Description:

DEDICATORY CLAUSE

The invention described herein may be manufactured, used and licensed by or for the U.S. Government for governmental purposes without payment of any royalties thereon.

BACKGROUND OF THE INVENTION

I. Field of the Invention

The present invention pertains to tandem warheads. More particularly the present invention pertains to a tandem warhead that requires only a single initiation mechanism.

II. Discussion of the Background

Tandem warheads refer to warheads having two explosive charges. Typically, each charge is utilized for a specific lethal effect. Conventional tandem warheads have two initiation mechanisms. Typically the forward charge is initiated first with a second warhead being initiated after a prescribed time delay. In anti-armor warhead systems, the shaped charge is the most common kill mechanism. However, typical shaped-charge warheads do not have adequate fragmentation characteristics to be effective against personnel and other soft targets.

The need for two initiating mechanisms or fuzes in the conventional tandem warhead augments the cost and complexity of such devices and increases the likelihood of initiation failure.

SUMMARY OF THE INVENTION

The present invention utilizes a single initiation mechanism to activate the two respective explosive charges in the tandem warhead. This single initiation mechanism increases reliability while reducing the complexity and cost of the warhead.

In addition, the present invention utilizes a shaped-charge in the rear of the warhead sub-system as both an armor piercing kill mechanism and an initiation device for the forward fragmentation charge. Further, an explosive charge positioned at the front of the warhead sub-system acts as a fragmentation charge thereby providing desirable fragmentation effects for the warhead sub-system.

Accordingly, one object of the present invention is to provide a tandem warhead that requires only one initiation mechanism.

Another object of the present invention is to provide for a tandem warhead that combines armor piercing capability with lethal fragmentation capabilities.

These and other objects of the present invention are realized by a tandem warhead sub-system having a casing that has a forward portion, a middle portion and a rear portion. A frontal explosive fragmentation charge is positioned within the forward portion of the casing and a shaped charge is positioned within the rear portion of the casing.

A shaped charge jet formation region is located between the shaped charge and the frontal explosive fragmentation charge. The jet formation region is an open region within the middle portion of the casing. A detonating means or mechanism is positioned behind the shaped charge to initiate the shaped charge. A signal generating means or target detection device is provided for sending a detonation signal to the detonating means upon impact with a target.

Upon the detonating means receiving the detonation signal, detonation of the shaped charge occurs resulting in the collapse of the metallic shaped charge liner and formation of a high speed metallic jet in the jet formation region so as to penetrate and cause the initiation of the frontal explosive charge. The frontal explosive charge is a fragmentation charge. Fragmentation material in the forward portion of the metallic fragmenting casing is sprayed as a result of the fragmentation charge, i.e., the frontal explosive charge, being initiated.

At the detonation of the frontal explosive charge, the shaped charge jet generated by the shaped charge has so penetrated and initiated the frontal explosive charge that a residual portion of the jet continues forward in front of the frontal explosive charge thus providing armor-piercing capability to the warhead.

BRIEF DESCRIPTION OF THE DRAWINGS

A more complete appreciation of the invention and many of the attendant advantages thereof will be readily obtained as the same becomes better understood by reference to the following detailed description when considered in connection with the accompanying drawings, wherein:

FIG. 1 is a see-through side view of the tandem warhead of the present invention;

FIG. 2 is a schematic drawing showing that the trigger switch is electrically wired to detonator 52;

FIG. 3 is a screen shot from a CTH hydrocode analysis illustrating the respective positions of the frontal explosive fragmentation charge and the shaped charge prior to initiation;

FIG. 4 is a screen shot from a CTH hydrocode analysis illustrating the respective positions of the frontal explosive charge and the shaped charge immediately after initiation;

FIG. 5 is a screen shot from a CTH hydrocode analysis illustrating the respective positions of the frontal explosive fragmentation charge and the shaped charge immediately after the time frame shown in FIG. 3; and

FIG. 6 is screen shot from a CTH hydrocode analysis illustrating the respective positions of the frontal explosive charge and the shaped charge immediately after the time frame shown in FIG. 4.

DETAILED DESCRIPTION

Referring now to the drawings wherein like reference numerals designate identical or corresponding parts, and more particularly to FIG. 1, the single initiated warhead 10 of the present invention is provided with a casing 12 having a forward portion 14, a middle portion 18, and a rear portion 20. The forward portion 14 of casing 12 includes a metallic fragmentation case 16.

At the very front of the warhead 10 is the nose or front end 24 that is a part of the forward portion of the casing. Behind the rear portion 20 of the casing 12 is a rear end region 22.

A frontal or forward explosive charge 26 is positioned within the forward portion 14 of casing 12. The frontal charge 26 is a fragmentation charge. An explosive liner 28 (i.e., frontal explosive liner) in conjunction with the forward portion 14 of casing 12 forms a receptacle that houses the frontal charge 26. The explosive liner 28 is made of a plastic or similarly suitable material. The explosive liner 28 has a platform region 32 that is orthogonal to and is intersected by the center horizontal axis 60 of the warhead 10. Reference numerals 36 and 38 represent points on respective sloped, lateral sides of the explosive liner 28. The explosive liner is generally cup-shaped and forms a hollow inlet 34. A booster charge 30 is positioned on the platform region 32.

Within the rear portion 20 of casing 12 is shaped charge 40. A metallic shaped-charge liner 42 in conjunction with the rear portion 20 of casing 12 forms a shaped-charge housing. The shaped-charge liner 42 of the prototype of the present invention has a conical shape with a center point 44 being the closest point on the liner 42 to the rear end region 22. Reference numerals 46 and 48 represent points on respective, sloped lateral sides of the shaped-charge liner 42. The center point 44 of liner 42 is intersected by the center horizontal axis 60 of the warhead 10.

It is noted that other shapes of liners can be utilized within the concept of the present invention, with these shapes including shaped-charge liners having conical, hemispherical, trumpet, or tulip shapes.

The middle portion 18 of casing 12 is a hollow region that serves as a shaped charge jet formation region 50. An impact switch or sensor 56 is positioned at the nose or front end 24 of the casing 12. Upon impact with a target, a signal from the impact switch 56 is generated to the fuse 54 and detonator 52 located at the rear end 22 of the warhead 10.

Thus, upon a signal from the impact switch 56 being sent to the fuse 54 and detonator 52 the shaped charge 40 is initialized or detonated. An electrical wire or cable 64 connects the trigger switch to the fuse 54 which acts as a safe and arm device (FIG. 2). Immediately after the detonation of shaped charge 40, the explosive causes the metal liner 42 of the shaped charge to converge along the central axis into a shaped charge jet 58 into the jet formation region 50. The shaped charge jet 58 is directed into the inlet region 34 of forward explosive liner 28 and penetrates the explosive liner 28 causing detonation of the booster charge 30 and frontal charge 26.

With reference to FIG. 3, the shaped charge 40 and frontal charge 26 are shown as positioned after the warhead has been released or fired, but prior to impact. The arrow 62 demonstrates the direction in which the respective charges are moving.

In FIG. 4, the beginning moment of initiation is depicted with the shaped-charge jet 58 beginning to form and the shaped charge 40 moving in the direction of the frontal charge 26.

In FIG. 5 the shaped charge jet 58 has penetrated the frontal charge 26 and the shaped charge 40 has impacted the frontal charge 26.

In FIG. 6 a forward portion 58F of shaped charge jet 58 has totally penetrated the frontal charge 26 and is positioned at the front thereof and the shaped charge 40 has partially combined with the frontal charge. The forward charge portion 58F that is positioned to the front of frontal charge 26 includes metallic particles from the metal shaped-charge liner 42 that have been thrust forward by a shock wave of heat and pressure.

The present invention allows for the utilization of a single warhead in the engagement of a diverse set of targets. Although the performance of the shaped charge 40 is degraded as it penetrates and initiates the forward fragmentation charge 26, CTH hydrocode analyses and preliminary testing have demonstrated that the configuration of the present invention allows for sufficient penetration of lightly armored targets.

Testing has verified that the shaped charge jet 58 would reliably initiate the explosive of the forward fragmentation charge 26 and that the residual shaped charge jet 58F will penetrate light armor. The forward fragmentation charge 26 sprays fragments in a forward direction from 0 to 60 degree polar zones.

Modifications are possible without deviating from the spirit of the present invention. Accordingly the scope of the invention is limited only by the claim language which follows hereafter.