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Publication numberUS3796159 A
Publication typeGrant
Publication dateMar 12, 1974
Filing dateFeb 1, 1966
Priority dateFeb 1, 1966
Publication numberUS 3796159 A, US 3796159A, US-A-3796159, US3796159 A, US3796159A
InventorsR Conger
Original AssigneeUs Navy
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Explosive fisheye lens warhead
US 3796159 A
Abstract
An aimable warhead in the form of an explosive cylindrical lens with detonators spaced about its circumference for simultaneously aiming and firing the warhead in any direction by selectively firing a detonator on a side thereof opposite to the direction of aim and focusing the detonation waves in the aimed direction.
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Description  (OCR text may contain errors)

United States Patent [191 Conger Mar. 12, 1974 EXPLOSIVE FISHEYE LENS WARHEAD [75] Inventor: Robert L. Conger, Riverside, Calif.

[73] Assignee: The United States of America as represented by the Secretary of the Navy, Washington, DC.

[22] Filed: Feb. 1, 1966 [21] App]. No.: 524,352

[52] US. Cl 102/67, 102/56, 102/DIG. 2 [51] Int. Cl.....- F42b 13/48, F42b H00 [58] Field of Search lO2/7.2 R, 8, 9, l0, l6,

[56] References Cited UNITED STATES PATENTS 3,326,]25 6/1967 Silvia et al. 102/23 FIRE CONTROL Primary Examiner--Verlin R. Pendegrass Attorney, Agent, or FirmRichard S. Sciascia; J. M. St. Amand [5 7] ABSTRACT An aimable warhead in the form of an explosive cylindrical lens with detonators spaced about its circumference for simultaneously aiming and firing the warhead in any direction by selectively firing a detonator on a side thereof opposite to the direction of aim and focusing the detonation waves in the aimed direction.

3 Claims, 4 Drawing Figures PATENTEUIAR 12 m4 s;79s;159

FIRE CONTROL FIGJ FIG.2

PROPAGATION DIRECTION ROBERT L. CONGER INVENTOR.

FIG. 4 BY ATTORNEY EXPLOSIVE FISHEYE LENS WARHEAD The invention herein described may be manufactured and used by or for The Government of the United States of America for governmental purposes without the payment of any radial royalties thereon or therefor.

The present invention relates to fragmentation or blast warheads and the like, and more particularly to an explosive fisheye cylindrical lens.

This invention is related to copending application, Ser. No. 524,351 filed Feb. 1, l966 for Explosive Luneberg Lens Warhead.

When detonated, warheads currently used on guided missiles produce a fragment pattern that is either spherically or cylindrically symmetric about the warhead. Although the transfer of energy from the explosive to the fragments is efficient, only a small fraction of the fragments will intercept the target, assumed to be airborne, and therefore the overall efficiency of this type of warhead is low. A greater efficiency would be obtained if most of the energy were directed toward the target. A warhead having such capability is an aimable warhead.

Aiming is difficult because of the inability to determine, until a few milliseconds before the warhead is detonated, on which side of the target the missile and warhead will pass. Thus, in a period of a few milliseconds, the warhead must be aimed at the target and detonated. In this short time it is difficult to aim the warhead by changing its attitude, because the inertia of the warhead makes it difficult to physically rotate it into the proper position sufficiently fast to hit the target.

A system is disclosed herein for an aimable warhead in the form of an explosive fisheye cylindrical or spherical lens. With detonators spaced about its surface, the warhead can be simultaneously aimed and fired in any direction by firing a detonator on the opposite side. When a detonator opposite the direction of aim is fired, detonation waves progressing through the warhead will detonate all the explosive in the warhead in such a way as to focus the detonation waves on the side of the lens in the direction of aim. Equations are derived herein for the required detonation velocity as afunction of radius normal to a cylinder axis or through the center of a sphere; explosives are selected with the proper detonation velocities desired.

.It is an object of the invention; therefore, to form a warhead in the form of an explosive fisheye spherical or cylindrical lens.

Another object of the invention is to provide an efficient cylindrical warhead, aimable in any radial direction about its cylindrical surface.

A further object of the invention is to provide an explosive cylindrical warhead in which the explosive, when detonated along any line on.0ne side of warhead parallel to the cylinder axis, develops a shock wave focused on a line at the other side of said cylinder for propelling a concentration of warhead fragments in the direction of aim.

Other objects and many of the attendant advantages of this invention will become readily appreciated as the same becomes better understood by reference to the following detailed description when considered in connection with the accompanying drawings wherein:

FIG. 1 shows a typical fisheye lens warhead with a plurality of detonators spaced about its surface.

FIG. 2 is a series of cross-sectional views of a fisheye lens warhead, as in FIG. 1, showing progression of detonation wave through the warhead, from a point of detonation on one side, detonating the explosive in such a way as to focus the detonation waves on a point on the opposite side of the lens.

FIG. 3 illustrates the differential relationship for bending of the direction of propagation of a shock wave passing through a cylinder.

FIG. 4 illustrates the propagation direction of a shock wave in a fisheye lens.

The system discussed here is for a cylindrically symmetric warhead which can be aimed in a given radial direction about the cylinder axis without turning the warhead itself. The warhead 10 is constructed in the form of an explosive lens, analogous to Maxwell s fisheye. (J. c. Maxwell, Cambridge and Dublin Math J0ur., Vol. 8, 1854, p. 188.) The cylindrical warhead 10 has a plurality of linear arrays of exploding bridgewire-type detonators 12 (or plane-wave generators) mounted along lines about the surface of the explosive lens and parallel to the cylindrical axis. The warhead is simultaneously aimed and fired in a given direction by detonating any one of the detonator arrays or the like on the opposite side. The construction of the lens is such that the detonation waves, starting on an array line, fire all the explosive in the warhead in such a way that the detonation is focused on a line on the opposite side of the lens. Fire control system 18 determines the direction of aim, when and which detonator 12 to fire.

The fisheye lens warhead is constructed from a number of coaxial cylindrical shells 14 in which the detonation velocity v of each shell is given by the equation where r is the radius of the shell, r the radius of the lens, and v,, the detonation velocity at the lens surface. Equation (1), which is hereinafter derived, shows that the velocity increases slowly with r when r is small. Thus the central part of the lens can be uniform, as shown in FIG. 1. If there are five shells of explosive, for example, and the outer shell has a detonation velocity of 8,000 meters/sec, the detonation velocities might have the values shown in Table 1.

Table l. Detonation Velocity as a Function of Radius r r,, v, m/sec 0 to 0.5 r,, 0.25 r,, 4460 0.5 to 0.7 r,, 0.60 r,, 5720 0.7 to 0.8 r 0.75 r,, 6550 0.8 to 0.9 r 0.85 r, 7250 0.9 to L0 r,, 0.95 r, 8000 The detonation velocity of 4,460 meters/sec, in the first row of Table l, is lower than the detonation velocity of most explosives used in warheads. Although detonation velocities of 4,000 meters/sec and less can be obtained from low-density explosives, the detonation pressures produced by these explosives are also low. Baritol, a mixture of barium nitrate and TNT, is a better choice for the cylindrical core. Detonation velocities of Baritol mixtures can be 4,500 meters/sec or less, depending on the composition. Since the density of these explosives is high, the detonation pressure they produce is also high.

In tests of thin cylindrical fisheye explosive lens 6 inches in diameter and three-fourths inch thick each lens was constructed from coaxial rings of the explosives listed in Table 2. The first four rings were cast and composition C, was pressed into place. The first, third, and fourth detonation velocities are averages for 1.0 inch diameter charges of Table 2. Detonation Velocity of Explosives Used Radius. in Detonation inches Explosive velocity, m/sec to 1.50 67% Ba(NO 33 71 TNT 4890 1.50 to 210 33% Bu(NO;,),, 67'71 TNT 5720 2.10 to 2.40 TNT 6520 2.40 to 2.70 Composition B 7250 2.70 to 3.00 Composition C, 7900 the explosives as measured by streak camera and by pin switch oscilloscope methods. The second detonation velocity is a linear interpolation from the measured values for 50 percent Ba(NO )2 and 50 percent TNT, and for 100 percent TNT. The detonation velocity of Composition C is a handbook value. A comparison of Tables 1 and 2 shows that the detonation velocity of the inner ring deviated from the desired value by about percent. However, this deviation did not prevent the lens from functioning. The warheads tested detonated as theory indicated they should. Detonation started at the point of initiation A (top left in FIG. 2). By the time the detonation wave had passed halfway through the disc, the detonation front was almost plane; the detonation wave then converged, or focused, to a point B on the opposite side of the explosive lens (bottom right FIG. 2). Intense jets, which formed at this point, progressed away from the point of focus. FIG. 2 was drawn from a series of pictures taken by a Beckman & Whitley camera; another series of pictures showed the for mation of the jets as they move away from the point on the lens where the detonation waves converge. From the camera speed, which was 5.8 usec per frame, it was found that the jets have a velocity of about 3,500 meters/sec.

Tests proved conclusively that: the explosive lenses constructed in accordance with the invention perform effectively; (these warhead lenses produce jets that cause intensive damage at distances where an isotropic charge of the same size would have little effect; and the direction of the jets is a function of the point of initiation of the lens.

Equations for the explosive fisheye lens are derived here without any reference to optics.

The explosive fisheye lens is in the form of an inhomogeneous cylinder 10. If the explosive is detonated by a detonator 12 along a line parallel to the axis of the cylinder on the surface of the cylinder and the shock wave is to focus on a line at the other side of the cylinder, the propagation velocity of the shock wave must be larger on the outside of the cylinder, for this shock wave must travel farther in the same amount of time than a shock wave traveling through the center of the cylinder. Since the propagation velocity is a function of only the radius of the cylinder, lines normal to the shock fronts, or parallel to the direction of propagation, must lie in planes which are normal to the cylinder axis. Such a plane is shown in FIG. 3 where O is the axis of the cylinder. Bending of the propagation direction will result from the propagation velocity being a function of radius. In FIG. 2 the propagation velocity at a point r Ar will be greater by a small increment than the propagation velocity at the point r. This difference in propagation velocity causes a curvature of the direction of propagation by an amount Adi.

From FIG. 2, by Taylors expansion:

By trigonometry tan All; (v A! vAt/Ar/sin d1) sin d At(dv/dr) As At and Ar 0, this becomes dill sin I dl(dv/dr) where dill is the element of bending of the propagation direction. Since (from FIG. 3) dr/dt v cos I equation (4) can be written as d1l1=(dv/v) tan P The change in 101 or A I will be the difference between Aul: and the change in 0 or A6. From FIG. 3,

tan A6 (v A! sin D/r) As At 0, this becomes d0 (v sin Ddt/r) and from equations (4) and (7) dd sin I dt(dv/dr) (v sin 1 dt/r) Since dr/dt v cos 1 equation (8) can be written as dd tan @(dv/v) tan I (dr/r) Division by tan 1 and integration give r/v sin 1 k (10) where k is the constant of integration.

We will consider propagation curves starting at a point P on the surface of the cylinder of radius r l and passing through the cylinder to a second point on the opposite side, as shown in FIG. 4. The propagation velocity at the surface of the cylinder is assumed to have a value of unity. The propagation velocity inside the cylinder is less than 1.0. A particular propagation curve from P will make an angle a at P with a line passing through the center of the cylinder. From equation (10), since the propagation velocity equals 1.0 at the surface of the cylinder where r 1.0,

sina=k At 6 17/2, I 1'r/2: and therefore equation reduces to r/v* k where v* is the propagation velocity at 6 1r/2. From equations (5) and (10), by eliminating I we can derive the equation for the bending of the direction of 10 propagation,

dill (k dn/n V "2'2 k where n l/v.

The total angle of bending is 2:1 and, from equation l l a sin k. At 9 17/2, half the bending has taken place and v v*. Thus, from equations (11) and (13),

the total bending is given by WWW? (M) where n* l/v*.

It can now be shown that equation 14) is satisfied by n=(2/l +r When equation (14) is divided by 2 and equation (15) is substituted into the left side of equation (14), it can be integrated to give so that (16) becomes 1r/2 sin V lk 6 Taking the sin of 19) gives sin [(11/2) sin" V l P] cos (sin Vl k Thus the integral of equation (14) reduces to sin k, which shows that equation I5) is a solution of the integral equation (14). Equation (15), it can be noted, is the basis for equation (1).

Obviously many modifications and variations of the present invention are possible in the light of the above teachings. It is therefore to be understood that within the scope of the appended claims the invention may be practiced otherwise than as specifically described.

What is claimed is:

1. An aimable explosive warhead operable to be aimed without physical rotation of the warhead and fired in any given radial direction about the axis thereof, comprising:

a. an explosive fisheye lens warhead in the form of an inhomogeneous cylinder,

b. said explosive fisheye lens having an outer cylindrical warhead fragmentation casing,

c. said cylindrical casing being filled with explosives,

said explosives consisting of a plurality of concentric cylindrical explosive shells about a cylindrical explosive core,

d. a plurality of linear detonator arrays mounted and equally spaced about the cylindrical surface of said warhead casing in parallel alignment with the cylinder axis of said explosive. fisheye lens,

e. fire control means for selectively firing any of said detonator arrays upon command,

f. said explosive fisheye lens warhead operable to be aimed in any radial direction by said fire control means by selectively firing a detonator on the opposite side of the warhead from the desired direction of aim,

g. said fisheye lens warhead upon detonation of any one of said detonator arrays operable to cause detonation waves to progress from the line of detonation through the entire warhead detonating all the explosive therein such that the detonation waves are focused on a line on the opposite side of the fisheye lens from the detonation line in the direction of aim directing intense jets of warhead fragments in the direction of aim.

2. A warhead as in claim 1 wherein said explosive shells and core are each of different explosive composition.

3. A warhead as in claim 1 wherein the adjacent explosive shells and core are each of different density.

Patent Citations
Cited PatentFiling datePublication dateApplicantTitle
US3326125 *Sep 20, 1965Jun 20, 1967Denis A SilviaSequenced initiation-a technique for explosive wave shaping
Referenced by
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US4170940 *Jul 7, 1977Oct 16, 1979Societe D'etudes, De Realisations Et D'applications TechniquesProjectile charges
US4655139 *Sep 28, 1984Apr 7, 1987The Boeing CompanySelectable deployment mode fragment warhead
US6920827Oct 31, 2003Jul 26, 2005Raytheon CompanyVehicle-borne system and method for countering an incoming threat
US6931994Nov 21, 2002Aug 23, 2005Raytheon CompanyTandem warhead
US6973878Jun 5, 2003Dec 13, 2005Raytheon CompanyWarhead with aligned projectiles
US7017496 *Mar 10, 2003Mar 28, 2006Raytheon CompanyKinetic energy rod warhead with imploding charge for isotropic firing of the penetrators
US7143698May 13, 2005Dec 5, 2006Raytheon CompanyTandem warhead
US7412916Jan 18, 2006Aug 19, 2008Raytheon CompanyFixed deployed net for hit-to-kill vehicle
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US7621222Feb 17, 2005Nov 24, 2009Raytheon CompanyKinetic energy rod warhead with lower deployment angles
US7624682Feb 17, 2005Dec 1, 2009Raytheon CompanyKinetic energy rod warhead with lower deployment angles
US7624683Jul 20, 2005Dec 1, 2009Raytheon CompanyKinetic energy rod warhead with projectile spacing
US7712465 *Jun 15, 2005May 11, 2010Black Market Sportz LimitedValve for gas operated gun
US7717042Jan 6, 2005May 18, 2010Raytheon CompanyWide area dispersal warhead
US7726244Jul 20, 2007Jun 1, 2010Raytheon CompanyMine counter measure system
US8127686 *Jul 20, 2005Mar 6, 2012Raytheon CompanyKinetic energy rod warhead with aiming mechanism
US8418623Apr 2, 2010Apr 16, 2013Raytheon CompanyMulti-point time spacing kinetic energy rod warhead and system
DE10251676B4 *Nov 7, 2002Jun 6, 2007TDW Gesellschaft für verteidigungstechnische Wirksysteme mbHFokussierte Unterwasserladung
DE19524726B4 *Jul 7, 1995May 24, 2006Nico-Pyrotechnik Hanns-Jürgen Diederichs GmbH & Co KGGefechtskopf
Classifications
U.S. Classification102/492, 102/701
International ClassificationF42C19/095
Cooperative ClassificationY10S102/701, F42C19/095
European ClassificationF42C19/095