-29 | Munition |
US11/030,455 | 2005-01-06 | ||
US11/030,455 US7717042B2 (en) | 2004-11-29 | 2005-01-06 | Wide area dispersal warhead |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2006118606A2 true WO2006118606A2 (en) | 2006-11-09 |
WO2006118606A3 WO2006118606A3 (en) | 2008-10-16 |
Family
ID=37308425
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/US2005/040789 WO2006118606A2 (en) | 2004-11-29 | 2005-11-14 | Wide area dispersal warhead |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP1817539B1 (en) |
CA (1) | CA2588780C (en) |
WO (1) | WO2006118606A2 (en) |
Family Cites Families (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1272984A (en) * | 1917-02-05 | 1918-07-16 | Michael Mutro | Projectile for field-guns. |
US2406135A (en) * | 1943-04-12 | 1946-08-20 | Reinaldo C Chavez | Explosive shell |
DE3736842A1 (en) * | 1987-10-30 | 1989-05-11 | Diehl Gmbh & Co | BLASTING BULLET WITH A BULLET BODY |
US4947754A (en) * | 1987-12-10 | 1990-08-14 | General Dynamics Corporation, Pomona Division | System and method for penetrating orbiting targets |
GB2302395A (en) * | 1995-06-16 | 1997-01-15 | Numerica Limited | Grenade |
US6598534B2 (en) * | 2001-06-04 | 2003-07-29 | Raytheon Company | Warhead with aligned projectiles |
-
2005
- 2005-11-14 EP EP05857830A patent/EP1817539B1/en active Active
- 2005-11-14 CA CA2588780A patent/CA2588780C/en active Active
- 2005-11-14 WO PCT/US2005/040789 patent/WO2006118606A2/en active Application Filing
Non-Patent Citations (1)
Title |
---|
See references of EP1817539A4 * |
Also Published As
Publication number | Publication date |
---|---|
EP1817539B1 (en) | 2012-10-17 |
CA2588780A1 (en) | 2006-11-09 |
WO2006118606A3 (en) | 2008-10-16 |
EP1817539A4 (en) | 2011-05-04 |
CA2588780C (en) | 2010-08-10 |
EP1817539A2 (en) | 2007-08-15 |
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