Dual-function penetrator liner for multifunctional warhead

Abstract

A dual-function penetrator liner for a multifunctional warhead. A dome-shaped outer portion is disposed in an inner front end of a warhead body to be concave in a direction opposite to a direction in which the warhead body is fired. A fastening portion is disposed in an outer circumferential direction of the outer to fasten the outer portion to the warhead body. A conical central portion is enclosed by the outer portion to protrude in a direction opposite to the direction in which the warhead body is fired. The outer portion and the central portion are concentric.

Claims

1. A multifunctional warhead including a warhead body and a dual-function penetrator liner which has functions of forming fragments and functioning as an explosively formed penetrator, wherein the dual-function penetrator liner comprises: a dome-shaped outer portion disposed in an inner front end of the warhead body to be concave in a direction opposite to a direction in which the warhead body is fired; a fastening portion disposed in an outer circumferential direction of the outer portion to fasten the outer portion to the warhead body; and a conical central portion enclosed by the outer portion to protrude in a direction opposite to the direction in which the warhead body is fired, wherein the outer portion and the central portion are concentric, and wherein thickness of the outer portion is larger than thickness of the central portion to obtain an optimal penetration performance, and the fastening portion is stepped along an outermost peripheral portion of the outer portion.

2. The multifunctional warhead according to claim 1, wherein a maximum diameter of the central portion is about 30% of a maximum diameter of the outer portion.

3. The multifunctional warhead according to claim 2, wherein the thicknesses of the outer portion and the central portion are measured in the direction in which the warhead body is fired.

4. The multifunctional warhead according to claim 3, wherein the thickness of the outer portion is about 3% to about 5% of a maximum diameter of the outer portion.

5. The multifunctional warhead according to claim 4, wherein the thickness of the central portion is about 2% to about 4% of a maximum diameter of the central portion.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) The above and other objects, features and advantages of the present invention will be more clearly understood from the following detailed description taken in conjunction with the accompanying drawings, in which:

(2) FIG. 1 is a cross-sectional view illustrating a configuration of a multifunctional warhead equipped with a dual-function penetrator liner for a multifunctional warhead according to the present invention;

(3) FIGS. 2A and 2B are a cross-sectional view and a perspective view illustrating the dual-function penetrator liner for a multifunctional warhead according to the present invention;

(4) FIGS. 3A and 3B are a front image and a top image illustrating a dual-function penetrator liner for a multifunctional warhead according to the present invention;

(5) FIG. 4A is a schematic view illustrating a metal jet generated by a typical shaped charge warhead, and

(6) FIG. 4B is a schematic view illustrating the shaped charge warhead;

(7) FIG. 5A is a schematic view illustrating a penetrator generated by a typical explosively formed penetrator warhead, and

(8) FIG. 5B is a schematic view illustrating the explosively formed penetrator warhead; and

(9) FIG. 6 is a schematic view illustrating changes in the shape of a dual-function penetrator liner for a multifunctional warhead, over time, after being fired.

DESCRIPTION OF THE PREFERRED EMBODIMENTS

(10) For better understanding of the present invention, exemplary embodiments of the present invention will be described with reference to the accompanying drawings. The embodiments of the present invention may be modified in many different forms and the scope of the present invention should not be limited to the embodiments set forth herein. Rather, these embodiments are provided so that this disclosure will be thorough and complete, and will fully convey the concept of the present invention to those skilled in the art. In the drawings, the shapes and dimensions may be exaggerated for clarity, and the same reference numerals will be used throughout to designate the same or like components. Detailed explanations of known related functions and constitutions may be omitted to avoid unnecessarily obscuring the subject matter of the present invention.

(11) The present invention relates to a dual-function penetrator liner 32 for a multifunctional warhead, having dual functions of forming fragments and functioning as an explosively formed penetrator. The dual-function penetrator liner 32 includes: a dome-shaped outer portion 32b disposed in an inner front end of a warhead body 33 to be concave in a direction opposite to a direction in which the warhead body 33 is fired; a fastening portion 32c disposed on the outer circumference of the outer portion 32b to fasten the outer portion 32b to the warhead body 33; and a central portion 32a enclosed by the outer portion 32b to protrude in the direction opposite to the direction in which the warhead body 33 is fired. The outer portion 32b and the central portion 32a are concentric.

(12) The maximum diameter D2 of the central portion 32a is about 30% of the maximum diameter D1 of the outer portion 32b.

(13) The thicknesses of the components are measured in a direction in which a guided missile is fired.

(14) The thickness t1 of the outer portion 32b is about 3% to 5% of the maximum diameter D1 of the outer portion 32b, while the thickness t2 of the central portion 32a is about 2% to 4% of the maximum diameter D2 of the central portion 32a.

(15) The fastening portion 32c is stepped along the outermost peripheral portions of the outer portion 32b.

(16) In the dual-function penetrator liner 32 for a multifunctional warhead according to the present invention, when a multifunctional warhead 31 functioning as fragments and an explosively formed penetrator is disposed within a guided missile, the dual-function penetrator liner 32 can destroy a target by minimizing a decrease in kinetic energy of the explosively formed penetrator by removing interferences from front components or the like. FIG. 1 is a cross-sectional view illustrating a configuration of the multifunctional warhead 31 equipped with the penetrator liner 31 having dual functions for a multifunctional warhead according to the present invention. FIG. 1 is given for better understanding of the shape and fastening method of the dual-function penetrator liner for a multifunctional warhead according to the present invention.

(17) FIGS. 2A and 2B are a cross-sectional view and a perspective view illustrating the dual-function penetrator liner for a multifunctional warhead according to the present, invention.

(18) As apparent from FIGS. 1, 2A, and 2B, the central portion 32a has the shape of a shaped charge, and the outer portion 32b has the shape of an explosively formed penetrator. FIG. 2A is the cross-sectional view of the dual-function penetrator liner for a multifunctional warhead, illustrating the diameters and thicknesses of respective portions. The maximum diameter D1 of the outer portion is the diameter of the outer portion 32b adjoining the inner surface of the warhead body 33. The maximum diameter D2 of the central portion means the diameter of a round-machined edge portion of the central portion adjoining the outer portion, i.e. the maximum diameter of the portion machined to be round.

(19) The ratio of the maximum diameter D1 of the outer portion with respect to the maximum diameter D2 of the central portion must be a specific value to maximize an effect of removing the front components in the guided missile (obtained by the central portion) and an effect of penetrating a target (obtained by the outer portion). When analysis and experiment were performed by using the ratio of the maximum diameters between the outer portion 32b and the central portion 32a as a variable, it was determined that optimal penetration performance can be obtained when the maximum diameter of the central portion is 30% of the maximum diameter of the outer portion. This can be represented by the following formula 1:
D.sub.2/D.sub.10.3,[Formula 1]
where D1 is the maximum diameter of the outer portion, and D2 is the maximum, diameter of the central portion.

(20) In addition, although the explosively formed penetrator for a multifunctional warhead may be designed such that the thickness thereof is variable, optimal performance can be obtained only in the case that the thicknesses of respective portions are predetermined ratios of the diameter of the dual-function penetrator liner 32 for a multifunctional warhead. Specifically, the thickness t2 of the central portion is about 2% to about 4% of the maximum diameter D2 of the central portion, while the thickness t1 of the outer portion is about 3% to about 5% of the maximum diameter D1 of the outer portion. These can be represented by the following formulas 2 and 3:
0.03t.sub.1/D.sub.10.05[Formula 2]
0.02t.sub.2/D.sub.20.04,[Formula 3]

(21) where D1 is the maximum diameter of the outer portion, D2 is the maximum diameter of the central portion, t1 is the thickness of the outer portion, and t2 is the thickness of the central portion.

(22) FIG. 4A is a schematic view illustrating a metal jet generated by a typical shaped charge warhead, and FIG. 4B is a schematic view illustrating the shaped charge warhead. In addition, FIG. 5A is a schematic view illustrating a penetrator generated by a typical explosively formed penetrator warhead, and FIG. 5B is a schematic view illustrating the explosively formed penetrator warhead. Referring to FIGS. 4A, 4B, 5A, and 5B, a shaped charge liner 12 and a detonator tube are concentric, while an explosively formed penetrator liner 22 and a detonator tube are concentric. These configurations are intended to maximize the explosive performance of guided missiles. The dual-function penetrator liner 32 for a multifunctional warhead according to the present invention is also configured to be concentric with a detonator tube 36.

(23) Next, the explosion sequence of the guided missile, to which the dual-function penetrator liner for a multifunctional warhead according to the present invention is applied, will be described. In response to an explosive signal being received from a fuse disposed in a rear cover 35 at the rear of the multifunctional warhead 31, explosive energy of an electric explosive tube detonates the detonator tube 36 and then detonates a main charge 34 within the warhead. Then, first, the warhead body 33 made of a metal, forming the shell of the warhead, is fragmented by expansion and rupture, due to the explosive energy of the main charge 34 transferred thereto. In subsequence, the explosive energy of the main charge 34 is transferred in the axial direction of the warhead, thereby arriving at the central portion 32a of the dual-function penetrator liner 32 for a multifunctional warhead, prior to the outer portion 32b. The central portion 32a is collapsed by the explosive energy, thereby being deformed into a metal jet having a jet tip speed of about 7 km/sec to about 9 km/sec. The metal jet is ejected to the front of the guided missile, thereby penetrating and rupturing components disposed in front of the guided missile. Afterwards, the explosive energy is transferred to the outer portion 32b, causing the outer portion 32b to be self-forged into the shape of a penetrator. The self-forged penetrator, i.e. the outer portion 32b, is ejected forwardly from the guided missile at a speed of about 2 km/sec to about 4 km/sec. Since the outer portion 32b having the shape of a penetrator is ejected along a path obtained as a hollow space, penetrated and ruptured by the central portion 32a in the shape of a metal jet, a decrease in the penetration by interferences with the front components is reduced. In other words, the dual-function penetrator liner 32 for a multifunctional warhead is deployed into a shape having two functions, i.e. forming a metal jet and an explosively formed penetrator, by the explosive energy of main charge.

(24) FIG. 6 is a schematic view illustrating changes in the shape of a dual-function penetrator liner for a multifunctional warhead, over time, after being fired. Referring to FIG. 6, the shape of the dual-function penetrator liner 32 for a multifunctional warhead is gradually deformed, in the direction from right to left. As in the right part of FIG. 6, at an early stage of firing, both the central portion 32a and the outer portion 32b are ejected. Gradually, the central portion is ejected ahead due to the faster speed thereof, and the outer portion follows after the central portion. Afterwards, as in the left part of FIG. 6, the central portion 32a proceeds, separated from the outer portion 32b.

(25) When the dual-function penetrator liner 32 for a multifunctional warhead is connected to a warhead 33 designed to form fragments, the dual-function penetrator liner 32 is fixed to the warhead 33 using a locking nut 37, since the concentricity of assembly is important for obtaining a predetermined level of penetration performance. Afterwards, adjoining portions of the warhead body 33 and the dual-function penetrator liner 32 for a multifunctional warhead are sealed using an adhesive 38 or the like. This can consequently remove gaps, through which the main charge 34, i.e. a castable plastic bonded explosive, or the like may leak when injected through the rear portion of the warhead body. It is advantageous for increasing penetration force when shockwaves of explosive energy are symmetrically transferred due to detonation occurring at the center of the warhead. Thus, the detonator tube 36 is disposed to be accurately located in the central portion of the main charge 34, using a charging tool or the like, so that the detonator tube 36 and the main charge 34 are set to be concentric when the main charge 34 is cured.

(26) Although the exemplary embodiments of the present disclosure have been described for illustrative purposes, a person skilled in the art will appreciate that various modifications and other equivalent embodiments are possible without departing from the essential characteristics of the present disclosure. It should be understood that the present invention is not limited to the foregoing particular embodiments but the technical scope of the present invention shall be defined by the technical spirit of the appended Claims. In addition, it should be understood that the present invention shall embrace all modifications, equivalents, and substitutions within the spirit and scope of the present invention defined by the appended Claims.