Multiple shaped charge jet (SCJ) warhead

Patent metadata

Field	Value
Publication number	US-12535304-B2
Application number	US-202418742564-A
Country	US
Kind code	B2
Filing date	Jun 13, 2024
Priority date	Jun 13, 2024
Publication date	Jan 27, 2026
Grant date	Jan 27, 2026

Abstract

In a MSCJ warhead detonation of the main charge is controlled to provide elevated pressure at multiple locations on the back surface of the liner to cut the liner and to form and propel forward a plurality of SCJs. An initiation system is configured for multi-point initiation of a plurality of booster charges to detonate the main charge to produce a plurality of detonation waves that constructively interfere at multiple locations on the back surface of the liner to form pressure hot spots that cut the liner and to form and propel forward a plurality of SCJs. In different embodiments, the elevated pressures are between 110% and 200% of the detonation pressure at the front of an individual detonation wave. The liner may, for example, include a plurality of recesses such as shallow dimples or deeper conical structures in which case the boosters are aligned to the center of the recessed structures.

First claim

We claim:

1 . A warhead having a height H 1 along an axis and a diameter D 1 , comprising:
a main charge;
a liner on a top surface of the main charge;
a plurality of booster charges spaced apart on a bottom surface of the main charge; and
an initiation system configured for multi-point initiation of the plurality of booster charges to detonate the main charge to produce a plurality of detonation waves;
wherein the liner is positioned within a defined range from the plurality of booster charges equal to a height H 2 of the main charge along the axis in which 0.3<=H 1 /D 1 <=0.6 such that pairs of directly adjacent detonation waves constructively interfere to form elevated pressures at multiple locations on the back surface of the liner to cut the liner and to form and propel forward a plurality of shaped charge jets (SCJs).

2 . The warhead of claim 1 , wherein the elevated pressures at the multiple locations is at least 110% a detonation pressure at the front of the detonation waves between the locations.

3 . The warhead of claim 2 , wherein the elevated pressures at the multiple locations is up to 200% of the detonation pressure.

4 . The warhead of claim 1 , wherein the liner includes a plurality of recesses, wherein the plurality of booster charges are aligned to the centers of the recesses such that each recess is cut and formed into a SCJ.

5 . The warhead of claim 1 , wherein each SCJ has a tip velocity of 4-10 km/s and a penetration depth of 7-10× a diameter of the corresponding recess.

6 . The warhead of claim 4 , wherein each recess has an apex angle of less than 180°.

7 . The warhead of claim 4 , wherein each recess is a dimple having an apex angle of 120-170°.

8 . The warhead of claim 4 , wherein each recess is a conical structure having an apex angle 40-120°.

9 . The warhead of claim 4 , wherein each recess has a recess diameter D 2 across the axis, wherein 0.5<=H 2 /D 2 <=1.5.

10 . The warhead of claim 1 , wherein the initiation system comprises:
an inert housing including a single point initiation site and a plurality of tracks that connect the single point initiation site to the plurality of booster charges; explosive material in the plurality of tracks; and a detonator at the single point initiation site, wherein initiation of the detonator produces detonation waves that travel through the explosive material in the tracks to initiate the plurality of booster charges.

11 . The warhead of claim 10 , wherein the plurality of tracks are equal length to facilitate simultaneous initiation of the plurality of booster charges.

12 . A warhead having a height H 1 along an axis and a diameter D 1 , said warhead comprising:
a main charge having a height H 2 ;
a liner on a top surface of the main charge, said liner having a plurality of recesses each having a diameter D 2 and an apex angle less than 180°;
a plurality of booster charges spaced apart on a bottom surface of the main charge and aligned to centers of the plurality of recesses; and
an initiation system configured for multi-point initiation of the plurality of booster charges to detonate the main charge produce a plurality of detonation waves;
wherein the liner is position within a defined range H 2 from the plurality of booster charges in which 0.3<=H 1 /D 1 <=0.6 and 0.5<=H 2 /D 2 <=1.5 such that pairs of directly adjacent detonation waves constructively interfere to form elevated pressures at multiple locations on the back surface of the liner at the edges of the recesses to cut the liner and to form the recesses into a plurality of shaped charge jets (SCJs) that are propelled forward.

13 . The warhead of claim 12 , wherein the elevated pressures at the multiple locations between 110% and 200% of a detonation pressure at the front of the detonation waves between the multiple locations.

14 . The warhead of claim 12 , wherein each recess is a dimple having an apex angle of 120-170° or a conical structure having an apex angle of at most 40-120°.

15 . A warhead having a height H 1 along an axis and a diameter D 1 , comprising:
a main charge;
a liner on a top surface of the main charge, said liner having a plurality of recesses;
a plurality of booster charges spaced apart on a bottom surface of the main charge and aligned to centers of the plurality of recesses; and
an initiation system including an inert housing having a single point initiation site and a plurality of tracks that connect the single point initiation site to the plurality of booster charges, explosive material in the plurality of tracks and a detonator at the single point initiation site, wherein initiation of the detonator produces detonation waves that travel through the explosive material in the tracks to initiate the plurality of booster charges to detonate the main charge and produce a plurality of detonation waves;
wherein the liner is positioned at a defined range from the plurality of booster charges equal to a height H 2 of the main charge along the axis in which 0.3<=H 1 /D 1 <=0.6 such that pairs of directly adjacent detonation waves constructively interfere to form elevated pressures at multiple locations on the back surface of the liner at a pressure between 110% and 200% of a detonation pressure of a single detonation wave to cut the liner and to form and propel forward a plurality of shaped charge jets (SCJs).

16 . The warhead of claim 14 , wherein each recess is a dimple having an apex angle of 120-170° or a conical structure having an apex angle of at most 40-120°.

Assignees

• Raytheon Co

Inventors

• Sadler Coulton T
• Lukow Brian J
• Turner Christopher M
• Johnson Michael R

Classifications

• F42B12/16

  in combination with an additional projectile or charge, acting successively on the target {(see also F42B12/625)} · CPC title

• F42B12/10 Primary

  with shaped or hollow charge (shaped or hollow charges per se F42B1/02 {; mines having hollow charges F42B23/04}) · CPC title

• F42B1/02

  Shaped or hollow charges (blasting cartridges with cavities in the charge F42B3/08; oil winning using shaped-charge perforators E21B43/116) · CPC title

• F42B1/028 Primary

  characterised by the form of the liner · CPC title