US20150033971A1 - Warhead having selectable axial effects - Google Patents
Warhead having selectable axial effects Download PDFInfo
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- US20150033971A1 US20150033971A1 US13/604,887 US201213604887A US2015033971A1 US 20150033971 A1 US20150033971 A1 US 20150033971A1 US 201213604887 A US201213604887 A US 201213604887A US 2015033971 A1 US2015033971 A1 US 2015033971A1
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- warhead
- peripheral segments
- segment
- target
- detonation
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- 230000000694 effects Effects 0.000 title claims description 7
- 230000002093 peripheral effect Effects 0.000 claims abstract description 72
- 238000005474 detonation Methods 0.000 claims abstract description 30
- 239000002360 explosive Substances 0.000 claims abstract description 18
- 230000000149 penetrating effect Effects 0.000 claims abstract description 5
- 238000013467 fragmentation Methods 0.000 claims description 8
- 238000006062 fragmentation reaction Methods 0.000 claims description 8
- 238000009987 spinning Methods 0.000 claims description 7
- 238000000034 method Methods 0.000 claims description 6
- 238000000059 patterning Methods 0.000 claims description 4
- 230000000717 retained effect Effects 0.000 claims description 2
- 239000012634 fragment Substances 0.000 description 5
- 238000004880 explosion Methods 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 2
- 229910052802 copper Inorganic materials 0.000 description 2
- 239000010949 copper Substances 0.000 description 2
- 238000010304 firing Methods 0.000 description 2
- 230000001965 increasing effect Effects 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- 230000009466 transformation Effects 0.000 description 2
- 230000000295 complement effect Effects 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 230000001066 destructive effect Effects 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000003292 diminished effect Effects 0.000 description 1
- 230000002708 enhancing effect Effects 0.000 description 1
- 238000003331 infrared imaging Methods 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
Images
Classifications
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- 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
- F42B12/04—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type
- F42B12/10—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type with shaped or hollow charge
-
- 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
- F42B12/04—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type
- F42B12/10—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type with shaped or hollow charge
- F42B12/16—Projectiles, missiles or mines characterised by the warhead, the intended effect, or the material characterised by the warhead or the intended effect of armour-piercing type with shaped or hollow charge in combination with an additional projectile or charge, acting successively on the target
-
- 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
-
- 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
- F42B12/207—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 characterised by the explosive material or the construction of the high explosive warhead, e.g. insensitive ammunition
-
- 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
- F42B12/208—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 characterised by a plurality of charges within a single high explosive warhead
-
- 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
Definitions
- the present invention is related to the field of explosive warheads, and in particular to air-delivered tactical warheads used against ground targets such as vehicles and personnel.
- Warheads of the type known as explosively formed penetrators or EFPs are generally known.
- a liner closes one end of a cylindrical body filled with high explosive.
- the liner is of a relatively dense and low-yield material such as copper.
- the liner forms an elongated, high-velocity slug capable of penetrating steel vehicle bodies and other relatively hard target objects.
- the liner has patterning to promote a desired pattern of fragmentation, such as to form a ring of smaller projectiles or “p-charges” about a central EFP slug.
- the smaller projectiles are effective against lighter vehicles, other ground-based equipment, and personnel.
- the effectiveness of air-delivered tactical warheads can be improved by features providing for altering the warhead configuration depending on the type of target, specifically depending on whether the target is primarily an armored vehicle or similar single hardened target or primarily a collection of lighter vehicles and/or personnel in a small area.
- a configuration maximizing the power of an EFP slug can be used, while for area targets a configuration maximizing forward-directed fragmentation can be used.
- the selection may be made dynamically based on the characteristics of targets as they are pursued or encountered, either by human user input or by automatic action of target acquisition electronics carried by the warhead.
- a disclosed warhead has a generally cylindrical shape and is divided into a conical central segment and a plurality of peripheral segments surrounding the central segment.
- the central segment has a disk-shaped liner at a front end, the liner bounding a cavity of the central segment filled with high explosive and configured to form one or more high-speed projectiles in a forward direction upon detonation of the high explosive.
- the liner is configured to form an EFP slug, and may also include separate smaller p-charges for lighter targets in the area of an armored vehicle or similar hardened target.
- the peripheral segments are hingedly attached to the central segment about the liner at the front end.
- Each peripheral segment has an outer segment face bounding a cavity of the peripheral segment filled with high explosive, and the segment faces of the peripheral segments form sidewall portions of the warhead when the peripheral segments are in a closed or folded position.
- the peripheral segments are operable to be released from the folded position to an open position in which the segment faces are pointed in the forward direction for detonation.
- a detonator initiates simultaneous detonation of the high explosive of the central and peripheral segments.
- the warhead may be used in the closed position, in which case the explosions of the peripheral segments provide confinement for the explosive of the central segment, resulting in maximized energy imparted to the EFP slug formed by the liner (as well as any separate p-charges from the liner if present). In this use the result is similar to that of the conventional EFP warhead.
- the warhead may also be used in the open position, in which case the fragments formed from the outer walls of the peripheral segments are directed forward toward area target(s), adding to the destructive effect of the EFP slug and any p-charges formed by the liner.
- the manner of use is selectable, enabling flexible deployment based on specific target types. For example, the opening of the warhead may be enabled at a time of launch of the warhead, or at a time of target acquisition after launch. Thus a single warhead type can be carried in the field and used in a flexible manner to support different missions and tactical situations.
- FIG. 1 is a perspective view of a warhead with peripheral segments in folded positions as at launch;
- FIG. 2 is a schematic rear view of the warhead
- FIGS. 3-5 are views of the warhead from different angles and with peripheral segments in both folded and open positions;
- FIG. 6 is a view of a warhead according to an alternative embodiment.
- FIG. 7 is a schematic diagram depicting use of the warhead.
- FIG. 1 shows a warhead 10 (also referred to as “submunition” herein) having a cylindrical body 12 closed at one end by a disk-shaped liner 14 .
- the body 12 is generally of steel or a similar hard, high-strength material, while the liner 14 is of a denser and more deformable material such as copper.
- the body 12 is divided into multiple peripheral segments 16 (shown as 16 - 1 , 16 - 2 etc.) about the axis of the warhead 10 . In the illustrated example, four peripheral segments 16 are used, with three segments 16 - 1 , 16 - 2 and 16 - 3 being visible in FIG. 1 .
- Each peripheral segment 16 is secured to a central segment 18 by a respective hinge 20 .
- Both the peripheral segments 16 and central segment 18 are hollow members having internal cavities filled with high explosive.
- One or more detonators (not shown in FIG. 1 ) are used to detonate the explosive when the warhead 10 comes into range of a target. As described more fully below, detonation forms both an explosively formed penetrator (EFP) slug from liner 14 as well as a number of smaller fragments.
- EFP explosively formed penetrator
- the warhead 10 may be used in two basic configurations. In the configuration shown in FIG. 1 , the main effect is that of the EFP formed by liner 14 , which can be used against harder point targets such as armored vehicles.
- the first configuration shown in FIG. 1 , is referred to herein as the “closed” or “folded” configuration or position, while the second configuration is described below and is referred to as the “open” or “unfolded” position.
- FIG. 2 is a schematic view of the bottom of the warhead 10 .
- Triangular-shaped bottom surfaces of the four peripheral segments 16 are shown.
- the central segment 18 has a cone shape, broad at the top and narrow at the bottom, while the peripheral segments 16 have complementary annular-section or wedge shapes having triangular radial cross section.
- Shown schematically is a latch 22 used to maintain the warhead 10 in the closed or folded configuration, the latch being disengaged during operation to enable the peripheral segments 16 to rotate about the hinges 20 to the open position.
- respective detonation points 24 for the segments 16 , 18 There may be distinct detonators (not shown) used for respective segments 16 , 18 , or in an alternative embodiment there may be fewer detonators (e.g., one) coupled to the detonation points 24 by detonation cord for example.
- FIGS. 3 and 4 are side views illustrating the opening of the warhead 10 during operation.
- FIG. 3 shows the warhead 10 in the closed position, as in FIGS. 1 and 2 .
- the dotted lines 30 indicate inward-facing surfaces of the wedge-shaped peripheral segments 16 , which abut the rear conical surface of the central segment 12 .
- the peripheral segments 16 When the peripheral segments 16 are in the closed position, the curved outer surfaces 34 of the peripheral segments 16 together form the cylindrical sidewall of the warhead 10 .
- FIG. 4 shows the warhead 10 in the open position, in which the peripheral segments 16 have rotated approximately 90 degrees so that their respective curved outer surfaces 34 are facing in the same forward direction as the liner 14 . Only two of the peripheral segments 16 are shown; it will be appreciated that the other two peripheral segments 16 open in directions out of the plane of FIG. 4 .
- FIG. 5 shows a front view of the warhead 10 in the open position as in FIG. 4 . All four peripheral segments 16 are shown. Also shown is a particular patterning of the liner 14 , specifically a central depression 36 and a ring of surrounding smaller depressions 38 . This patterning promotes a predetermined fragmentation of the liner 14 upon detonation to achieve a desired effect. Specifically, the center portion of the liner 14 forms a relatively large EFP slug as for other types of EFP warheads. The outer ring of depressions 38 fragments into smaller projectiles which can be effective against personnel and light vehicles. When the warhead 10 is detonated in the open position as in FIG. 5 , this latter effect is increased by forward-directed fragments created from the walls 34 of the peripheral segments 16 .
- the warhead 10 may be detonated in either the folded (closed) or open position.
- the manner of use may be fixed, while in other embodiments it may be user-selectable in some manner.
- the latch 22 may be non-releasable or even replaced by other structure to fixedly retain the peripheral segments 16 in the closed position, such as by screws or similar fasteners or even welding.
- the warhead 10 may be used in the same manner as a conventional EFP warhead.
- the explosion of the peripheral segments 16 acts to confine the explosion of the central segment 18 , increasing the velocity and effectiveness of the slug and any other projectiles formed by the liner 14 .
- This kind of use may also be selected, for example by simply refraining from unlatching or releasing the peripheral segments 16 prior to detonation.
- a variety of control schemes for detonation with or without release of the peripheral segments 16 to the open position may be used.
- a releasable latch 22 in a given application it may not be activated, so that the warhead 10 is detonated with the peripheral segments 16 retained in the folded position of FIG. 3 .
- the detonator and latch 22 may also be configured to initiate detonation of the warhead 10 with the peripheral segments 16 in the open position after release by the latch 22 . In this case the projectiles formed by fragmentation of the outer surfaces 34 of the peripheral segments 16 are directed forward toward the target, enhancing effectiveness against lighter equipment and/or personnel.
- Selection and timing of the position of detonation may be made in a variety of ways.
- electronic control circuitry carried by the warhead controls operation.
- the circuitry may be programmed or otherwise instructed to use particular timing and/or conditions for releasing the latch 22 to attain the open position for detonation.
- the release may be enabled by user input prior to launch of the warhead 10 toward a target, which may be effective when the user knows the characteristics of the target prior to launch.
- the release may be enabled at a time of target acquisition by automatic action of the control circuitry carried by the warhead. This configuration can increase effectiveness when the exact characteristics of the target are not known at launch but can be ascertained by the control circuitry based on sensor input (e.g., visible-light or infrared imaging input).
- the outer surfaces 34 of the peripheral segments 16 may be specifically configured to achieve a desired fragmentation into projectiles of predetermined size and shape upon detonation of the warhead 10 .
- the surfaces 34 may be scored with a pattern of lines.
- a relief pattern of thickness variation may be used, such as dimpling, analogous to the above-described depressions 38 of the liner 14 .
- FIG. 6 shows an alternative embodiment 40 employing six peripheral segments 42 along with a central segment 44 having a hexagonal-shaped forward end 44 .
- the peripheral segments 42 have the same general shape as the peripheral segments 16 of FIGS. 1-5 , but their outer surfaces 48 are flat rather than curved.
- the warhead 40 In the closed position the warhead 40 is cylindrical with a hexagonal cross section. It will be appreciated that in alternative embodiments other polygonal cross-sectional shapes may be utilized.
- FIG. 7 illustrates one manner of deployment of a warhead 10 or 40 (identified as 10 for ease of description).
- a set of multiple warheads 10 may be stacked in a cylindrical canister 50 that can be launched from an airborne vehicle.
- the individual warheads 10 are ejected from the canister 50 above an area of a target.
- a spinning motion is imparted to it by suitable means, examples of which are described below.
- sensing circuitry 52 detects the target and initiates the opening and detonation of the warhead 10 in a desired manner.
- the warhead is opened 10 by releasing the latch 22 , causing the peripheral segments 16 to rotate on the hinges 20 under effect of centrifugal force created by the spinning motion. Once the peripheral segments 16 are in the fully open position, the warhead 10 is detonated.
- Munition spin can be achieved using a small rocket motor with canted nozzles. Other techniques could be used including aerodynamic spin-up or gun-firing induced spin for example, depending on the type of delivery system in use.
- SADARM a weapon system known as SADARM
- an artillery round is used which carries several EFP-like munitions. In that case the artillery projectile is spun up during launch and the munitions are ejected over the target while the artillery projectile is still spinning
- the spin rate may be intentionally decreased after firing, using a vortex parachute for example, to a lower rate for scan and fire phase.
- the munition could attain the erected or open state during such a lowered spin rate while hanging on a parachute.
- the mode of operation may depend on how and when a target is identified as a soft target versus a hard target in a given application, as the geometric transformation would be made at or after that time. It could be that the decision about which configuration to use is made even before the artillery projectile is launched. If that is normally the case, then the transformation might occur during a higher spin rate phase, such as during parachute deployment in SADARM-style systems for example.
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Abstract
Description
- The present invention is related to the field of explosive warheads, and in particular to air-delivered tactical warheads used against ground targets such as vehicles and personnel.
- Warheads of the type known as explosively formed penetrators or EFPs are generally known. In one type of EFP, a liner closes one end of a cylindrical body filled with high explosive. The liner is of a relatively dense and low-yield material such as copper. Upon detonation, the liner forms an elongated, high-velocity slug capable of penetrating steel vehicle bodies and other relatively hard target objects. In some cases the liner has patterning to promote a desired pattern of fragmentation, such as to form a ring of smaller projectiles or “p-charges” about a central EFP slug. The smaller projectiles are effective against lighter vehicles, other ground-based equipment, and personnel.
- The effectiveness of air-delivered tactical warheads can be improved by features providing for altering the warhead configuration depending on the type of target, specifically depending on whether the target is primarily an armored vehicle or similar single hardened target or primarily a collection of lighter vehicles and/or personnel in a small area. For a single hardened target, a configuration maximizing the power of an EFP slug can be used, while for area targets a configuration maximizing forward-directed fragmentation can be used. The selection may be made dynamically based on the characteristics of targets as they are pursued or encountered, either by human user input or by automatic action of target acquisition electronics carried by the warhead.
- A disclosed warhead has a generally cylindrical shape and is divided into a conical central segment and a plurality of peripheral segments surrounding the central segment. The central segment has a disk-shaped liner at a front end, the liner bounding a cavity of the central segment filled with high explosive and configured to form one or more high-speed projectiles in a forward direction upon detonation of the high explosive. In one embodiment the liner is configured to form an EFP slug, and may also include separate smaller p-charges for lighter targets in the area of an armored vehicle or similar hardened target. The peripheral segments are hingedly attached to the central segment about the liner at the front end. Each peripheral segment has an outer segment face bounding a cavity of the peripheral segment filled with high explosive, and the segment faces of the peripheral segments form sidewall portions of the warhead when the peripheral segments are in a closed or folded position. The peripheral segments are operable to be released from the folded position to an open position in which the segment faces are pointed in the forward direction for detonation. A detonator initiates simultaneous detonation of the high explosive of the central and peripheral segments.
- The warhead may be used in the closed position, in which case the explosions of the peripheral segments provide confinement for the explosive of the central segment, resulting in maximized energy imparted to the EFP slug formed by the liner (as well as any separate p-charges from the liner if present). In this use the result is similar to that of the conventional EFP warhead. The warhead may also be used in the open position, in which case the fragments formed from the outer walls of the peripheral segments are directed forward toward area target(s), adding to the destructive effect of the EFP slug and any p-charges formed by the liner. In one embodiment, the manner of use is selectable, enabling flexible deployment based on specific target types. For example, the opening of the warhead may be enabled at a time of launch of the warhead, or at a time of target acquisition after launch. Thus a single warhead type can be carried in the field and used in a flexible manner to support different missions and tactical situations.
- The foregoing and other objects, features and advantages will be apparent from the following description of particular embodiments of the invention, as illustrated in the accompanying drawings in which like reference characters refer to the same parts throughout the different views. The drawings are not necessarily to scale, emphasis instead being placed upon illustrating the principles of various embodiments of the invention.
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FIG. 1 is a perspective view of a warhead with peripheral segments in folded positions as at launch; -
FIG. 2 is a schematic rear view of the warhead; -
FIGS. 3-5 are views of the warhead from different angles and with peripheral segments in both folded and open positions; -
FIG. 6 is a view of a warhead according to an alternative embodiment; and -
FIG. 7 is a schematic diagram depicting use of the warhead. -
FIG. 1 shows a warhead 10 (also referred to as “submunition” herein) having acylindrical body 12 closed at one end by a disk-shaped liner 14. Thebody 12 is generally of steel or a similar hard, high-strength material, while theliner 14 is of a denser and more deformable material such as copper. Thebody 12 is divided into multiple peripheral segments 16 (shown as 16-1, 16-2 etc.) about the axis of thewarhead 10. In the illustrated example, fourperipheral segments 16 are used, with three segments 16-1, 16-2 and 16-3 being visible inFIG. 1 . Eachperipheral segment 16 is secured to acentral segment 18 by arespective hinge 20. Both theperipheral segments 16 andcentral segment 18 are hollow members having internal cavities filled with high explosive. One or more detonators (not shown inFIG. 1 ) are used to detonate the explosive when thewarhead 10 comes into range of a target. As described more fully below, detonation forms both an explosively formed penetrator (EFP) slug fromliner 14 as well as a number of smaller fragments. Thewarhead 10 may be used in two basic configurations. In the configuration shown inFIG. 1 , the main effect is that of the EFP formed byliner 14, which can be used against harder point targets such as armored vehicles. In another configuration described below, a somewhat diminished EFP effect is accompanied by a hail of fragments forming smaller projectiles, usable against softer and/or area targets such as light vehicles and personnel. The first configuration, shown inFIG. 1 , is referred to herein as the “closed” or “folded” configuration or position, while the second configuration is described below and is referred to as the “open” or “unfolded” position. -
FIG. 2 is a schematic view of the bottom of thewarhead 10. Triangular-shaped bottom surfaces of the fourperipheral segments 16 are shown. As described more fully below, thecentral segment 18 has a cone shape, broad at the top and narrow at the bottom, while theperipheral segments 16 have complementary annular-section or wedge shapes having triangular radial cross section. Shown schematically is alatch 22 used to maintain thewarhead 10 in the closed or folded configuration, the latch being disengaged during operation to enable theperipheral segments 16 to rotate about thehinges 20 to the open position. Also indicated schematically arerespective detonation points 24 for the 16, 18. There may be distinct detonators (not shown) used forsegments 16, 18, or in an alternative embodiment there may be fewer detonators (e.g., one) coupled to therespective segments detonation points 24 by detonation cord for example. -
FIGS. 3 and 4 are side views illustrating the opening of thewarhead 10 during operation.FIG. 3 shows thewarhead 10 in the closed position, as inFIGS. 1 and 2 . Thedotted lines 30 indicate inward-facing surfaces of the wedge-shapedperipheral segments 16, which abut the rear conical surface of thecentral segment 12. When theperipheral segments 16 are in the closed position, the curvedouter surfaces 34 of theperipheral segments 16 together form the cylindrical sidewall of thewarhead 10. -
FIG. 4 shows thewarhead 10 in the open position, in which theperipheral segments 16 have rotated approximately 90 degrees so that their respective curvedouter surfaces 34 are facing in the same forward direction as theliner 14. Only two of theperipheral segments 16 are shown; it will be appreciated that the other twoperipheral segments 16 open in directions out of the plane ofFIG. 4 . -
FIG. 5 shows a front view of thewarhead 10 in the open position as inFIG. 4 . All fourperipheral segments 16 are shown. Also shown is a particular patterning of theliner 14, specifically acentral depression 36 and a ring of surroundingsmaller depressions 38. This patterning promotes a predetermined fragmentation of theliner 14 upon detonation to achieve a desired effect. Specifically, the center portion of theliner 14 forms a relatively large EFP slug as for other types of EFP warheads. The outer ring ofdepressions 38 fragments into smaller projectiles which can be effective against personnel and light vehicles. When thewarhead 10 is detonated in the open position as inFIG. 5 , this latter effect is increased by forward-directed fragments created from thewalls 34 of theperipheral segments 16. - In general, the
warhead 10 may be detonated in either the folded (closed) or open position. In some embodiments, the manner of use may be fixed, while in other embodiments it may be user-selectable in some manner. As an example of a fixed use, thelatch 22 may be non-releasable or even replaced by other structure to fixedly retain theperipheral segments 16 in the closed position, such as by screws or similar fasteners or even welding. In this embodiment thewarhead 10 may be used in the same manner as a conventional EFP warhead. The explosion of theperipheral segments 16 acts to confine the explosion of thecentral segment 18, increasing the velocity and effectiveness of the slug and any other projectiles formed by theliner 14. This kind of use may also be selected, for example by simply refraining from unlatching or releasing theperipheral segments 16 prior to detonation. - If the manner of use is selectable, then a variety of control schemes for detonation with or without release of the
peripheral segments 16 to the open position may be used. As noted, when areleasable latch 22 is used, in a given application it may not be activated, so that thewarhead 10 is detonated with theperipheral segments 16 retained in the folded position ofFIG. 3 . The detonator and latch 22 may also be configured to initiate detonation of thewarhead 10 with theperipheral segments 16 in the open position after release by thelatch 22. In this case the projectiles formed by fragmentation of theouter surfaces 34 of theperipheral segments 16 are directed forward toward the target, enhancing effectiveness against lighter equipment and/or personnel. Selection and timing of the position of detonation may be made in a variety of ways. In one case, electronic control circuitry carried by the warhead controls operation. The circuitry may be programmed or otherwise instructed to use particular timing and/or conditions for releasing thelatch 22 to attain the open position for detonation. In one example, the release may be enabled by user input prior to launch of thewarhead 10 toward a target, which may be effective when the user knows the characteristics of the target prior to launch. Alternatively, the release may be enabled at a time of target acquisition by automatic action of the control circuitry carried by the warhead. This configuration can increase effectiveness when the exact characteristics of the target are not known at launch but can be ascertained by the control circuitry based on sensor input (e.g., visible-light or infrared imaging input). - The
outer surfaces 34 of theperipheral segments 16 may be specifically configured to achieve a desired fragmentation into projectiles of predetermined size and shape upon detonation of thewarhead 10. For example, thesurfaces 34 may be scored with a pattern of lines. Alternatively, a relief pattern of thickness variation may be used, such as dimpling, analogous to the above-describeddepressions 38 of theliner 14. -
FIG. 6 shows analternative embodiment 40 employing sixperipheral segments 42 along with acentral segment 44 having a hexagonal-shapedforward end 44. Theperipheral segments 42 have the same general shape as theperipheral segments 16 ofFIGS. 1-5 , but theirouter surfaces 48 are flat rather than curved. In the closed position thewarhead 40 is cylindrical with a hexagonal cross section. It will be appreciated that in alternative embodiments other polygonal cross-sectional shapes may be utilized. -
FIG. 7 illustrates one manner of deployment of awarhead 10 or 40 (identified as 10 for ease of description). A set ofmultiple warheads 10 may be stacked in acylindrical canister 50 that can be launched from an airborne vehicle. Theindividual warheads 10 are ejected from thecanister 50 above an area of a target. As awarhead 10 is ejected, a spinning motion is imparted to it by suitable means, examples of which are described below. As thewarhead 10 is spinning and falling towards a target, sensingcircuitry 52 detects the target and initiates the opening and detonation of thewarhead 10 in a desired manner. The warhead is opened 10 by releasing thelatch 22, causing theperipheral segments 16 to rotate on thehinges 20 under effect of centrifugal force created by the spinning motion. Once theperipheral segments 16 are in the fully open position, thewarhead 10 is detonated. - Munition spin can be achieved using a small rocket motor with canted nozzles. Other techniques could be used including aerodynamic spin-up or gun-firing induced spin for example, depending on the type of delivery system in use. In a weapon system known as SADARM, an artillery round is used which carries several EFP-like munitions. In that case the artillery projectile is spun up during launch and the munitions are ejected over the target while the artillery projectile is still spinning In this kind of system the spin rate may be intentionally decreased after firing, using a vortex parachute for example, to a lower rate for scan and fire phase. In one embodiment, the munition could attain the erected or open state during such a lowered spin rate while hanging on a parachute. The mode of operation may depend on how and when a target is identified as a soft target versus a hard target in a given application, as the geometric transformation would be made at or after that time. It could be that the decision about which configuration to use is made even before the artillery projectile is launched. If that is normally the case, then the transformation might occur during a higher spin rate phase, such as during parachute deployment in SADARM-style systems for example.
- While various embodiments of the invention have been particularly shown and described, it will be understood by those skilled in the art that various changes in form and details may be made therein without departing from the spirit and scope of the invention as defined by the appended claims.
Claims (22)
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US13/604,887 US8955443B1 (en) | 2012-09-06 | 2012-09-06 | Warhead having selectable axial effects |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US13/604,887 US8955443B1 (en) | 2012-09-06 | 2012-09-06 | Warhead having selectable axial effects |
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| US20150033971A1 true US20150033971A1 (en) | 2015-02-05 |
| US8955443B1 US8955443B1 (en) | 2015-02-17 |
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Cited By (3)
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| CN106382860A (en) * | 2016-11-11 | 2017-02-08 | 万耀东 | Folding type ground drilling bomb |
| EP3171121A1 (en) | 2015-11-18 | 2017-05-24 | Textron Systems Corporation | Multi-warhead munition with configurable segmented warhead |
| US20170146326A1 (en) * | 2015-08-08 | 2017-05-25 | TDW Gesellschaft für verteidigungstechnische Wirksysteme mbH | Method and device for controlling the power type and power emission of a warhead |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| IL222989A (en) * | 2012-11-12 | 2016-02-29 | Israel Aerospace Ind Ltd | Warhead |
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| US3960085A (en) | 1967-05-25 | 1976-06-01 | The United States Of America As Represented By The Secretary Of The Navy | Variable geometry warhead |
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| US5377594A (en) * | 1989-08-15 | 1995-01-03 | Alford; Sidney C. | Flexible linear explosive cutting or fracturing charge |
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| US20050126420A1 (en) * | 2003-09-10 | 2005-06-16 | Givens Richard W. | Wall breaching apparatus and method |
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| US20170146326A1 (en) * | 2015-08-08 | 2017-05-25 | TDW Gesellschaft für verteidigungstechnische Wirksysteme mbH | Method and device for controlling the power type and power emission of a warhead |
| US9903692B2 (en) * | 2015-08-08 | 2018-02-27 | TDW Gesellschaft für verteidigungstechnische Wirksysteme mbH | Method and device for controlling the power type and power emission of a warhead |
| EP3171121A1 (en) | 2015-11-18 | 2017-05-24 | Textron Systems Corporation | Multi-warhead munition with configurable segmented warhead |
| US10145661B2 (en) | 2015-11-18 | 2018-12-04 | Textron Innovations Inc. | Multi-warhead munition with configurable segmented warhead |
| CN106382860A (en) * | 2016-11-11 | 2017-02-08 | 万耀东 | Folding type ground drilling bomb |
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| Publication number | Publication date |
|---|---|
| US8955443B1 (en) | 2015-02-17 |
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