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.
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, 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. In this embodiment 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.
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 a releasable latch 22 is used, 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
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. For example, the surfaces 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-described depressions 38 of the liner 14.
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.
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